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1146

DEPARTMENT OF THE AIR FORCE

HEADQUARTERS OGDEN AIR LOGISTICS CENTER

HILL AIR FORCE BASE, UTAH  84056-5609 
 

FOREWORD 

Description:  The purpose of this security classification guide is to provide the basis for assigning the degree of security protection for information, regardless of form, concerning the Minuteman and Peacekeeper weapon systems.  The Minuteman and Peacekeeper weapon systems include the Minuteman and Peacekeeper Intercontinental Ballistic Missiles (ICBMs), launch facilities (LFs), missile alert facilities (MAFs), missile support bases (MSBs), support equipment, test equipment/facilities and Minuteman/Peacekeeper operational codes.  This Guide should be used in conjunction with the MK11, MK 12, MK 12A, MK 21 Guides. 

AUTHORITY:  DoD 5200.1-R/AFI 31-401, Information Security Program Management and Executive order 12958, Classified National Security Information. 

OFFICE OF PRIMARY RESPONSIBILITY:  ICBM System Program Office, Ogden Air Logistics Center (OO-ALC/LM) 

ORIGINAL TOP SECRET CLASSIFICATION AUTHORITY:  Commander, Ogden Air Logistics Center 
 
 

ORIGINATING OFFICIAL: 
 
 

THOMAS W. TAIT

Deputy Program Director

ICBM Systems Program Office 
 
 

COORDINATING OFFICIAL: APPROVING OFFICIAL:  
 
 

TIMOTHY G. HARDY, Lt Col, USAF RICHARD H. ROELLIG, Major General, USAF

Commander, 75th Security Forces Squadron Commander

 

        
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

This page intentionally left blank. 

 

Table of Contents 

Section  Page 

Attachment 2 (Peacekeeper)

 

SECTION I 

GENERAL INSTRUCTIONS 
 

1. PURPOSE:  This Guide identifies information developed during various phases of the development, production, deployment and subsequent maintenance phases of the Minuteman and Peacekeeper weapon systems requiring protection in the interest of national security. 
2. OFFICE OF PRIMARY RESPONSIBILITY (OPR):  This Guide is issued by OO-ALC/LM.  Classification management of this Guide is the responsibility of 75 SFS/SFA.  Inquiries concerning content or interpretation of this Guide should be addressed to:  

       OO-ALC/LMDM     75 SFS/SFAI

       6014 Dogwood Ave    6010 Gum Lane

       Hill AFB UT 84056-5816    Hill AFB UT 84056-5825 

       DSN 777-3015     DSN 777-7811

       COMM (801) 777-3015    COMM (801) 777-7811 

3. CLASSIFICATION RECOMMENDATIONS:  Send completely documented and justified recommendations for change through appropriate channels to the OPR if the security classifications in this Guide impose impractical requirements, or if operational conditions, technological changes in the state-of-the-art, or any other contributory factors indicate a need for changes.  Pending final decision, handle and protect the items of information involved at the highest of the present or recommended classifications.  Users of this Guide are encouraged to assist in improving and maintaining the currency and adequacy of this Guide.  
4. APPLICATION, REPRODUCTIONS, AND DISSEMINATION:  
a. Specified groups involved with Minuteman and Peacekeeper weapon systems, including industrial activities may make reproductions and extracts or selections of portions of this Guide. 
b. Distribution of this Guide includes those offices specified in DOD 5200.1-R and other interested Government agencies and contractor facilities. 
c. All agencies and offices requiring this Guide will be on an official distribution list whether it be primary distribution from this office or secondary distribution from the base or  unit focal point.  
5. "FOR OFFICIAL USE ONLY" (FOUO):  For Official Use Only (FOUO) is not a security classification.  However, handle, protect, and dispose of FOUO information according to AFI 37-131, Freedom of Information Act Program  or the applicable industrial security guideline, DOD 5220.22-M, National Industrial Security Program Operating Manual.  
 
6. MANUFACTURE, TEST, AND ASSEMBLY:  During manufacture, test, and assembly process, the classification assigned by this Guide applies at the earliest point whenever design, performance, and/or other classified characteristics can be derived from or traced to the system(s) identification herein.  
 
7. DISASSEMBLY AND REPAIR:  During disassembly and repair, the classification assigned by this Guide no longer applies at the earliest point where design, performance or other classified characteristics can no longer be derived from or traced to the system(s) identified herein.  
8. TEMPEST REQUIREMENTS:  TEMPEST requirements must be considered whenever classified automated data processing (ADP) will occur.  ADP refers to any electronic or electromechanical equipment which might process classified information.  
 

 

SECTION II 

ADMINISTRATIVE DETAILS 
 

1. PUBLIC RELEASE:  The fact that this Guide shows certain details of information as unclassified does not permit automatic public release of them.  Send proposed public disclosures of unclassified information regarding MM ICBMs to OO-ALC/PA, 7981 Georgia Street, Hill AFB, UT 84056-5824 for review before the date the proposer needs them for release.  
a. The term "information" applies, but is not limited to, articles, speeches, photographs, brochures, advertisements, displays, and presentations, on any phase of the MM or PK weapon system. 
b. Defense contractors and other agencies must screen all information they submit for determination of releasability to ensure it is both unclassified and technically accurate.  The letter of transmittal must certify this view.  Copies of the material may not be released outside official channels until the review process is complete.  If you find information during the review process that you suspect is classified, notify all holders of the document the degree of protection required.  When doubt exists concerning the classified status of a proposed release pertaining to this program, OO-ALC/LM makes the final decision.  The material submitted for review must include a valid suspense date, if applicable.  
c. Only information that has been reviewed and certified for public release may be released.  Submit information developed after initial approval for public release for review and further processing as outlined in a. and b.  
d. Material which requires an export license may not be entered into security review channels for public release approval to circumvent the licensing requirements of the Departments of State and Commerce.  
e. Obtain approval for planned or contemplated visits of public media representatives from OO-ALC/LM and OO-ALC/PA.  
2. RELEASE OF CLASSIFIED INFORMATION TO FOREIGN GOVERNMENTS OR THEIR REPRESENTATIVES:  Any military activity or defense contractor receiving a request from a foreign government or representative thereof for classified information pertaining to the MM AND PK weapon system must send the request to OO-ALC/FMM/FDPO, Hill AFB, UT 84056.  Contractors who wish to honor such requests rather than send them to the Foreign Disclosure Office, must apply for an export license according to the International Traffic in Arms Regulation (ITAR) and notify the military of their intent to apply for such license.  
3. RELEASE OF UNCLASSIFIED TECHNICAL INFORMATION (NOT APPROVED FOR PUBLIC RELEASE)  TO U.S. CITIZENS OR FOREIGN NATIONALS RESIDING IN A FOREIGN COUNTRY:  Any defense contractor must either obtain the approval from the cognizant military activity under the ITAR or apply for an export license to the Department of State under the ITAR and notify the military of their intent to apply for such license.  Material which requires an export license may not be entered into security review channels for public release approval in order to circumvent the license requirements of the Departments of State or Commerce.  
4. This publication of the ICBM Security Classification Guides incorporates the changes mandated in Executive Order 12958.  The following information is provided as a quick reference as to reasons for classification and declassification exemptions.  
• To be eligible for classification, information must fall within one or more of the categories of information listed in Section 1.5 of the Order.  These reasons are identified in the guide as 1.5.a, 1.5.b, etc.  
a. Military plans, weapons systems, or operations.  
b. Foreign government information.  
c. Intelligence activities (including special activities), intelligence sources or methods, or cryptology.  
d. Foreign relations or foreign activities of the United States, including confidential sources.  
e. Scientific, technological, or economic matters relating to the national security.  
f. United States Government programs for safeguarding nuclear materials or facilities.  
g. Vulnerabilities or capabilities of systems, installations, projects or plans relating to the national security.  
• All information must be declassified or reevaluated within 10 years unless it meets one or more of the criteria established by the Order.  These exemptions are identified in the guide as X1, X2, etc.  
X1. Reveal an intelligence source, method or activity, or a cryptologic system or activity.  
X2. Reveal information that would assist in the development or use of weapons of mass destruction.  
X3. Reveal information that would impair the development or use of technology within a United States weapons system.  
X4. Reveal United States military plans or national security emergency preparedness plans.  
X5. Reveal foreign government information.  
X6. Damage relations between the United States and a foreign government, reveal a confidential source, or seriously undermine diplomatic activities that are reasonably expected to be ongoing for a period longer than 10 years.  
X7. Impair the ability of responsible United States Government officials to protect the President, the Vice President, and other individuals for whom protection services, in the interest of national security, are authorized.  
X8. Violate a statute, treaty, or international agreement.  

 

SECTION III 

PERFORMANCE DATA 
 

1. The purpose of this section is to establish the philosophy of the classification of test data, raw and processed, and operational data.  Precise distinctions between unclassified and classified data or between data at various levels of classification cannot always be achieved.  Often, the decision as to proper classification of data depends upon the context in which the data is viewed or to the extent to which the source and nature of the data is apparent or, particularly in the case of raw data, on the availability of information on the format or storage or calibration conventions which are required in order to understand the information in the data.  Keeping the above factors in mind, judgment should be used in assigning classification.  
a. Data may be derived from flight test of components or the entire system.  The components flown may be operationally or experimentally configured.  The data may directly originate from:  
b. Data may be derived from ground tests of components of the system.  The configuration may be either operational or experimental.  The data may originate from a variety of sources.  
c. Data may originate from theoretical studies, in the form of quantitative predictions or interpretations of system component performance under specified conditions.  
2. DATA DIFFERENTIATION: 
a. A collection of data is known as a record regardless of the physical form in which the data appears.  For the purposes of this Guide, it is proper to distinguish three types of data records.  
   Magnetic tapes
   Decks of computer cards
   Computer printouts (listings)
   Manuscript scratch sheets
   Oscillograph records
   Rough operator logs
   Photographic displays:
3. OPERATIONAL DATA: 

Operational data includes that data accumulated during normal operation of the weapon system recorded by the Expanded Missile Data Analysis System (EMDAS) and consisting of Line Replaceable Unit (LRU) failure, system status and Inertial Measuring Unit (I) Performance Data (IPD).  While these data elements may lead to classified data, they, in themselves, under the definitions provided by this Guide, do not provide information for the derivation of reliability and accuracy.  

   a. LRU failure and system status data  

LRU failure and system status data provides information that supports the determination of system and subsystem reliability.  Since this data provides only some of the factors required, it does not provide specified interval or stated condition; it is considered UNCLASSIFIED unless specifically classified in accordance with other sections of this Guide.
b. IPD 
IPD originates in the MGS as a result of normal alert operations.  These data express the ground performance of the inertial instruments and airborne computer computations relating to that performance.  While these data are used to measure stability and predict long term performance and are related to guidance accuracy, it is not sufficient to predict weapon system accuracy.  The official alert rate cannot be derived from IPD even though the operational status of some key components of the weapon system can be.  

 

SECTION IV 

DEFINITIONS 

a.  Access: 
b.  Assembly:  The first major subdivision of a component. 
c. Atomic weapon:  An atomic weapon as defined in Public Law 708, 83rd Congress, Section 11d, is any device utilizing atomic energy, exclusive of the means of transporting or propelling the device (where such means is a separable or divisible part of the device), the principal purpose of which is for use as or for development of a weapon, weapon prototype or weapon test device.  See Reentry Vehicle (RV) Guides. 
d. Auxiliary system:  A separate function associated with the missile weapon system but not part of the missile itself (e.g., launch facility personnel access auxiliary system). 
e. Component:  The first major subdivision of a subsystem; e.g., the computer is a component of the guidance subsystem. 
f. Computer memory security check (CMSC):  A nonlinear compilation of memory content resulting in a characteristic number. 
g. Communications Security (COMSEC):  COMSEC is a process designed to protect any and all information that may be of possible intelligence value.  A designation or marking applied to all information concerning COMSEC exclusive of that designated CONTROLLED COMSEC ITEM or CRYPTO (former designation still in use). 
h. Configuration item (CI):  An aggregation of hardware/software or any of its discrete portions which satisfies an end use function and is designated by the government for configuration management.  The CI number and the Figure A (Fig A) number mean the same thing. 
i. Critical nuclear weapons design information (CNWDI):  Top Secret-Restricted Data or Secret-Restricted Data revealing the theory of operation or design of the components of a thermonuclear or implosion type fission bomb, warhead, demolition munitions or test device.  Information concerning arming, fusing and firing systems; limited life components; and total contained quantities of fissionable, fusionable and high explosive materials by type are excluded.  Among those excluded items are components that service personnel set, maintain, operate, test or replace.  See RV guides and the DOE/DOD Joint Nuclear Weapons Classification Guide and the Air Force Security Classification Guide for Nuclear Weapons. 
j. Deployment module:  That portion of the post-boost vehicle (PBV) which consists of the means for mounting and releasing RVs and penetration aids.  It may or may not include the post-boost control system (PBCS). 
k. Formerly Restricted Data (FRD):  Information removed from the Restricted Data category upon determination jointly by the Department of Energy (DOE) and Department of Defense that such information relates primarily to military utilization of atomic weapons and that such information can be adequately safeguarded as classified defense information.  
l. Hardness:  A measure of the ability of a system to withstand exposure to one or more effects of manmade hostile environments.  The resistance or degree of resistance to nuclear countermeasures or hostile environments such as neutron exposure or electromagnetic pulse (EMP) radiation.  This definition encompasses those environments resulting from normal handling; powered flight and/or atmospheric reentry of the vehicle are not included. 
m. Hardness critical item:  Any item at any assembly level which is launch essential and/or mission critical or could adversely impact launch-essential or mission-critical equipment if hardness were not considered. 
n. Latch-up time:  The time required by the security subsystem to detect and hold a security violation to assure interrogation of the Launch Facility (LF) by the Missile Alert Facility (MAF). 
o. Launch essential:  An item of equipment or a subsystem function or characteristic is launch-essential if it is required in order to launch the missile from its silo or whose malfunction would prevent such launch in a pre-, trans- or  post- nuclear attack environment. 
p. Maneuvering Reentry Vehicle (MaRV):  The concept of a RV as an independent entity capable of altering its own course after release from the booster.  It does not cover manned vehicles. 
q. Minuteman (MM) Weapon System:  The MM weapon system includes the WS-133B or WS-133AM facilities, LGM30B, LGM30G missiles, MK11 Series, MK12 and MK12A RSs. 
r. Missile guidance set (MGS):  That portion of the missile which measures the missile position and attitude and provides control signals to all stages of the missile. 
s. Mission critical (MC):  An item of equipment or a subsystem function is MC if it is required to launch a missile within a given time span or to successfully complete the mission or whose malfunction would prevent such mission completion.  Successful completion of the mission includes: 

       (3)  System retains its retargeting capability 

       (4)  System retains redundancy in communications (cable and radio) 

       (5)  System retains valid status reporting capability 

       (6)  System retains specified emergency and extended survivability capability. 

t. Multiple Independent Reentry Vehicle (MIRV):  The concept of one booster carrying multiple reentry vehicles which can be aimed at separate targets. 
u. Peacekeeper (PK) Weapon System:  The PK weapon system consists of the LGM-118 missile, WS-133 AM missile alert and launch facilities modified with a unique PK canister system for support and launch of the PK missile, and MK21 RSs.     
v. Penetration aids (Pen aids):  Elements such as decoys and chaff which increase the probability of successful RV penetration of an area which is defended against ballistic missile attack. 
w. Post-boost vehicle (PBV):  That portion of a missile which performs its primary function after separation from the prime launch vehicle and which consists of a payload (single/multiple RVs and/or Pen Aids), structure and equipment for providing guidance and control, propulsion and deployment of the payload.  This includes PBCS and PSRE.

x. Propulsion system rocket engine (PSRE):  That portion of the PBV which provides linear acceleration in any direction attitude control and angular acceleration about the pitch and yaw axes. 
y. Reentry system (RS):  Portions of the ICBM or payload which have an active role to perform after third stage thrust termination.  This usually includes the RV, Pen Aids and Pen Aids wafer on the MM II and the support payload platform, Pen Aids and RVs on the MM III. 
z.  Reentry vehicle (RV):  That part of a ballistic missile designed to reenter the earth's atmosphere in the terminal portion of the trajectory.  Its prime purpose is to enable an internal payload to survive the severe environment encountered during reentry until impact or warhead detonation.  In the strictest sense of the word, the term RV automatically includes the payload or warhead. 
aa. Reliability:  The probability that an item will perform its intended function for a specified interval under stated conditions.  Normally data sets, such as those contained in maintenance failure/status reporting systems, are unclassified because they do not contain all the elements necessary to determine reliability as defined above.  If any data set describes a specific vulnerability or limitation, it will be classified in accordance with the specific area of this Guide covering the system/subsystem described by that data set. 
ab. Restricted Data (RD):  All data concerning (1) design, manufacture or utilization of atomic weapons, (2) the production of special nuclear material or (3) the use of special nuclear material in the production of energy but shall not include data declassified or removed from the RD category pursuant to the Atomic Energy Act of 1954, Section 142. 
ac. SUAVE:  Silo Upgrade Addressing and Verification program. 
ad. Subassembly:  The first major subdivision of an assembly. 
ae. Subsystem:  The first major subdivision of a system, e.g., of the missile system, the propulsion subsystem. 
af. TSEC:  Transmission security designation used for COMSEC items. 
ag. Train:  As related to the weapon systems, the term "train" refers to a reentry train.  A reentry train consists of a series of objects in one of three configurations (i.e., chaff alone, RV with chaff or RV alone) which are deployed from a common RS and are targeted to arrive on the same target at  approximately the same time.  Any of the three configurations can also have its payload deployed in any train combination.  The reentry train is sometimes referred to as a cloud train due to the presence of chaff clouds after chaff deployment. 
ah. Unclassified Controlled Nuclear Information:  Unclassified information pertaining to the physical protection of special nuclear material in accordance with Section 1123 of Public Law 100-180.  Interim procedures are contained in Under Secretary of Defense, Security Policy, Memorandum, Subject:  Interim Guidance for Identifying and Controlling Unclassified Controlled Nuclear Information (UNCI) dated 18 Sep 1988. 
ai. Vulnerability:  The characteristics of a system which cause it to suffer a degradation (reduced capability to perform the designated mission) as a result of having been subjected to a certain level of each effect in a manmade hostile environment. 
aj. VNTK:  An acronym which stands for VN - vulnerability, T - type of device and K - constant.  It is a term used for assessing hardness achieved at a silo, squadron, wing or the force. 
ak. Weapon system:  All elements necessary to attain an operational missile capability, i.e., research and development, missiles, test and training programs, launch complexes, support bases, launch and support organizations, etc. 

 

SECTION V 
 

DISTRIBUTION 
 

20 AF/CC, Ste 1, /DO, Ste 2, /SE, Ste 4,/

LG, Ste 3,

7100 Saber Rd

20AF/MOC 6600 HQ Drive - 3943

Francis E Warren AFB, WY  82005-xxxx

22nd AF/SOM

Travis AFB, CA 94535-5000

30 OG/CC, 747 Nebraska Ave, Ste 32,  -6292

30 LG/CC, 747 Nebraska Ave, Ste 31, -6921

30SW/XPOD, 747 Nebraska Ave, Ste 34,-6294

576 FLTS/TEE, 1786 Utah St, Ste A

SMC/Det 9/ENM, 1515 Iceland Rd, Ste A

Chief, KMR Field Office/Attn:  CSSD-KA-RV

P.O. Box 5309, -0930

Vandenberg AFB, CA  93437-5000

321 MG/CC

       OGCC

       FMS

319 SPS/SPAI

MAIL ALL COPIES TO

450 G St, Ste 321

Grand Forks AFB, ND  58205-6023

341 MG/CC

       OG/CC

       FMS

43 SPS/SPAII

MAIL ALL COPIES TO

341 MAG, BLDG 500, STE 148, 2177 St N.

Malmstrom AFB, MT  59402-7538

341 SW/LGLOJ

2177 Street North

Bldg 500, Ste 150

Malmstrom AFB, MT  59402-7538

4220 Weapons System Evaluation Squadron

Offutt AFB, NE 68113-5001

625 MOF/TAB

901 SAC BLVD

Ste 2B23

Offutt AFB, NE  68113

650 ABW/CE

225 North Rosemond Blvd

Edwards AFB, CA  93524-8540

6595 Test and Evaluation Group/MTP

Vandenberg AFB, CA  93437-5000

750 SPTS/SPA, Box 051, -1236

750 SGP/OL-A-DOO, Box 061, -1237

1808 Lockheed Way

Onizuuka AFB, CA  94089-xxxx

363 TRSS, -5420

Sheppard AFB, TX  76311-xxxx

90 MG/CC

       OS

       LG

       SSS/SPAI

MAIL ALL COPIES TO:

5305 Randall Ave

Francis E Warren AFB, WY  82005-2274

91 MG/CC

       OS

       OMMS

       FMMS

       5 SPS/SPAI

MAIL ALL COPIES TO

5 MSS/MSIAC, 220 Peacekeeper PL

Minot AFB, ND  58705-5000

95 SPTG/AS

15 South Munroc Dr

Edwards AFB, CA 93524-8040

ACDA Classification Advisor

US Arms Control & Disarmament Agency

320 21st Street NM

Washington DC 20451

SP - 100 Kindel Dr, Ste C301, - 5000

Arnold AFS, TN 37389-xxxx

Aerojet Propulsion Division

ATTN:  Crawford Butler

Bldg 2006, Dept 1711

PO Box 13222

Sacramento, CA  95813-6000

Aeromet, Inc

ATTN:  Facility Security Officer

PO Box 701767

Tulsa, OK  74170-1767

AFMC

Wright Patterson AFB, OH  45433-5006

4375 Chidlaw Road

   SP

   SC

AFMC/SPO, Ste 5E21, 4255 Logistics

Ave, -5760/

XRS, STE 6, 4315 Chidlaw Rd, -5006

ASC/SP, Rm 103A, 1801 10th St, -6825

1970 3rd St, -6504

Wright-Patterson AFB, OH 45533-xxxx

AFSAA/SAI

1580 Air Force Pentagon

Washington DC 20330-1580

AFSPC SD/SPI

LAAFB/ PO Box 92969

Los Angeles, CA  90009-2960

AFTAC/DOJ

1030 South Highway AIA

Patrick AFB, FL  32925-3002

Attn:  Capt. McCobb

Air Force Media Center

AFMEC/SP

1363 Z St, Bldg 2730

March AFB, CA 92518-2717

Alliant Techsystems, Inc

Bacchus Works (ATTN:  Security Supervisor)

PO Box 98

Magna, UT  84044

Allied Signal Aerospace

Electronics Systems

ATTN:  Security Department

250 Knotter Drive

Cheshire, CT  06410

Appraisal and Disposition Section

Records Group 342

Federal Archives and Records Center

1000 Commodore Drive

San Bruno, CA  94066-2350

ASD/FM (Operations)

The Pentagon, Rm 3D868

Washington DC 20301-1100

Atlantic Research Corp

5945 Wellington Road

Gainesville, VA  22065

Atlantic Research Corporation

Liquid Propulsion

PO Box 300 LPO

6686 Walmore Rd

Niagara Falls, NY  14304-0300

Atlantic Research Corporation

Liquid Propulsion

PO Box 771

Clearfield, UT  84015

AVCO Corporation

Textron Defense Systems Division

ATTN:  Security Supervisor

201 Lowell Street

Wilmington, MA 01887

AWFL/SP

Kirtland AFB, NM 87115-5000

Batelle Columbus Laboratories

ATTN:  Security Officer

505 King Avenue

Columbus, OH  43201-2693

Boeing Guidance Repair Center

Attn:  Security

813 Irving-Wick D West

Newark AFS, OH 43055-5149

Boeing North American

Autonetics Strategic Systems Division

3370 Miraloma Ave

Anaheim, CA  92803

Boeing North American

Autonetics Strategic Systems Division

ATTN:  K. George

6039 Wardleigh Rd

Hill AFB, UT  84056-5838

Capitol Hill Area, DIS

Hoffman Building

2416 Eisenhower Avenue

Alexandria, VA  22331-1000

Central Region, DIS

Mid-Western Region

610 South Canel Street, Room 908

Chicago, IL  60607-4599

Central Region, DIS

Southwestern Sector

106 Decker Court, Suite 200

Irving, TX  75062-2795

Charles Stark Draper Laboratories, Inc

ATTN:  Document Control

Mail Station 74

555 Technology Square

Cambridge, MA  02139

Chief National Archives

Federal Archives & Records Center, NARA

24000 Avila Road

Laguna Niguel, CA  92656-3497

Commander

US Army Missile Command

AMSMI-WS-SA

ATTN: Mr Seinford

Redstone Arsenal, AL  35898

Commander,

Field Command

Defense Nuclear Agency

ATTN: FCSS

1680 Texas St SE

Kirtland AFB, NM 87117-5669

Commander, USAKA

ATTN:  CSSD-KA-RO

P.O. Box 26

APO San Francisco, CA  96555

Commanding Officer

Naval Explosive Ordnance Disposal Center

ATTN: Tech Library Division

Indianhead Naval Station, MD 20640-5000

DCASMA BOSTON

ATTN:  FACC-C2

495 Summer St

Boston, MA  01120-2109

DCG USASSDC

ATTN:  CSSD-TE-O/CSSD-KA-RH

P.O. Box 1500

Huntsville, AL  35807-3801

Defense Nuclear Agency/ISCM

Washington DC  20305-2000

Defense Technical Information Center

Building 5, Cameron Station

Alexandria, VA  22304-6145

Deputy Director Security Classification Safeguards

DISS, ODASD(CISCM), OASD (C31)

The Pentagon, Rm 3C274

Washington DC  20301-3040

DET 1 OO-ALC

901 SAC Blvd, Ste 1F21

Offutt AFB, NE  68113-5660

Director

National Imagery Mapping Agency Aerospace Center

ATTN: SO (Jack Cumbow)

3200 South Second St

St Louis AFB, MO  63118-3399

Director

National Imagery Mapping Agency

ATTN:  ISA ST A-15 (H. Ketts)

Fairfax, VA  22031-2137

Director of Security Plans and Programs

Office of the Deputy Under Secretary of Defense (Policy)

Washington CD  20301-2000

Director or Information Security

Ofc of the Dep Under Sec of Defense (Policy)

Washington DC  20301-0001

Directorate, Freedom of Information and Security Review

Office of the Assistant Secretary of Defense

(Public Affairs)

1400 Defense Pentagon

Washington DC  20301-1400

DISA/DO

701 S. Court House Rd

Alexandria, VA  22204-2219

DMA

Bldg 56, ATTN:  PR

US Naval Observatory

Washington DC  20350

DMAAC/GCB

ATTN:  Operations Division

P.O. Box 9617

Francis E Warren AFB, WY  82005-6300

DPMC

The Boeing Company

PO Box 3707

Seattle, WA  98124-2207

DPMC

Rockwell International

Rocketdyne Division

6633 Canoga Avenue

Canoga Park, CA  91303-2790

DPMC

Northrop Corporation

2301 W. 120th Street

Hawthorne, CA  90250-3363

DPMC

Martin Marietta Aerospace

Denver Division

PO Box 179

Denver, CO  80201-1079

DPMC

Morton Thiokol Corporation

Wasatch Division

PO Box 524, MS-250

Brigham City, UT  84032-0524

DPMC

GTE Government Systems Corporation

360 First Avenue

Needham Hts, MA  02194-2787

DPMC

Hercules Inc

Aerospace Division

PO Box 98

Magna, UT  84044-0098

DPMC

Aerojet General Corporation PO Box 15846

PO Box 15846

Sacramento, CA  95852-1846

DPMC

General Electric Astrospace Division

ATTN:  Security

23 Goddard Blvd

King of Prussia, PA  19406-2902

DPMC DET 40

AVCO Corporation

Textron Defense Systems

201 Lowell Street

Wilmington, MN  01887-2941

DPMC Rockwell International Corp

3370 Mira Loma

Anaheim, CA  92803-3110

DPMC San Antonio

Austin Residency

6500 Tracor Lane

Austin, TX  78725-2000

DPMC TRW

1 Space Park, E1/1081

Redondo Beach, CA  90278-1078

DTIC

Cameron Station

Alexandria, VA  22304-6100

Dynamics Research Corporation

ATTN:  Security Office

60 Concord St

Wilmington, MA  01887-2934

Ertec Western, Inc

ATTN:  Security Office

3777 Long Beach Blvd

Long Beach, CA  90807-3309

General Electric Company

Ordnance Systems Division

100 Plastic Ave

Pittsfield, MA  01201-3698

Gilbert Associates, Inc

ATTN:  Security Office

PO Box 1498

Reading, PA  19603-1498

GTE Government Systems Corporation

3502 Lincoln Ave, Ste 4

Ogden, UT  84401

GTE Government Systems Corporation

ATTN:  Security Supervisor

77 ìAî Street

Needham, MA  02194

Hercules Inc

Aerospace Division

Bacchus Works

ATTN:  Security Office

PO Box 98

Magna, UT  84044-0098

Honeywell, Inc

ATTN:  Dee Burch, M/S 190-1

13350 US Highway 19N

Clearwater, LF  34624-7290

HQ AETC/

AOS/AOX, Ste 2, 1 F ST, -4325

Randolph AFB, TX  78148-xxxx

HQ AFHRA/ISR

600 Chennault Circle

Maxwell AFB, AL  36112-6424

HQ AFHSO/HOS

170 Luke Ave Suite 400

Bolling AFB, DC  20332-5113

HQ AFIA/IM

6700 G Ave SE

Kirtland AFB, NM 87117-5670

HQ AFOTEC/SP, 85OO Gibson Blue,

SE, -5558

377 SPS/CC/SPA, 1351 1st St SE, -5527

OL-NS/ENG, 1651 1st St SE, -5617

AFMC NSO/SWN, 1680 Texas St SE, -5669

Kirtland AFB, NM  87117-xxxx

HQ AFSC/SEW

9700 Avenue G SE

Kirtland AFB, NM  87117-5670

HQ AFSPC CEF/CC

1520 E Willamette Ave

Colorado Springs, CO  80909-4554

HQ AFSPC/

       DLM -4180

       DOT -4240

       DOM -4180

       DOMN -4180

       DRM -4760

       LGM -4470

       SCMB -4400

       SEWM -4260

       SFPON -4560

150 Vandenberg St, Ste 1105

Peterson AFB, CO  80914-xxxx

HQ DIS Industrial Security Office (VO410)

1340 Braddock Pl

Alexandria, VA  22314-1651

HQ DNA/ISIS

6801 Telegraph Rd

Alexandria, VA  22310-3390

HQ RL/SP

26 Electronic Parkway

Griffiss AFB, NY  13441-4514

HQ USAF

XOFS/XOOB/XORS/XORW

1480 Air Force Pentagon, -1480

LGSW/LGMW

1030 Air Force Pentagon, -1030

SEC

1400 Air Force Pentagon, -1400

Washington DC 20330-xxxx

HQ USAF/SPI

1340 Air Force Pentagon

Washington DC 20330-1340

HQ USSTRATCOM/

       J-005, Ste 1H9, -6005

       J-312/-331-334-362/-441/-443,

       Ste BA3, -8300

       J-511/-541, Ste 2E8, -6500

       J-523, Ste 2E8, -6500

       J-611, Ste 2B9, -6600

901 SAC Blvd

Offutt AFB, NE  68113-xxxx

ITT Federal Services Corporation

ATTN:  Facility Security Officer

PO Box 5728

Vandenberg AFB, CA  93437

Johnson Controls World Services, Inc

ATTN:  Document Control

401 Wynn Drive

Huntsville, AL  35805

Johnson Controls World Services, Inc

ATTN:  Document Control

PO Box 1761

APO San Francisco, CA  96555

KMR Weather Station

Aeromet, Inc

PO Box 67

APO San Francisco, CA  96555

Lawrence Livermore Laboratory

ATTN:  Classification Office (L-302)

PO Box 808

Livermore, CA  94551-9900

Litton Systems Inc

G&C Systems Division

5500 Canoga Avenue

Woodland Hills, CA  91365-6698

Lockheed-Martin

ATTN:  Facility Security Officer, M/S 13B

9970 Federal Drive

Colorado Springs, CO  80921-3697

Lockheed-Martin Missiles and Space

Valley Forge Operation

ATTN:  Security Supervisor

230 Mall Blvd

King of Prussia, PA  19406-2995

Lockheed-Martin Missiles and Space

ATTN:  Security Supervisor

PO Box 3504

Sunnyvale, CA  94088-3504

Logicon, Inc

ATTN:  Security Supervisor

PO Box 471

San Pedro, CA  90733-0471

Logicon, Inc

ATTN:  Security Supervisor

3701 Skypark Dr, Ste 200

Torrance, CA  90505-4794

Los Alamos National Laboratory

ATTN:  Group OS6

PO Box 1663

Los Alamos, NM  87545

MAC/SP

Scott AFB, IL  62225-5001

Maxwell Labs, Inc

S-Cubed Division

ATTN:  Security

PO Box 1620

LaJolla, CA  92038-1620

McDonnell Douglas

ATTN:  Denise Schmate

5201 Bolsa Avenue

Huntington Beach, CA  92647-0299

MIT Lincoln Laboratory

ATTN:  KREMS Site Manager

PO Box 58

APO San Francisco, CA  96555-5000

MIT/Lincoln Laboratory/KREMS

ATTN:  Bing Potts

PO Box 58

APO San Francisco, CA  96555

MIT/Lincoln Laboratory/KREMS Data Library

ATTN:  Document Control

PO Box 73

244 Wood Street

Lexington, MA  02173-9108

Morton Thiokol, Inc

Wasttch Division

ATTN:  Security Office

PO Box 524

Brigham City, UT  84032-0524

National Archives and Records Admin (NIR)

Records Group 342

Washington, DC  20408-0001

National Security Agency

Attn: DDI

9800 Savage Rd

Fort George Meade, MD  20755-6000

Northeast Region, DIS

Mid-Atlantic Sector

1040 Kings Highway North

Cherry Hill, NJ  08034-1908

Northeast Region, DIS

New England Sector

495 Summer Street

Boston, MA  02210-2192

Northrop Corporation

Electronics Division

ATTN:  Security Office

2310 W. 120th Street

Hawthorne, CA  90251-5032

NSA-Asst Dir NSA for COMSEC

Ft George G. Meade, MD  20755-5000

NSA/DDI

9800 Savage Rd

Fort George Mead, MD  20755-6700

OL-AA, Phillips Laboratory/XPG

Attn:  Noreen Diamond

29 Randolph Rd

Hanscom AFB, MA  01731-3010

OL-AC, Phillips Laboratory/SP

ATTN:  Danny Green

5 Pollux Dr

Edwards AFB, CA  93524-7062

ONRR

Massachusetts Institute of Technology

Lincoln Laboratory/RM E19-628

77 Massachusetts Avenue

Cambridge, MA  02139-4307

OO-ALC/

PA, 7981 Georgia St, -5824

TI/TIE, 5851 F St, -5713

75 SFS/SFAI 6010 Gum LN, -5825

649 EOD/ESO, 6316 Juniper Dr, -5931

Hill AFB UT  84056-xxxx

Orbital Sciences Corporation

Space Data Division

ATTN:  Security Supervisor

3380 South Price Rd

Chandler, AZ  85248

Pacific  Region, DIS

Southern and Northern Sector

3605 Long Beach Blvd, Suite 405

Long Beach, CA  90807-4013

Palisades Geophysical Institute, Inc

PO Box 1751

Cape Canaveral, FL  32920-1751

Pan Am World Services, Inc

ATTN:  Range Operations Manager

PO Box 1761

APO San Francisco, CA  96555-5000

R. A. Hanson Company, Inc

ATTN:  Security Office

PO Box 7400

Spokane, WA  99207-0400

Raytheon Company

ATTN:  Security Supervisor

528 Boston Post Road

Sudbury, MA  01776

Rockwell International Corporation

Rocketdyne Division

ATTN:  Security Office

6633 Canoga Avenue

Canoga Park, CA  91303-2790

Rockwell International Corporation

Rocketdyne Division

ATTN:  Security

PO Box 59098

Vandenberg AFB, CA  93437-5000

SA-ALC

NW, 413 Jackson, -5314

76SPS/SPA, 206 Duncan Dr, -5936

Kelly AFB, TX  78241-xxxx

SA-ALC/NWIS

1651 First Street SE

Kirtland AFB, NM  87117-5617

SAF/AAZD

c/o   HQ AU

55 LeMay Plaza South

Maxwell AFB, AL 36112-6335

Sandia National Laboratories

ATTN:  R.E. Martinell, 8535

Classification Officer

PO Box 969

Livermore, CA  94551-0969

Science Applications International Corporation

ATTN:  Security Supervisor

10260 Campus Point Dr

San Diego, CA  92121-1578

SDIO/DSIM

The Pentagon, Rm 1E1062

Washington DC 20330-7100

Secretary of the Air Force

AQQS(M),

1060 Air Force Pentagon, -1060

PAS

1690 Air Force Pentagon, -1690

Washington DC 20330-xxxx

Southeastern Region, DIS

2300 Lake Park Drive, Suite 250

Smyrna, GA  30080-7606

The Aerospace Corporation

ATTN:  Classification Management

PO Box 92957

Los Angeles, CA  90009

The Boeing Company

ATTN:  Security Supervisor

PO Box 3707

Seattle, WA  98124

The Boeing Company

ATTN:  Security

PO Box 1004

Clearfield, UT  84015

Thiokol

Wasatch Division

PO Box 524

Brigham City, UT  84302

TRW Data Technologies Division

ATTN:  Security

PO Box 6213

Carson, CA  90749

TRW Space and Electronics

ATTN:  Security Supervisor

One Space Park

Redondo Beach, CA  90278

TRW Strategic Systems Division

ATTN:  Security

PO Box 1310

San Bernardino, CA  92402

TRW Strategic Systems Division

Systems Integration Group

1104 Country Hills Drive

Ogden, UT  84403-2400

United Technology Corporation

Chemical Systems Division

ATTN:  Document Control

PO Box 49028

San Jose, CA  95161-9028

US DOE/Classification Division

P O Box 5400

Albuquerque, NM  87185-5400

Weidlinger Associates

ATTN:  Dr. Jeremy Isenberg

620 Hanson Way, Suite 100

Palo Alto, CA  94303-1014

Westinghouse Electric Corporation

Marine Division

ATTN:  Debra Martin

PO Box 3499

Sunnyvale, CA  90488-3499

XONTECH, Inc

ATTN:  Security Supervisor

6151 West Century Blvd

Los Angeles, CA  90045

 
 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

This page intentionally left blank 

 
 
 

 

SECTION I 

FUNDING, PROCUREMENT AND PRODUCTION 
 

 
Information Revealing

Classification

Reason

Date

Remarks

       
1 Complete funding for the entire WS-133A, WS-133B or WS-133AM program (including all appropriations) for the current and subsequent fiscal years except RV funds.

S-FRD

1.5.a (X2)

UNCLASSIFIED after DOD release.  See RV guides for RV funding data classification.
2 Complete funding to date, including the current fiscal year for the entire WS-133B and WS-133AM programs.

U

Includes numbers delivered and rate of delivery.
3 Complete funding for any one R&D or production contract.  
 
 
 
  a. Total unit cost of any missile.

U

 
 
  b. Total unit cost of any subsystem.

U

For warheads, see RV guides.
4 Parts, accessories and equipment available on the open market.

U

 
 
5 Provisioning parts breakdown except RV.

U

See RV guides.
6 Production data on operational force missile.  
 
 
 
  a. Total number of missiles to be produced on a given contract.

U

 
 
  b. Total number of missiles produced on all contracts.

U

 
 
  c. Total number of missiles                 planned for future production.

U

 
 
  d. Total number of missiles                 that have been have delivered to                 an operational site.

U

 
 
7 Production data on R&D missiles:  
 
 
 
  a. Total number of missiles                  planned or programmed.

U

 
 
  b. Total number of missiles that are produced on a given                 contract.

U

 
8 Subsystem production:  
 
 
 
  a. Total number of subsystems for                 future production for operational use except RV.

U

For RVs, see applicable RV guides.
  b. Total number of subsystems       planned for future production            for R&D use.

U

 
 
  c. Total number of subsystems             that have been produced on all              contracts.

U

 
 
 
  d. Total number of subsystems                 that have been produced on all                 contracts.

U

 
 
  e. Warhead subsystems production                 information.

U

See applicable RV guides.
  f. Pen Aids subsystems production                 quantities.

U

See Section XVII and XVIII.

 
 

SECTION II 

HARDWARE CLASSIFICATION 

See USSTRATCOM SD 501-12 for items identified as requiring special handling. 

 

Information Revealing

Visual

Access

Physical

Access

Remarks

         
1 Propulsion subsystem:      
  a. Complete Stage 1 propulsion subsystem, including nozzles

U

U or S

1.5.g (X2)

Stage 1 subsystem is UNCLASSIFIED prior to installation of classified P-89, Stage 1 nozzle control units.  SECRET for those subsystems with classified P-89s installed.
  b. Complete Stage 2 propulsion subsystem, including nozzles for MM I (WS-133A)

U

U

 
  c. Complete Stage 2 of MM II and III.

U

U or S

DECLAS

31 Dec 2007

Stage 2 subsystems UNCLASSIFIED prior to installation of classified P-90, Stage 2 attitude control group.  SECRET for subsystems with classified P-90s installed.
  d. Complete Stage 3 of MM III propulsion subsystem, including nozzle.

U

U or S

DECLAS

31 Dec 2007

Stage 3, MM III subsystems, UNCLASSIFIED prior to installation of classified P-116, liquid injection thrust vector control (LITVC) unit.  SECRET for subsystems with classified P-116s installed.
  e. Complete Stage 3 of MM II propulsion subsystem, including engine nozzles and thrust termination component.

U

U or S

DECLAS

31 Dec 2007

Stage 3, MM II subsystems UNCLASSIFIED prior to installation of classified P-91, Stage 3 nozzle control units.  SECRET for subsystems with classified P-91s installed.
  f. Complete PSRE

U

U

 
  g. Angular accelerometer between Stage 2 and 3, P-68.

U

U or S

DECLAS

31 Dec 2007

Unit UNCLASSIFIED prior to P/N 25170-102-21.  SECRET for P/N-21s.
  h. Nozzle control unit Stage 1, P-89

U

U or S

DECLAS

31 Dec 2007

UNCLASSIFIED prior to P/N 25340-102-581.  SECRET for P/N-581s and higher.
  i. Attitude control group, Stage 2, P-90

U

U or S

DECLAS

31 Dec 2007

UNCLASSIFIED prior to P/N 25333-102-551.  SECRET for P/N 551s and higher.
  j. Nozzle control unit, Stage 3, P-91

U

U or S

DECLAS

31 Dec 2007

UNCLASSIFIED prior to P/N 25341-102-581.  SECRET for P/N 581s and higher.
  k Cable assembly, Stage 1, P-93

U

U

 
  l. Cable assembly, Stage 2, P-113

U

U

 
  m. Cable assembly, Stage 3, P-114

U

U

 
  n. LITVC unit, P-116.

U

S

DECLAS

31 Dec 2007

Classification due to presence of hardness material
  o. Complete ordnance cable assembly for Stage 2, MM II retrofit, and Stage 2, MM III, Block IV, and Stage 3, MM II & III, Block IV.

U

U

 
  p. Complete aluminum ground strip assembly for MM III, Stage 3, Block IV.

U

U

 
  q. Complete roll control valve junction box and cable assembly for MM II, Stage 2 retrofit, and MM III, Stage 2, Block IV.

U

U

 
  r.  Complete raceway conductive strip assembly for Stage 3, MM III, Block IV.

U

U

 
  s. Complete boosters:      
 
  • (1 MM I

U

U or S

DECLAS

31 Dec 2007

Physical access will be classified SECRET if any classified components described in 1.a. through 1.j. above are incorporated.
 
  • (2) MM II

U

S

DECLAS

31 Dec 2007

Classified SECRET unless all classified hardware is removed.  All operationally configured boosters are SECRET.
 
  • (3) MM III

U

S

DECLAS

31 Dec 2007

See Remark in 1.s.(2) above
2 Reverse thrust subsystem:      
  a. Reverse thrust subsystem

U

U

 
  b. Complete roll control and LITVC system in Stage 2, Wing VI, and subsequent.

U

U

 
  c. Retro-rocket motor

U

U

 
  d. Tumble rocket motor

U

U

 
 
 
e. A portion of cured propellant for rocket motors.

U

U

 
3 Guidance subsystem:      
  a. MGS (NS10) which includes the stabilized platform, computer, magnetic memory.

U

C

DECLAS

31 Dec 2007

This subsystem is no longer deployed in the weapon system.  It is used at Vandenberg AFB.  Classified due to presence of design information currently used in NS17 units.
  b. MGS (NS17):

U

TS-CRYPTO

DECLAS

31 Dec 2007

Physical access to this subassembly is SECRET to TOP SECRET CRYPTO.  The computer can be SECRET to TOP SECRET-CRYPTO and requires special handling as outlined in USSTRATCOM SD 501-12 when the memory contains MM codes/SIOP data.
 
  • (1) Body Section.

U

S

DECLAS

31 Dec 2007

P/Ns 9214-300001-571 and -581.  Physical access to the body section and many other radiation shielding parts is classified SECRET because the material could be identified and radiation shielding capability determined.
 
  • (2) Gyro-stabilized platform

U

S

DECLAS

31 Dec 2007

P/N 67369-301.  See 3.b.(1)
 
  • (3) Housing, platform

U

S

DECLAS

31 Dec 2007

P/N 69207-201.  See 3.b.(1)
 
  • (4) Gyro compass assembly.

U

C

DECLAS

31 Dec 2007

P/N 67439-301.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument.  Inertial instruments are unclassified when not in operational condition.
 
  • (5) G6B4 gyro.

U

C

DECLAS

31 Dec 2007

P/N 66777-302.  Physical access to inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capabilities of the instrument.
 
  • (6) Wiring harness

U

S

DECLAS

31 Dec 2007

P/N 65541-402.  See 3.b.(1)
 
  • (7) Ring, nutplate

U

S

DECLAS

31 Dec 2007

P/N 68076-201.  See 3.b.(1)
 
  • (8) Cover

U

S

DECLAS

31 Dec 2007

P/N 68081-201.  See 3.b.(1)
 
  • (9) Nut, special

U

S

DECLAS

31 Dec 2007

P/N 69737-201.  See 3.b.(1)
 
  • (10) PIGA

U

C

DECLAS

31 Dec 2007

P/N 102500.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition.
 
  • (11) Computer, missile D37C

U

TS-CRYPTO

DECLAS

31 Dec 2007

P/N 55032-106.  Classification is dependent upon information contained in the memory.  Special handling required as outlined in USSTRATCOM SD 501-12 , Vol I when unit contains MM codes/SIOP data.
 
  • (12) Memory subsystem, computer.

U

TS-CRYPTO

DECLAS

31 Dec 2007

P/N 64128-501.  Classification is dependent upon information contained in the memory.  Special handling required as described in 3.b.(11).
 
  • (13) Memory Disk

U

TS-CRYPTO

DECLAS

31 Dec 2007

P/N 55713-304.  Classification is dependent upon information contained in the memory.  Special handling required as described in 3.b.(11)
 
  • (14) Cover, guidance loose equipment

U

S

DECLAS

31 Dec 2007

P/Ns 8541-303378 and 8541-303380.  See 3.b.(1)
 
  • (15) Window shield

U

S

DECLAS

31 Dec 2007

P/N 69437-201.  See 3.b.(1).
 
  • (16) GI-TI-B gyro

U

C

DECLAS

31 Dec 2007

P/N 78170.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the  instrument. Inertial instruments are unclassified when not in operational condition.
  c. MGS (NS20):

U

S

to

TS-CRYPTO

DECLAS

31 Dec 2007 

Physical access to this subassembly is SECRET to TOP SECRET-CRYPTO depending on what information is in the computer memory.  The computer/NS-20 requires special handling outlined in USSTRATCOM SD 501-12 when it contains MM codes/SIOP data.
 
  • (1) Gyro compass assembly

U

C

DECLAS

31 Dec 2007

P/N 67776-301.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition.
 
  • (2) G6B4 gyro

U

C

DECLAS

31 Dec 2007

P/N 66777-302. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition.
 
  • (3) Gyro-stabilized platform

U

C

DECLAS

31 Dec 2007

P/Ns 68110-301 and 968110-301.  See 3.c.(4) below
 
  • (4) Housing, stable platform

U

S

DECLAS

31 Dec 2007

P/Ns 70752-201 and 68160-301.  Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined.
 
  • (5) Housing assembly platform, upper

U

S

DECLAS

31 Dec 2007

P/N 70754-201.  See 3.c.(4).
 
  • (6) Cover, platform, lower.

U

S

DECLAS

31 Dec 2007

P/N 70768-201.  See 3.c.(4).
 
  • (7) Cover, platform, upper

U

S

DECLAS

31 Dec 2007

P/N 70771-201.  See 3.c.(4).
 
  • (8) GI-TI-B gyro

U

C

DECLAS

31 Dec 2007

P/N 78170.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition.
 
  • (9) PIGA

U

C

DECLAS

31 Dec 2007

P/N 102500.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition.
 
  • (10) Cover, MGS Control (MGSC), lower

U

S

DECLAS

31 Dec 2007

P/N 70602-201.  See 3.c.(4).
 
  • (11) Cover, MGSC, upper

U

S

DECLAS

31 Dec 2007

P/N 70603-201.  See 3.c.(4).
 
  • (12) Computer, D37D

U

S to

TS-CRYPTO

DECLAS

31 Dec 2007 

P/N 55035-106.  Classification is dependent upon information contained in the memory.  Special handling required as directed by USSTRATCOM SD 501-12 Vol I, when unit contains MM codes/SIOP data.
 
  • (13) Memory, Computer

U

S to

TS-CRYPTO

DECLAS

31 Dec 2007 
 

P/N 31200-501.  Classification is dependent upon information contained in the memory.  Special handling required as noted in 3.c.(12).
 
  • (14) Memory Disk

U

S to

TS-CRYPTO

DECLAS

31 Dec 2007

P/N 56213-304.  Classification is dependent upon information contained in the memory.  Special handling required as noted in 3.c.(12).
 
  • (15) Cover, computer, upper

U

S

DECLAS

31 Dec 2007

P/N 70601-201.  See 3.c.(4)
 
  • (16) Cover, computer, lower

U

S

DECLAS

31 Dec 2007

P/N 70800-201.  See 3.c.(4).
 
  • (17) P92 amplifier assembly

U

S

DECLAS

31 Dec 2007

P/N 25343-102.  See 3.c.(4).
 
  • (18) Cover assembly, amplifier

U

S

DECLAS

31 Dec 2007

P/Ns 70589-201 and 56973-501.  See 3.c.(4).
 
  • (19) Mount, P92

U

S

DECLAS

31 Dec 2007

P/N 57940-507.  See 3.c.(4).
 
  • (20) Cover, transient detector, upper

U

S

DECLAS

31 Dec 2007

P/N 70814-507.  See 3.c.(4).
 
  • (21) Cover, transient detector, lower

U

S

DECLAS

31 Dec 2007

P/N 70815-507.  See 3.c.(4).
 
  • (22) Housing platform cover

U

U

P/N 8537-404223.
  d. MGS (NS50):

U

S

1.5.g (X2)

Physical access to this subassembly is either SECRET to TOP SECRET-CRYPTO depending on what information is in the computer memory.  The MGS requires special handling outlined in ACCR 55-56 when the computer (MGC) contains MM codes/SIOP data.
 
  • (1) Gyro-stabilized platform

U

S

1.5.g (X2)

P/Ns 13400-301 and 968110-301.  See 3.c.(4).
 
  • (2) Gyro compass assembly

U

C

1.5.g (X2)

P/N34108700.  Physical access to the inertial instruments in classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument.  Instruments are unclassified when not in operational condition.
 
  • (3) G6B4 gyro

U

C

1.5.g (X2)

P/N 66777-302. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. 
 
  • (4) Housing, stable platform

U

S

1.5.g (X2)

P/Ns 70752-201 and 68160-301.  Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined. 
 
  • (5) Housing assembly platform, upper

U

S

1.5.g (X2)

P/N 70754-201.  See 3.c.(4).
 
  • (6) Cover, platform, lower

U

S

1.5.g (X2)

P/N 70768-201.  See 3.c.(4).
 
  • (7) Cover, platform, upper

U

S

1.5.g (X2)

P/N 70771-201.  See 3.c.(4).
 
  • (8) GI-TI-B gyro

U

C

1.5.g (X2)

P/N 78170.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument.  Instruments are unclassified when not in operational condition.
 
  • (9) PIGA

U

C

1.5.g (X2)

P/N 102500.  Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. 
 
  • (10) Computer, MGC

U

S

15.g (X2)

P/N BG9761B.  The MGC is classified because of the shield within the MGC.  (P/N 11777-403, 11778-403 & 11779-403) and memory contents.  The memory becomes unclassified when all power (flight battery and SRAM battery) is removed.  See 3.c.(4).
 
  • (11) Baffle-IMU aft, assembly

U

U

P/N 8537-404223.
 
  • (12) P/N 11723-403, Shield, Connector, 23 Shell Size

U

S

1.5.g (X2)

Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined.
 
  • (13) P/N 11724-403, Shield, Bottom-MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (14) P/N 11725-403, Shield, Mounting - MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (15) P/N 11726-403, Shield, Mounting MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (16) P/N 11727-403, Shield, Connector, MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (17) P/N 11728-403, Shield, Filter, MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (18) P/N 11729-403, Shield, Top, MGSC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (19) P/N 11731-403, Shield, Bottom, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (20) P/N 11732-403, Shield, Top, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (21) P/N 11733-403, Shield, Coolant, Left, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (22) P/N 11734-403, Shield, Access, Cover, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (23) P/N 11735-403, Shield Connector, Plug, KMC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (24) P/N 11736-403, Shield, Connector, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (25) P/N 11737-403, Shield, Coolant, Right, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (26) P/N 11739-403, Shirt, Boot - 11 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (27) P/N 11740-403, Skirt, Boot - 21 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (28) /N 11741-403, Skirt, Boot - 23 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (29) P/N 11742-403, Skirt, Boot - 25 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (30) P/N 11744-403, Shield, Spacer, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (31) P/N 11753-403, Wrap, Boot - 21 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (32) P/N 11752-403, Wrap, Boot - 21 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (33) P/N 11753-403, Wrap, Boot, - 23 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (34) P/N 11754-403, Wrap, Boot - 25 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (35) P/N 11755-403, J13, Wrap, Boot - 25 Shell Size

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (36) P/N 11756-403, J13 Wrap, Boot - 23 Shell Size, 45 degrees

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (37) P/N 11777-403, Shield, Top, CNN, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (38) P/N 11778-403, Shield, Bottom, CMM, MGC

U

S

1.5.g (X2)

See 3.e.(12)
 
  • (39) P/N 11779-403, Shield, Pins, CMM, MGC

U

S

1.5.g (X2)

See 3.e.(12)
  e.   Classified Economic Order Quantity (EOQ) items for NS10 and/or NS17 and/or NS20 and/or NS50:      
 
  • (1) Baffle, flange-N

U

S

DECLAS

31 Dec 2007

P/Ns 57780-507 and 57778-507.  Physical access is classified SECRET because the shielding material could be identified and radiation shielding capability determined.
 
  • (2) Baffle, insulate

U

S

DECLAS

31 Dec 2007

P/N 58200-507.  See 3.d.(1).
 
  • (3) Base, activator

U

S

DECLAS

31 Dec 2007

P/N 54722-507  See 3.d.(1).
 
  • (4) Boot, cable assembly.

U

S

DECLAS

31 Dec 2007

P/N 56188-507.  See 3.d.(1).
 
  • (5) Boot, dust and M

U

S

DECLAS

31 Dec 2007

P/N 57970-507.  See 3.d.(1).
 
  • (6) Cable nipple, EL

U

S

DECLAS

31 Dec 2007

P/Ns 57776-507 and 57339-507.  See 3.d.(1).
 
  • (7) Cover, access

U

S

DECLAS

31 Dec 2007

P/Ns 70615-201 and 70605-201.  See 3.d.(1).
 
  • (8) Cover, connector

U

S

DECLAS

31 Dec 2007

P/N 69954-201.  See 3.d.(1).
 
  • (9) Cover, fastener

U

S

DECLAS

31 Dec 2007

P/N 57992-507.  See 3.d.(1).
 
  • (10) Cover, manifold

U

S

DECLAS

31 Dec 2007

P/N 60801-201.  See 3.d.(1).
 
  • (11) Cover, protective

U

S

DECLAS

31 Dec 2007

P/N 57992-507.  See 3.d.(1).
 
  • (12) Cover, shield pin

U

S

DECLAS

31 Dec 2007

P/N 50589-507.  See 3.d.(1).
 
  • (13) Frame, window optical.

U

S

DECLAS

31 Dec 2007

P/N 8541-3003336.  See 3.d.(1).
 
  • (14) Gasket

U

S

DECLAS

31 Dec 2007

P/Ns 57993-507 and 50583-507.  See 3.d.(1).
 
  • (15) Insulation, sleeve

U

S

DECLAS

31 Dec 2007

P/Ns 50575-507 and 50574-507.  See 3.d.(1).
 
  • (16) Nut, special

U

S

DECLAS

31 Dec 2007

P/N 69737-201.  See 3.d.(1).
 
  • (17) Nutplate, ring R

U

S

DECLAS

31 Dec 2007

P/N 60878-201.  See 3.d.(1)
 
  • (18) Pan, electronic

U

S

DECLAS

31 Dec 2007

P/N 57972-507.  See 3.d.(1).
 
  • (19) Plug, counterbore.

U

S

DECLAS

31 Dec 2007

P/N 50582-507.  See 3.d.(1)
 
  • (20) Ring, cover

U

S

DECLAS

31 Dec 2007

P/N 57973-507.  See 3.d.(1).
 
  • (21) Screw, special

U

S

DECLAS

31 Dec 2007

P/N 67A53001P44.  See 3.d.(1).
 
  • (22) Seal, rubber, special

U

S

DECLAS

31 Dec 2007

P/N 57790-507.  See 3.d.(1).
 
  • (23) Shielding assembly

U

S

DECLAS

31 Dec 2007

P/N 483-0224-002.  See 3.d.(1)
 
  • (24) Sleeve, shield R

U

S

DECLAS

31 Dec 2007

P/Ns 50573-507 and 50577-507.  See 3.d.(1).
 
  • (25) Spacer, plate.

U

S

DECLAS

31 Dec 2007

P/N 56191-507.  See 3.d.(1).
 
  • (26) Stud, shouldered

U

S

DECLAS

31 Dec 2007

P/N 57991-507.  See 3.d.(1).
 
  • (27) Trap, egress

U

S

DECLAS

31 Dec 2007

P/N 85075-201.  See 3.d.(1)
 
  • (28) Washer, flat

U

S

DECLAS

31 Dec 2007

P/Ns 57996-507 and 57782-507.  See 3.d.(1).
 
  • (29) Washer, special

U

S

DECLAS

31 Dec 2007

P/Ns 57999-507-1 and 57995-507-1.  See 3.d.(1).
 
  • (30) Window, observation

U

S

DECLAS

31 Dec 2007

P/N 69457-201-3.  See 3.d.(1).
4 RS Subsystem.     See Section V.
5 Warhead subsystems (RV).     See appropriate RV guide
6 Command Data Buffer:      
  a. LCF Processor (LCFP), Fig A 14058 (applies to all drawers associated with LCFP)

U

U or

TS-CRYPTO

(SIOP-ESI)

1.5.c (X1)

LCFP rack UNCLASSIFIED with no drawers installed.  TOP SECRET - CRYPTO with TSEC/KI-22 SDU Fig A 1506 and keying variable.
  b. Programmer group (LF) Fig A 1201 (applies to all associated drawers).

U

U or S

or

TS-CRYPTO

1.5.c (X1)

Rack UNCLASSIFIED with no drawers installed.  SECRET with SDU and test keying variable installed.  TOP-SECRET-CRYPTO with operational keying variable installed.
  c. Digital data terminal (LF) Fig A 14152 (and all associated drawers).

U

U or S

or

TS-CRYPTO

1.5.c (X1)

Initially UNCLASSIFIED.  Special handling required.  SECRET - CONTROLLED COMSEC ITEM with SDU and test keying variable installed.  TOP SECRET-CRYPTO with SDU and operational keying variable installed.
  d. IPD processor drawer CI 17791.

U

U

or

S-CRYPTO

or

TS-CRYPTO

1.5.c (X1)

UNCLASSIFIED when SDU and keying variables are removed.  SECRET - CRYPTO with SDU and operational keying variable installed.  Up to TOP SECRET-CRYPTO with contractor test IPD processor keying variable assembly installed.  All other drawers and units associated are classified and handled the same.
  e. Secure Data Unit (SDU) Fig A 1506.  Transmission Security (TSEC)/KI-22T.  

S

1.5.c (X1)

SECRET Controlled COMSEC Item with no keying variable.  Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved.
  f. SDU Fig A 1506, TSEC/KI-22M

U

S

1.5.c (X1)

SECRET Controlled COMSEC Item with no keying variable.  Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved.
  g. SDU Fig A 1506. TSEC/KI-22

U

S

1.5.c (X1)

SECRET Controlled COMSEC Item with no keying variable.  Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved.
  h. Keying variables:     All keying variables are accountable as separate items when not installed and accountable under the item in which installed.
 
  • (1) Operational permutation plug USKAZ-2/TSEC (P Plug)

U

TS-CRYPTO

1.5.c (X1)

Used with MGS in MM II, III

Information is classified because it could reveal a cryptologic system or activity (XI).

 
  • (2) Operational keying variable, USCAZ-11-12-78/TSEC

U

TS-CRYPTO

-11, -78  -12 WG IV

1.5.c (X1)

Used with SDU, KI-22, Fig A 1506.
 
  • (3) Operational keying variable, USKAZ-77/TSEC

U

S-CRYPTO

1.5.c (X1)

Used with SDU, KI-22M, Fig A 1506 in IPD modem.
 
  • (4) Contractor test IPD modem keying variable assembly, USKTZ-77/TSEC

U

U or

TS-CRYPTO

1.5.c (X1)

Initially UNCLASSIFIED.  Special handling required.  Used with SDU, KI-22M, Fig A 1506 in IPD processor.
 
  • (5) Test P-Plug

U

U

1.5.g (X2)

Controlled COMSEC Item.  Used with MGS in MM II, III.
 
  • (6) USKTZ -11-12 -78/TSEC, HQ AFSPC and contractor test/training HICS keying variable PROM.

U

S

1.5.g (X2)

Controlled COMSEC Item.  SDU Keying Variable PROM.  DECLAS according to applicable COMSEC documents/guidance.
7 Command control auxiliary subsystem:      
  a. Decoder - command signals ground (CSD-G), Fig A 1268.

U

U

 
  b. Decoder - command signals - missile (CSD-M) , Fig A 6752

U

U to

S-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Initially UNCLASSIFIED.  Special handling required.
  c. Panel assembly launch control (Part of Console) Fig A 1243, 1243M

U

U to

S-CRYPTO

1.5.c (X1)

Initially UNCLASSIFIED.  Special handling required.
 
  • (1) Panel assembly launch control, Fig A 14150

U

U to

TS-CRYPTO

1.5.c (X1)

Initially UNCLASSIFIED.  Special handling required.
  d. Secure code unit assembly Mechanical Code Unit (MCU)

U

U to

TS-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Initially UNCLASSIFIED.  Special handling required.
  e. Wing code processing system,

       (WCPS) CI 42156:

U

S

to

TS-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Initially SECRET.  Special handling required.
 
  • (1) Weapon system controller, Fig A 400 (AN-UYK-11) memory drawer:

U

S-CRYPTO

to

TS

(SIOP-ESI)

1.5.c (X1)

Special handling required.
 
  • (a) If unit fails while performing WCPS functions

U

TS-CRYPTO

(SIOP-ESI)

1.5.c (X1)

Until successful overwrite is accomplished.
 
  • (2) Memory controller group, Fig A 14061 (drum drawer only).

U

U to TS

1.5.g (X2)

Initially UNCLASSIFIED.  Special handling required.
  f. Code change verifier CI 05201.

U

U to

TS-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Initially UNCLASSIFIED.  Special handling required.
  g. Launch Enable Panel.

U

U to TS-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Initially UNCLASSIFIED.  Special handling required.
  h. Launch enable control group, Fig A 5034.

U

U to

TS-CRYPTO

1.5.c (X1) &

1.5.g (X2)

Special handling required.
  i. Launch commit key, operational and R&D.

U

U

Keys to panels in operational use will be controlled by at least two military members.
  j. Cartridge tape unit.

U

U or S

1.5.c (X1)

UNCLASSIFIED only in situations such as disassembly where it is visually evident that the two classified printed circuit assemblies interface control module and drive control module have been removed
  k. Amplifier, radio frequency, Fig A 9201.

U

U

R&D only.  When tuned to classified frequency, classification will be the same as that of the frequency to which it is tuned.
  l. Instrumentation group trainer test, guided missile Fig A 6370LW.

U

U

VAFB flight test only.  MM III mod 7.
  m. Instrumentation group trainer test, guided missile Fig A 6380.

U

U

VAFB flight test only.  MM II mod 8
8 LCC Hardware      
  a. Weapon System Processor (WSP) C0032102

U

U

All WSP random access (volatile) memory (RAM) is dissipated when power is removed.  The WSP is therefore UNCLASSIFIED when power is removed.  Special handling required.
  b. Bulk Storage/Loader (BS/L) C0032107

U

U

or

TS- FRD, (SIOP-ESI)

Cat 6

and 10

1.5.g (X2)

The hard disk assembly (HDA) is a removable hard disk.  All weapon system control element (WSCE) executable software and databases are resident on the removable HDA.  HDA becomes UNCLASSIFIED after successful overwrite.  Overwrite procedure complies with CJCSI 3231.01.
  c. Floppy Disk Drive, (FDD) C0032106

U

U

or

TS- FRD, (SIOP-ESI)

Cat 6

and 10,

1.5.g (X2)

Used in the console.  Floppy disk drive does not retain classified information after power is removed.  Diskettes installed in this drive become TOP SECRET - SIOP-ESI, unless the write protect tab is active during upload operations.  If the write protect tab is not active, the information on the diskettes is classified.
  d. Rapid Message Processor (RMP) CI 00200

U

U

All RMP RAM memory is dissipated when power is removed.  The RMP is therefore UNCLASSIFIED when power is removed.
  e. RMP Backup Processor (RMPB) CI 00700

U

U

All RMP Backup RAM memory is dissipated when power is removed.  The RMP backup is therefore UNCLASSIFIED when power is removed.
  f. Operator Input Device (OID) CI 032108

U

U

Keyboard and trackball.  Contains no memory.
  g. Video Display Unit (VDU)  CI 0032104

U

to

TS- FRD, (SIOP-ESI)

Cat 6

and 10

1.5.g (X2)

U

or

TS- FRD, (SIOP-ESI)

Cat 6

and 10

1.5.g (X2)

VDU can display classified information and visual/physical access must be restricted IAW data being displayed.  When turned off, visual/physical access is UNCLASSIFIED.  No data retained in VDU when power is removed.
  h. Printer, CI 0032105

U

or

TS- FRD, (SIOP-ESI)

Cat 6

and 10

1.5.g (X2)

U

or

TS FRD, (SIOP-ESI)

Cat 6

and 10

1.5.g (X2)

Printed material can be classified and visual/physical access to printouts must be restricted IAW classification of printed data.  Visual/physical access to the printer alone is UNCLASSIFIED.  No data is retained in the printer when power is removed.
  i. Coder-Decoder Assembly.  (CDA)

U

U

Provides mounting and power supply for KI-22.  The CDA itself is UNCLASSIFIED and retains no data.
9 Operations Procedures Trainer Hardware      
  a. Airborne Procedures Trainers (APT) Hardware      
 
  • (1) VAX-11/750 Computer (PH), 750XA-AE+

U

U

or

TS

1.5.g (X2)

Classification depends on information contained in the memory.  Becomes UNCLASSIFIED when memory cleared with power off and disk pack removal.
 
  • (2) RA-60 Disk Drive and Disk, RA60-AA+

U

U

or

TS

1.5.g (X2)

Disk packs may contain up to TOP SECRET data including training war plan information.  UNCLASSIFIED when power and disk removed.
 
  • (3) Instructor Terminal, PC 380-AA

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Classification depends on information contained in the memory.  Becomes UNCLASSIFIED when memory cleared with power off and diskette removed.  Diskettes may be classified up to TOP SECRET and contain training execution data.
 
  • (4) Instructor Printer, LA 50 RA+

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Printed material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical to the printer alone is UNCLASSIFIED.  No data is retained in the printer when power is removed.
 
  • (5) Computer System Printer, LA 12-DB

U

U

Used only by the computer operating system
 
  • (6) Demod/Decoder Simulator, 407-50291-()

U

U

 
 
  • (7) MSD/L Simulator, 407-50290-()

U

U

 
 
  • (8) KI-45 Simulator,
  •    407-50295-()

U

U

 
 
  • (9) Volatile Keying Ay Simulator 407-50276-()

U

U

 
 
  • (10) TEMPEST Isolation Filter    Simulator, 407-50280-()

U

U

 
 
  • (11) ALCS Controller Simulator and Expansion Chassis,
  •    407-50281-()

U

U

 
 
  • (12) Virtual Display Unit 407-50301-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

May be classified TOP SECRET when in operation.  UNCLASSIFIED otherwise.  No memory.
 
  • (13) HARDS Printer,
  •    407-50304-()

U

U

Does not process classified information.
 
  • (14) ALCS Printer, 110553-100

U or TS

1.5.g (X2)

U or TS

1.5.g (X2) 

Printer material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical to the printer alone is UNCLASSIFIED.  No data is retained in the printer when power is removed.
 
  • (15) KYX-9A Telephone Simulator, 407-50399-()

U

U

 
  b. Missile Procedures Trainers (MPT) Hardware Wg VI (LE)      
 
  • (1) PDP-11/34 Computer,
  • 2W-C110A-()

U

U or S

1.5.g (X2)

Classification depends on information contained in the memory.  Memory cleared with power off and disk pack removal.
 
  • (2) RL-01 Disk Drive and Disk, RL-01

U

U or S

1.5.g (X2)

Disk packs may contain SECRET data in the form of messages and systems parameters.  UNCLASSIFIED when disk pack is removed.  Declassify upon deactivation of WG VI unless needed for the NMD program.  If needed for NMD, hardware will be reclassified under NMD guidelines.
 
  • 3) VAX-11/751 Computer (LE), 03-1346404-()

U

U or TS

1.5.g (X2)

Classification depends on information contained in the memory.  Becomes UNCLASSIFIED when memory cleared with power removal.
 
  • (4) RA-60 Disk Drive and Disk (LE), RA-60AA

U

U

 
 
  • (5) Instructor Terminal (03-1346408-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Classification depends on information contained in the memory.  UNCLASSIFIED when memory cleared with power off and diskette removed.  Diskettes may be classified TOP SECRET and contain training war plan data.
 
  • (6) Instructor Printer, FX86e 11-1346405-()

U

to

TS

1.5.g (X2)

U

to

TS

1.5.g (X2)

Printed material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical access to the printer alone is UNCLASSIFIED.  No data is retained when power is removed.
 
  • (7) Computer System Printer (LE), 95120016-103

U

U

Used only by computer operating system.
 
  • (8) SACDIN KG-84A Simulator, 25-79508-()

U

U

Panels and switches, no computer functions.
 
  • (9) SACDIN MSU Simulator, 25-79512-()

U

U

Read-only simulator.  Drives retain no data after power removal.
 
  • (10) AFSATCOM KG-38 Simulator, 25-79512-()

U

U

No memory or codes used.
 
  • (11) Signal Data Recorder,
  •                    face="Times" size="2">5106-100-()

U

U

Printed material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical access to the recorder alone is UNCLASSIFIED.  No data is retained when power is removed.
 
  • (12) SACDIN LPU, 1506018G1

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Printed material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical access to the recorder alone is UNCLASSIFIED.  No data is retained when power is removed.
 
  • (13) SACDIN VDU, 2832120-2

U or S

1.5.g (X2)

U or S

1.5.g (X2)

May be classified TOP SECRET when in operation.  UNCLASSIFIED when power off.  No memory.
 
  • (14) SLFCS Demodulator Simulator

U or S

1.5.g (X2)

U or S

1.5.g (X2)

May be classified SECRET when in operation.  UNCLASSIFIED when power off.  No memory.
 
  • (15) LCP Simulator

U

U

Panel and switches.  No computer functions.  No memory.
 
  • (16) LEP Simulator

U

U

Panel and switches.  No computer functions.  No memory.
      (17) Keyboard Printer

 02-563002-5

U to TS

1.5.g (X2)

U to TS

1.5.g (X2)

Printed material may be classified and access to printouts must be restricted IAW classification of printed data.  Visual/physical access to the recorder alone is UNCLASSIFIED.  No data is retained when power is removed.
  c. Missile Procedures Trainer Hardware      
 
  • (1) Trainer Processor Computer (VAX 4000/200), C003143-()

U

U

or

TS

1.5.g (X2)

UNCLASSIFIED when power off because processor memory does not retain data after removal of power.  Processor contains TOP SECRET- data during operation with Removable Storage Element (RSE).
 
  • (2) Hard Disk Removable Storage Element (RSE), C003470-()

U

TS

1.5.g (X2)

RSE hard disk stores the MPT software including the MPTCP, MPTCOP, and EPP/MA database.
 
  • (3) Instructor Tape Drive, C003550-()

U

TS

1.5.g (X2)

Classification of the tape is dependent upon data that is archived to it.
 
  • (4) Audio Controller Computer, C003146-()

U

U

Processor memory does not retain data after removal of power.
 
  • (5) Audio Controller Computer Floppy Disk Drive, C003146-()

U

U

or

TS

1.5.g (X2)

Floppy disk drive does not retain classified information after power is removed.  Floppy diskette remains UNCLASSIFIED if write protect tab is set during upload, otherwise the disketter assumes the highest classification of information in the system.
 
  • (6) Instructor Printer, C003156-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Printouts may be classified and visual/physical access to printout must be restricted IAW classification of printed data.  Visual/physical access to the printer alone is UNCLASSIFIED.  No data is retained after power off.
 
  • (7) Instructor Terminals, C003155-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Visual/physical access must be IAW classification of displayed data.  UNCLASSIFIED after power off, no data is retained.
 
  • (8) Student Monitor VDU, C004998-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Visual/physical access must be IAW classification of displayed data.  UNCLASSIFIED after power off, no data is retained.
 
  • (9) Student VDUs, C005006-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Visual/physical access must be IAW classification of displayed data.  UNCLASSIFIED after power off, no data is retained.
 
  • (10) RMP Backup Simulator, C003163-()

U

U

Panel and switches, no computer functions.
 
  • (11) Bulk Storage/Loader Simulator, C003478-()

U

U

Panel and switches, no computer functions.
 
  • (12) Student Printer, C004973-()

U

or

TS

1.5.g (X2)

U

or

TS

1.5.g (X2)

Printouts may be classified and visual/physical access to printout must be must be restricted IAW classification of printed data.  Visual/physical access to the printer alone is UNCLASSIFIED.  No data is retained after power off
 
  • (13) Weapon System Processor Simulator, C003179-()

U

U

Panel and switches, no computer functions.
 
  • (14) RMP Primary Processor Simulator, C003161-()

U

U

Panel and switches, no computer functions.
 
  • (15) HAC/RMPE Journal Memory Loader (JML), C003161-()

U

U

or

TS

1.5.g (X2)

UNCLASSIFIED after power off.  TOP SECRET  when diskettes are installed in this drive.
 
  • (16) Console Floppy Disk Drive, C004388-()

U

U

or

TS

1.5.g (X2)

UNCLASSIFIED after power off.  Diskettes installed in this drive become TOP SECRET,  unless the write protect tab is active during upload operations.
 
  • (17) Launch Enable Panel Simulator 25-45942-() (RY) 89-1014830-() (LE)

U

U

Panel and switches, no computer functions.
 
  • (18) Launch Control Panel Simulator

U

U

Panel and switches, no computer functions.
 
  • (19) SLFCS Demodulator Simulator

U

or

S

1.5.g (X2)

U

or

S

1.5.g (X2)

May be classified SECRET when in operation.  UNCLASSIFIED when power off and thumbwheel switches normalized.  No memory.
 
  • (20) SACDIN KG-84A Simulator, 25-79508-()

U

U

Panel and switches, no computer functions.
 
  • (21) SACDIN Mass Storage Unit Simulator (8î Floppy Drive), 25-79512-()

U

U

Simulator does not contain read/write head.  Simulator contains optical device to detect presence of diskette.  Drive retains no data after power removal.
 
  • (22) Audio Communications and Discussions

U

U

to

TS 

No attenuation provided by trainer enclosure.  See AFI 31-209
 
  • (23) Trainer Enclosure

U

U

to

TS

DECLAS

31 Dec 2007

TEMPEST:  No attenuation provided by trainer enclosure

 
 

SECTION III 

PROPULSION SUBSYSTEMS 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Complete design for Stages 1, 2, and 3 and the PSRE, not including hardness material associated with control units

U or S

1.5.g (X2)

See Section XIV.
2 Physical characteristics for Stages 1, 2, and 3 and PSRE:

U

 
  a. Weight and mass properties

U

Such as propellant, inert and total weights, center of gravity and moments of inertia.
  b. Component material properties and characteristics, not including hardness materials associated with control units.

U

See Section XIV.
3 Solid propellant

U

Such as formula, density, physical samples (cured or uncured), malfunctioning process or sensitivity to shock or fire.
4 Specific propulsion performance for Stages 1, 2, and 3 and PSRE

U

Such as thrust action time, total or specific impulse, chamber pressure or combustion efficiency.
5 Thrust vector control, attitude control, roll control for Stages 1, 2, 3, and PSRE, not including information on hardness properties.

U

Including actuation program, LITVC, delivered side forces, axial thrust augmentation or attitude control forces.  See Section XIV.
6 Maintenance, repair and overhaul data and handbooks for Stages 1, 2, and 3, and PSRE.

U

 
7 Manufacturing process, tooling and gauges for Stages 1, 2, and 3, and PSRE.

U

 
8 Reliability of Stages 1, 2, and 3, and PSRE.

U to S

1.5.g (X2)

UNCLASSIFIED unless the component (motor or PSRE) reliability is less than the propulsion subsystem reliability specification.  CONFIDENTIAL if the component reliability is less than propulsion subsystem specification but greater than the system countdown and flight specification.  SECRET if the component reliability is less than the system countdown and flight specification.
9 Vulnerability of Stages 1, 2, and 3, and PSRE to countermeasures.

S

1.5.g (X2)

Hardness vulnerability, See Section XIV.

 

SECTION IV 

MISSILE GUIDANCE SET (MGS) SUBSYSTEM 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Detailed design of complete subsystem

S

1.5.g (X2)

Hardness vulnerability see Section XIV.
2 Specific performance of subsystem components and assemblies if such information reveals missile or subsystem operational capability or accuracy.

S

1.5.g (X2)

See Section IV.  For hardness vulnerability see Section XIV.
  a. G6B4 gyroscope

C to S

1.5.g (X2)

G6B4 performance data by itself is considered CONFIDENTIAL.  If associated with other inertial instruments it is  considered SECRET.  Data in EMDAS and MM Repair and Evaluation Data (RED) B portion of GO 78 is UNCLASSIFIED.
  b. 16 PIGA MOD G accelerometer

C to S

1.5.g (X2)

16 PIGA MOD G performance data by itself is considered CONFIDENTIAL.  If associated with other inertial instruments it is  considered SECRET.  Data in EMDAS and MM REDB is UNCLASSIFIED.
  c. GI-TI-B gyroscope

C to S

1.5.g (X2)

GI-TI-B performance data by itself is considered CONFIDENTIAL.  If associated with other inertial instruments it is considered SECRET.  Data in EMDAS and MM REDB is UNCLASSIFIED.
  d. Subsystem data available at repair depots    
 
  • (1) GCA/OER/Align Set performance data

U

 
 
  • (2) PIGA DMGE printouts

U

 
 
  • (3) G6B4 Gyro (Gyro F Station and Gyro Test Station) DMGE printouts

U

 
 
  • (4) GI-T1-B Gyro Test Station Data

U

 
 
  • (5) NS20 D37 data and NS50 MGC data remaining after overwrite

U to S

1.5.g (X2)

D37 hot channel data extracted prior to Overwrite is classified in accordance with other portions of this guide.  Some classified data remains in the computer memory after Overwrite, and the D37 Hot Channel Protection Test or Mode 153.  Data printed out by the depot configured software thereafter is unclassified.
 
  • (6) MGSC & Module data

U

 
 
  • (7) MGS/GSP & GCA Final Acceptance test print from system level test

U

 
3 Reliability (NS-17, NS-20, NS-50)    
  a. MGS (NS-17, NS-20 and NS-50).

U or S

1.5.g (X2)

In-flight reliability of the MGS and its components is SECRET.
  b. Components (Computer, GSP, MGSC, P92A3 downstage amplifier and downstage flight controls).

U or S

1.5.g (X2)

See 3a comments.
  c. Assemblies (D37 memory, G6B4 gyroscope, 16 PIGA Mod G accelerometer, GI-TI-B gyroscope).

U or S

1.5.g (X2)

See 3a comments.
  d. Subassemblies (Integrated circuits, and other related electronics).

U or S

1.5.g (X2)

See 3a comments

 
 

SECTION V 

REENTRY SYSTEMS (RS) 

The national policy on nuclear weapons dictates that only limited information will be released.  Specifically no authority exists to divulge, confirm or deny the location at which special weapons are positioned, wherever they are positioned.  No questions will be answered regarding the employment of nuclear weapons in a particular situation.  The reply to questions on authority to employ nuclear weapons will be authorized by the President.  In reply to inquiries, use of the terms thermonuclear and hydrogen should not be used; atomic and nuclear should be avoided.  Replies should be phrased in such a way that they cannot be misconstrued as gratuitous official pronouncements.  Any unnecessary statements concerning US nuclear-capable deterrent forces should be restrained.  In accordance with established policy, the US does not discuss the arms carried by specific aircraft, vessels or other elements of its military forces and avoids drawing attention to the need for conducting continuous military operations with nuclear weapons.  Certain US weapons systems have been publicly identified as having a nuclear capability.  This identification does not in itself provide authority to release information concerning details of storage, handling, or transportation of nuclear weapons or components. 

Except where noted, the following guidance applies, as applicable, to both MM II and MM III. 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 RVs:

U to

TS-RD-CNWDI

1.5.g (X2)

See RV guides.
  a. Association of an operational RS/RV with its nuclear warhead    
  b. Fact that W56, W62, and/or W78 are thermonuclear weapons    
  c. Warhead unit cost   See RV guides
  d. RV performance   See RV guides and Sections X and XIV
  e. Warhead yields   See RV guides and Sections X and XIV
  f. Target analysis studies   See RV guides and Sections X and XIV
  g. Height of Burst (HOB). Operational or test.    
 
  • (1)  HOB
  See RV guides and Sections X and XIV
 
  • (2)  Deviation in HOB
  See RV guides and Sections X and XIV
  h. Any other RV (warhead) information characteristics or performance   See RV guides and Sections X and XIV
       
2 Pen Aid systems:    
  a. MM II   See Section XVII.
  b. MM III    
  c. Hardening of Pen Aid systems.   See Section XIV, XVII, and XVIII.
3. RS:    
  a. Administrative Information:    
 
  • (1) Association or cross-association of the terms MM III, MK12, MK12A, MIRV, PBV, PSRE, PBCS, Pen Aids, Chaff, Dipoles, MK12 RS, MK 12A RS, 3 RVs

U

 
 
  • (2) Total RS quantities to be produced excluding RVs:
   
 
  • (a) To support the Force structure.

U

 
 
  • (b) To support any other Force structure.

C

1.5.g (X2)

 
 
  • (3) RV production quantities
  See RV guides.
 
  • (4) Development, planning or production schedules which reveal numbers of the RSs intended for operational use.

S-FRD

1.5.g (X2)

See subparagraph 3.a.(2) above.
 
  • (5) Planned or actual rates delivery of RSs to any operational site

S-FRD

1.5.g (X2)

For additional information regarding Pen Aids, see Sections XVII and XVIII.
 
  • (6) Total number of RSs  produced or delivered for operational use as of a specific date.

S-FRD

1.5.g (X2)

 
 
  • (7) Association of RS or RS components with nuclear test events or event names.

U

or C-FRD

or S-FRD

1.5.g (X2)

SECRET-FRD when W78 is identified as event source.  CONFIDENTIAL-FRD is unannounced event is revealed.  UNCLASSIFIED if W78 is not identified as the event source and only a planned or announced event is revealed.
 
  • (8) When missile system, RV or component thereof, is exposed to an unspecified effect

U

IAW TCG-WT-1 and TCG-WT-5
 
  • (9) Association of an RS, as a whole, with the Department of Energy (DOE), or the Energy Research and Development Agency (ERDA)

U

 
 
  • (10) RS Fig A end item listing, including names.

U

 
 
  • (11) Any RS cost except for W56, W62 or W78.

U

Except RV cost.  See MK12 and MK12A guides.
  b. Capability or performance information, actual or predicted:   See Section X, XVII, and XVIII.
 
  • (1) Accuracy:
   
 
  • (a) Of RS subsystem without RV data

S

1.5.g (X2)

 
 
  • (b) Of RS combined with RV data.

S-FRD

1.5.g (X2)

 
 
  • (c) RS contribution to CEP.

S

1.5.g (X2)

 
 
  • (d) RV contribution to CEP.
  See RV guides
 
  • (e) Total weapon system CEP.

S-FRD

1.5.g (X2)

 
 
  • (f) Of Pen Aid system

S

1.5.g (X2)

See Sections XVII and XVIII
 
  • (2) Reliability:
   
 
  • (a) RS without RV data

S

1.5.g (X2)

 
 
  • (b) RS including RV data
  See RV guides
 
  • (3) Maximum number of:
   
 
  • (a) Chaff dispensers

U

See Sections XVII and XVIII
 
  • (b) Chaff clouds per dispenser

S

1.5.g (X2)

 
 
  • (c) Chaff clouds

S

1.5.g (X2)

 
 
  • (d) RVs that can be carried on Operational Missiles

U

 
 
  • (4) Impacts and scoring
  See Section X item 4.h. and RV guides.
 
  • (5) Maximum or minimum range of Pen Aid system

S

1.5.g (X2)

 
  c. Physical properties    
 
  • (1) Visual Access:
  Whether in person or via photos, drawings or sketches.
 
  • (a) RS with shroud installed

U

 
 
  • (b) RS with shroud removed:

U

 
 
    • 1. Without RVs or Pen Aids

U

 
 
    • 2. With RVs but without Pen Aids.
   
 
    • a. If RV nozzle cant angles are visible or can be determined.
  See RV guides
 
    • b. If RV nozzle cant angles are not visible and cannot be determined (for example, an absolute silhouette photo of an RV or RS).

U

Unclassified models, drawings, sketches, etc., shall not be made except for specific official requirements.  Public release or display of unclassified photographs, etc., is not authorized.  See RV guides.
 
    • 3. With Pen Aids but without RVs.

U to S

1.5.g (X2)

See item 3.c.(3)(c) below.
 
    • 4. With RVs and Pen Aids

U to

S-FRD

1.5.g (X2)

Use the most restrictive single or combined applicable guidance from 3c(1)(b)1. thru 3. above.
 
  • (c) RVs:
   
 
    • 1. Fully assembled
  See RV guides
 
    • 2. Partially disassembled
  See RV guides
 
  • (2) Weights:
   
 
  • (a) Total or effective lift-off weight of any RS configuration.

S-FRD

1.5.g (X2)

 
 
  • (b) RV weights or weight tolerances.
  See RV guides
 
  • (c) Other RV properties
  See RV guides
 
  • (d) Shroud

U

 
 
  • (e) Deployment module

U

 
 
  • (f) Pen Aid weights

U to S

1.5.g (X2)

See Sections XVII and XVIII.
 
  • (3) Hardware classification:
   
 
  • (a) Deployment module (MM III):
   
 
    • 1. Complete RS

S-RD

CNWDI

1.5.g (X2)

 
 
    • 2. Shroud

U

 
 
    • 3. Support Structure

U

 
 
    • a. Bulkhead

U

 
 
    • b. Decoder

U

 
 
    • c. Arm and disarm device.

U

 
 
    • d. RS programmer

U

 
 
    • e. Cabling and harness

U

 
 
    • f. Environment Sensing Signal Generator (ESSG)

C-FRD

1.5.g (X2)

MK12A RS
 
    • 4. Payload attachment kit

U

 
 
    • 5. Interface cabling set.

U

 
 
  • (b) RVs:
   
 
    • 1. Visual access
  See RV guides
 
    • 2. Physical access
  See RV guides
 
  • (c) Pen Aids:
   
 
    • 1. Visual access

U to S

1.5.g (X2)

See Sections XVII and XVIII.
 
    • 2. Physical access

S

1.5.g (X2)

See Sections XVII and XVIII.
  d. Design Details:    
 
  • (1) Shroud

U

 
 
  • (2) Telemetry and transponder systems
  For RV telemetry, see RV guides.  For Mod 7/8 see Section X.
 
  • (3) Complete design specifications, significant operating details, performance, frequencies of operation, or reliability.

U to

S-FRD

1.5.g (X2)

Refer to applicable subsections of this Guide and the appropriate RV guide.
 
  • (4) Manufacturing process or operating techniques which represent a significant advance in the state of the art and which are developed specifically for any RS:
   
 
  • (a) R&D related

S

to

S-RD

1.5.g (X2)

Refer to applicable subsections of this Guide and the appropriate RV guide.  May be FRD or RD depending upon information revealed.
 
  • (b) Other

U to

S-FRD

1.5.g (X2)

Refer to applicable subsections of this Guide and the appropriate RV guide.
 
  • (5) R&D studies which include theoretical calculations or experimental data relating specifically to RS performance design problems or advanced design concepts.

U to

S-FRD

1.5.g (X2)

Refer to applicable subsections of this Guide and the appropriate RV guide.
 
  • (6) Initial Operational Capability (IOC) dates.

U to C-FRD

1.5.g (X2)

UNCLASSIFIED when IOC date has been officially released.  CONFIDENTIAL-FRD for MK12A until IOC date has been released by DOD.
 
  • (7) R&D studies, design specifications, operating details, performance, etc., relating to MK12A RV.

C-FRD

1.5.g (X2)

See this Guide and MK12A Guide
 
  • (8) RV information
  See RV guides
 
  • (a) Fact that the MK12 RV is a high beta RV
  See RV guides
 
  • (b) Actual beta value (ballistic coefficient).
  See RV guides
 
  • (c) RV spin rate
  See RV guides
 
  • (d) RV vulnerability to countermeasures:
  See RV guides
 
    • 1. If vulnerability sure kill.
  See RV guides
 
  • (9) Separation subsystems:
   
 
  • (a) Design details.

U

 
 
  • (b) Reliability.

S

to

TS-FRD

1.5.g (X2)

Refer to applicable subsections of this Guide and the appropriate RV guide.
 
  • (10) RV spin subsystem.
  See RV guides.
  e. Operational data:    
 
  • (1) RS configuration code:
   
 
  • (a) Definition of code.

U

 
 
  • (b) Code with no explanation

U

 
 
  • (2) Number of RVs on an operational missile in any given LF

S-FRD

1.5.g (X2)

 
 
  • (3) Number of RVs on operational test launch missiles.

U

Except for special missions.
 
  • (4) The fact of presence, or lack thereof, of Pen Aids on any operational missile.

U or S

1.5.g (X2)

The number and/or location of operational missiles with pen aids for more than one wing or 150 missiles is classified SECRET.
   f. PBV flight data predicted or actual at any time after Stage 3 thrust termination:   NOTE:  If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DOM approval for release or dissemination is required.
 
  • (1) Trajectory information:

U to

S-FRD

1.5.g (X2)

Real time radar and telemetry data measured and recorded by test range instrumentation is UNCLASSIFIED until processed.  When such data is subsequently processed or analyzed, it will be classified IAW the provisions of this Guide.  Specifically, all MM booster trajectory data up to thrust termination is UNCLASSIFIED.  For classification of data after thrust termination, refer to the appropriate RV guide.  Post launch analysis and trajectory reconstruction will be classified SECRET-FRD if precise target location, World Geodetic System (WGS), coordinates are derived and/or depicted.  Analysis of abnormal/anomalous trajectory will be classified IAW this Guide.
 
  • (a) Altitude

S-FRD

1.5.g (X2)

See RV guides.
 
  • (b) Velocity, RV or RS

S-FRD

1.5.g (X2)

See RV guides.
 
  • (c) Velocity vector, RV or RS

S-FRD

1.5.g (X2)

See RV guides.
 
  • (d) Velocity/altitude profiles

S-FRD

1.5.g (X2)

See RV guides.
 
  • (e) Attitude
  See RV guides.
 
    • 1. During a DAG (Deployment Attitude Guidance).

S-FRD

1.5.g (X2)

See RV guides.
 
    • 2. At time of RV deployment

S-FRD

1.5.g (X2)

See RV guides.
 
    • 3. During lateral translation

U

 
 
    • 4. During Pen Aid Deployment

S

U

1.5.g (X2)

See RV guides.
 
  • (2) Deployment geometry:
   
 
  • (a) Number of objects in a reentry train

S

1.5.g (X2)

 
 
  • (b) RV in-flight distances or spacing, with or without Pen Aids cover.

S-FRD

1.5.g (X2)

See RV guides.
 
  • (c) Location of RV in a reentry train

S-FRD

1.5.g (X2)

See RV guides.
 
  • (d) Separation distance or spacing of any objects in the reentry train.

S-FRD

1.5.g (X2)

See RV guides
 
  • (e) Separation distance between distinct trains.

S-FRD

1.5.g (X2)

See RV guides
 
  • (3) Event timing:
   
 
  • (a) Shroud separation

U

 
 
  • (b) Pen Aid deployment

S

1.5.g (X2)

 
 
  • (c) RV deployment

S-FRD

1.5.g (X2)

See RV guides
 
  • (d) All RV internal events

S-FRD

1.5.g (X2)

See RV guides
 
  • (4) Signature characteristics:
   
 
  • (a) Non-Pen Aid flight
  See RV guided
 
  • (b) Pen Aid flight
  See RV guides
 
    • 1. If no information concerning RV discrimination is revealed.

S-FRD

1.5.g (X2)

See RV guides
 
    • 2. If any RV discrimination is revealed.

TS-FRD

1.5.g (X2)

See RV guides
 
  • (c) Radar fuze frequency

C-FRD

1.5.g (X2)

See RV guides
 
  • (d) Radar cross section.

S-FRD

1.5.g (X2)

See RV guides
 
  • (e) Optical emanations

S-FRD

1.5.g (X2)

See RV guides
  (5) Exoatmospheric point mass.

S

1.5.g (X2)

 

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION VI 

IMPROVED MINUTEMAN PHYSICAL SECURITY SYSTEM (IMPSS)

SECURITY AUXILIARY SYSTEM 
 

Unclassified information that pertains to security measures, including plans, procedures and equipment, for the physical protection of Special Nuclear Material (SNM) where unauthorized dissemination could have a significant adverse effect on public safety, the common defense and security due to illegal production of nuclear weapons, or the theft, diversion or sabotage of SNM should be considered for protection as DOD UCNI.  Material originated prior to dissemination of DOD UCNI interim procedures that is found in the normal course of business to contain UCNI will be protected as UCNI.  There is no requirement to conduct detailed files searches to retroactively identify UCNI.  However, as unclassified information pertaining to the physical protection of SNM is withdrawn from file, it should be reviewed to determine if it meets the criteria for protection as UCNI (and marked accordingly). 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Complete design of the security subsystem

U or S

1.5.g (X2)

The hardware design is UNCLASSIFIED.  Complete software design is SECRET.  The secret aspects of the software design are:  The outer zone (OZ) amplitude and phase alarm threshold constants; The OZ time of integration constants; the inner zone (IZ) amplitude alarm threshold constants; and, the IZ time of integration constants.  Other software components are UNCLASSIFIED.
2 Schematic drawings or manufacturing drawings:

U or S

1.5.g (X2)

SECRET if the system/subsystem probability of detection for a human intruder using any penetration mode or technique is revealed or can be deduced.  SECRET if a system/subsystem vulnerability is revealed or can be deduced.  The OZ subsystem outer and inner range gate size is UNCLASSIFIED if no probability of detection information is revealed.
  a. R&D analyses/tradeoff studies

U

 
3 Reliability data

U

 
4 False/nuisance alarm rate data

U

 
  a. R&D analyses/tradeoff studies

U

 
5 Maintenance requirements and procedures

U or S

1.5.g (X2)

See Item 2. remarks.
6 Subsystem vulnerability:

S

1.5.g (X2)

Any information that reveals a system vulnerability is SECRET.
  a. Detection limitation.

S

1.5.g (X2)

See Item 2. remarks.
  b. Possible methods of degrading system performance that would not be identified by the Nuclear Safety Certification or system self check

S

1.5.g (X2)

SECRET if the plots or patterns of system detection sensitivity are drawn to scale and are labeled with probability of detection information. Plots or patterns of area of coverage with no information relative to system probability of detection are UNCLASSIFIED.
7 Plots or patterns of security system area of coverage with respect to actual or simulated human penetration

U or S

1.5.g (X2)

See Item 6.b. remarks
8 Transmitter frequency.

U

 
9 Power output.

U

 
10 Signal processing techniques.

1.5.g (X2)

SECRET when system sensitivity can be deduced.  The signal processing techniques are SECRET if they reveal or introduce a subsystem vulnerability (i.e., the differential side-band processing technique is UNCLASSIFIED).
  a. R&D analyses/tradeoff studies

U

 
11 False/nuisance alarm event.

U

 
12 Subsystem life.

U

 
13 Complete listing of operational subsystem software.

S

1.5.g (X2)

See Item 1. remarks.
14 Partial listing of the operational subsystem software.

U or S

1.5.g (X2)

See Item 1. and 2. remarks.
15 Development of test software.

U or S

1.5.g (X2)

See Item 2. remarks.
16 Test results and analysis 

a. Raw test data not relating to potential system design/performance

S -  U

1.5.g (X2)

Classified related to detection thresholds, patterns, or vulnerabilities.  If not related to the above, UNCLASSIFIED.  Unclassified if not related to detection thresholds, patterns or vulnerabilities.
17 OZ filter integration times.

S

1.5.g (X2)

See Item 1. remarks
18 IZ integration time.

S

1.5.g (X2)

See Item 1. remarks.
19 Military application

U

 
20 Latch-up time

U

 
  a. R&D analyses/tradeoff studies

U

 
21 Reset time

U

 
22 Circuit design thresholds for alarm

S

1.5.g (X2)

 
23 Frequency of drawer self check.

U

 
24 System probability of detection.

S

1.5.g (X2)

 
25 Detection limitations relative to target velocity.

S

1.5.g (X2)

The detection limitations relative to target velocity are SECRET if they reveal or introduce a subsystem vulnerability.
26 Physical security system hardware    
  (1) Receiver Transmitter alarm set P/N 25-90426-1, -3 (CI 1514AA)

U or S

1.5.g (X2)

Visual access UNCLASSIFIED.  Review security measures for possible protection as UNCI.  Receiver transmitter alarm set drawer is SECRET when processor P/N 21-61925 with PROMS P/N 21-61699-33, 34, 35, 36, or 38, 39, 40,41 are installed. If PROMS are not installed, the processor card and drawer are UNCLASSIFIED
  (a) Circuit card assembly processor, A2 P/N 21-61699-5

U or S

1.5.g (X2)

Visual access UNCLASSIFIED. Physical access SECRET when PROMS P/N 21-61699-33, 34, 35, 36, or 38, 39, 40, 41 are installed. If PROMS are removed the A2 circuit card is UNCLASSIFIED
  1. Programmable Read Only Memory (PROM) anti-intrusion alarm set operational software (CI 1516AA).

S

1.5.g (X2)

P/Ns 21-61699-33, 34, 35, 36.
  (2) Antenna assembly, (C1015151AA)

U

P/N 25-799-50-4
27 Development or production hardware.

U or S

1.5.g (X2)

Any development hardware or firmware that functionally or electrically represents the system baseline design, or production hardware or firmware that, when analyzed, reveals detection sensitivity or reveals a system/subsystem vulnerability is SECRET. The external view of any hardware is UNCLASSIFIED.

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION VII 

LAUNCH FACILITY PERSONNEL ACCESS AUXILIARY SYSTEM 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Design criteria

S

1.5.g (X2)

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.  Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET.
2 Specifications.

U

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.  Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET.
3 Schematic diagrams:    
  a. Entire security and alarm system, secondary door and security pit vault door circuits.

S

1.5.g (X2)

 
  b. Individual end items.

U

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.  Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET.
4 Design information:    
  a. Penetration resistance.

S

1.5.g (X2)

 
  b. Time configuration.

S

1.5.g (X2)

 
  c. External configuration

U

 
  d. Internal details.

S

1.5.g (X2)

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.
5 Maintenance and operating requirements and procedures.

S

1.5.g (X2)

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.
6 Drawings:    
  a. System.

S

1.5.g (X2)

Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET.
  b. Manufacturing.

S

1.5.g (X2)

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.
7 Total quantities.

U

TO 21M-LGM30F-2-19 contains unclassified procedures.  Applicable classified data is contained in TO 21M-LGM30F-4-1-2.
8 Reliability.

U

 
9 Hardware    
  a. Security pit vault door (Fig A 1608).    
 
  • (1) As an integral part of the site security system.

S

1.5.g (X2)

 
 
  • (2) When separated from an operational LF.

U

Provided the combination has been removed and IZ alarm switch loops are disconnected.
 
  • (3) Forced-entry template.

U

 
 
  • (4) Forced-entry door.

U

Provided the combination has been removed and IZ alarm switch loops are disconnected.
  b. Secondary door (Fig A 1604):    
 
  • (1) As an integral part of the site security system.

S

1.5.g (X2)

 
 
  • (2) When separated from an operational LF.

U

Provided the combination has been removed and IZ alarm switch loops are disconnected.

 
 
 

SECTION VIII 

AIRBORNE LAUNCH CONTROL SYSTEM (ALCS)

AUXILIARY SYSTEM 

Also see Worldwide Airborne Command Post System (WWABNCP) Security Classification Guide. 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 That an ALCS is being used.

U

 
2 Design and performance characteristics

U

UNCLASSIFIED unless information regarding the cryptologic is revealed. COMSEC Controlled Item.
  a. If information regarding the crypto logic is revealed.

S-CRYPTO

1.5.g (X2)

COMSEC Controlled Item.
3 Overall force hardness and survivability resulting from ALCS.

TS-FRD

1.5.g (X2)

 
4 Method of operation of control unit and groups (Stations 1, 2, and 3).

U

 
5 Operational ALCC-Wing data frequencies.

U

 
6 ALCS codes:   Also see USSTRATCOM SD 501-12
  a. Operational launch codes:    
 
  • (1) Encrypted

U

 
 
  • (2) Clear text

TS-CRYPTO

1.5.c (X1)

 
  b. Test codes:    
 
  • (1) Launch

U

 
 
  • (2) Keying

S-CRYPTO

1.5.c (X1)

 
7 ALCS auxiliary system:    
  a. Code Processor Equipment

 Fig A 1990, TSEC/K1-45

U to

TS-CRYPTO

1.5.c (X1)

Visual access UNCLASSIFIED.  S to TS-CRYPTO Controlled COMSEC Item TOP SECRET-CRYPTO with operational cryptovariable installed.  Special control handling, and classification required.  DECLAS according to applicable COMSEC document/guidance
  b. KIK-45/TSEC Volatile keying assembly

U

to

S

1.5.c (X1)

Visual access UNCLASSIFIED.  Controlled COMSEC Item.  One KIK-45 holds half the KI-45 key.  Used with USKAU/USKMU.  TOP SECRET - CRYPTO with operational codes installed DECLAS according to applicable COMSEC documents/guidance.
  c. USKAU -100 A/B keying variable assembly

U

or

TS-CRYPTO

1.5.c (X1)

Visual access UNCLASSIFIED.  Controlled COMSEC Item.  Used with KSK-45 DECLAS according to applicable COMSEC documents/guidance.
  d. USKMU-100 A/B

U

to

S-CRYPTO

1.5.c (X1)

Visual access UNCLASSIFIED.  Controlled COMSEC Item.   Used with KSK-45 DECLAS according to applicable COMSEC documents/guidance.
  e. Special purpose cryptographic keyer KSK-45

U

to

S

1.5.c (X1)

Visual access UNCLASSIFIED.  Controlled COMSEC Item.  Used to transfer the keying variable into the KIK-45.  Controlled COMSEC Item.  Used with KSK-45.  DECLAS according to applicable COMSEC documents/guidance.
  f. Power supply

U

 
  g. Transmitter control

U

 
  h. Input/Output unit

U

 
  i. Receiver groups

U

 
  j. Control unit stations 1, 2, and 3

U

 
  k. Group “A” kits (cabling, bracketing, harness, etc).  For aircraft installation.

U

 
  l. Components for communication assemblies used including frequencies.

U

 
  m. Tapes (ALCS)   See Section XIX
8 Reliability data:    
  a. ALCS

S

1.5.g (X2)

 
  b. Airborne system, ALCC

C

1.5.g (X2)

 
  c. Ground system.

C

1.5.g (X2)

Individual components not classified by other sections of this Guide are UNCLASSIFIED; however, any compilation of data which may indicate a trend or rate will be classified as indicated above
9 Parts, accessories, subassemblies and equipment available in the open market or produced for commercial use if classified use is not revealed.

U

 
10 Vulnerability information.

S

1.5.g (X2)

 
11 Impact of ALCS on operational capabilities.  Wing or Force.   Classify per other guidance in this guide
12 Initial operational readiness dates (ALCS):    
  a. Airborne system.

U

 
  b. Ground systems (Wing).

U

 
13 Aircraft

U

 
  a. Total number modified for ALCS

U

 
  b. Master schedule for modification.

U

 
14 Documents relating to training programs at Air Force or contractor facilities   Classified according to contents as determined by this guide.

 

SECTION IX 

COMMUNICATIONS - ELECTRONICS 
 

Higher authority communications terminals used in the Minuteman Weapon System to provide connectivity to the National Command Authority and other higher authorities may have performance parameters, modulation, signal processing, error correction, timing, and other characteristics that are classified.  The applicable communications system security classification guide should be consulted for classification determination of specific system characteristics. 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Design and specification of the voice telephone, interphone, and radio systems.

U

 
2 Design of the radio overlay control component.

U

 
3 Wire system specifications, wire layout and pair count.

U

 
4 Wire system field surveys.

U

 
5 Command control receiver.

U

 
6 MF radio launch control system (WS-133B only):    
  a. Generalized basic and background data.

U

 
  b. General frequency band of operation

U

 
  c. Specific operational frequencies.

U

 
  d. General antenna characteristics

U

 
7 Generalized information on jamming

U

No details.  No frequencies or frequency ranges.  No specific techniques.
8 Code requirements document.

S

1.5.c (X1)

 
9 Details of mechanical-electrical generation of codes.

S

1.5.c (X1)

 
10 General information on code formats

U

Provided no calibration information, frequencies or formats are revealed.  See USSTRATCOM SD 501-12
11 Hardness of operational sites.   See Section XIV.
12 Specific anti-jam features or techniques

S

1.5.c (X1)

Includes detailed drawings which reveal classified data.  System characteristics if such information reveals limitations or design.
13 Anti-jam test data

S

1.5.c (X1)

 
14 Launch codes:    
  a. Complete operational launch code.

TS-CRYPTO

1.5.c (X1)

Special handling required IAW USSTRATCOM SD 501-12. .
  b. Partial operational launch code.

S

to

TS-CRYPTO

1.5.c (X1)

More than half of the launch code is TOP SECRET-CRYPTO.
  c. Launch enable codes

S

to

TS-CRYPTO

1.5.c (X1)

See USSTRATCOM SD 501-12 for TOP SECRET-CRYPTO.
  d. Test launch codes

U

 
15 Command destruct frequencies   Test codes are unclassified unless specified otherwise by NSA or the COMSEC supplement to the Industrial Security Manual.
  a. Command destruct receiver frequency range.

U

 
  b. Sequencing logic required to trigger destruct.

U

 
16 Reliability

U or S

1.5.g (X2)

SECRET when reliability data is lower than weapon system reliability requirements.
17 Transattack/postattack communications availability and limitations.

S

1.5.g (X2)

Could reveal system vulnerabilities for exploitation.

 
 
 

SECTION X 

TESTING PROGRAM 
 

The purpose of this section of the Guide is to establish the classification of information generated in preparation for, in support of, or as a result of flight and ground test operations.  Flight test operations are herein defined to include Development Test and Evaluation (DT&E) and Operational Test and Evaluation (OT&E) flight tests.  Ground test operations are defined to include operational ground test programs such as, but not limited to, Simulated Electronic Launch Minuteman (SELM) where a modification to the weapon system or a subset of the weapon system is being evaluated without having missile flight as an objective.  In some instances, there may be a repetition of data presented in other sections of this Guide, but this was done intentionally to include all data pertinent to the testing community in one section of this Guide.  The classification guidance presented in this section is intended for flight test systems that are prepared and launched on the national test ranges as well as for ground tests conducted in the operational force, at Vandenberg AFB or Ogden ALC test facilities.  It is not intended to contradict or override the classifications assigned to operational deployed systems.  Depending on the configuration of the missile and the potential involvement of different Associated Operations on HQ AFSPC MM test launches, different RV and Associated Operation program Security Classification Guides may apply.  Review the missile configuration and list of approved Associated Operations from HQ AFSPC/DO for each mission (Glory Trip) to determine which other classification guides apply. 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Weapon system testing program:   Except warheads or warhead mockups.
  a. The fact that nonstandard payloads are flown on HQ AFSPC OT&E missions.

U

This is a general statement.  Items 1.c., d., and e. must be reviewed for applicability for each program.
  b. The fact that a nonstandard payload was flown on a specific HQ AFSPC OT&E mission (i.e., identifying Glory Trip # or WSMC Op #).

U to S

1.5.g (X2)

TBD by classification of the Associated  Operation Program or by  HQ AFSPC/DOM.
  c. Association of the sponsoring agency name, an unclassified program name or descriptive identifier (e.g., Infrared Imaging System) with HQ AFSPC in general.

U to TS

1.5.g (X2)

TBD by classification of the Associated  Operation Program and notified by HQ AFSPC/DOM.
  d. Association of an unclassified program name or descriptive identified (e.g., Infrared Imaging System) with HQ AFSPC OT&E).

U to TS

1.5.g (X2)

See Item 1.c remarks.
  e. Association of an unclassified program name or descriptive identifier (e.g., Infrared Imaging System) with a specific HQ AFSPC OT&E mission.

U to TS

1.5.g (X2)

An example is associating program name with Glory Trip # or WSMC Op #.  See Item 1.c. remarks
  f. Specific requirements for any associated operation will be handled in accordance with appropriate classification guides SCGs and/or supplemented by program security guidance issued by  HQ AFSPC.

U to TS

1.5.g (X2)

NOTE:  For Items 1.c., d., and e., the classification of the association may be downgraded to UNCLASSIFIED after each mission is flown.  TBD by classification of the Associated  Operation Program and notified by  HQ AFSPC/DOM.
  g. Information pertaining to anomalies discovered during developmental testing of a system/subsystem.

U to

TS-RD

1.5.g (X2)

If the same anomaly exists or can be expected to exist and adversely affect the performance of any current operational system, the data will be classified as directed in the appropriate section of this Guide.  Public utility furnished adjuncts and interfaces are exempted from classification.
  h. OT&E (flight tests, SELM tests) and other designated ground tests such as Olympic Plays.

U to

S

1,5,g (X2)

The fact that an Olympic Play or SELM anomaly occurred is UNCLASSIFIED. For SELM anomalies, the specific anomaly is classified until determination can be made of possible force wide implications

For Olympic Play testing anomalies, less than 10 failures in one squadron are UNCLASSIFIED.  Failure modes at higher rates are classified until determination can be made of possible force wide implications.  Reports describing these failures are also with classified or unclassified based on the squadron failure rates depicted in them.  EMDAS data and reports are unclassified.  Failure rates and descriptions from more than one wing are classified SECRET. 

 
  • (1) Objectives of test when specific weapon system performance capabilities or limitations are stated or when military objectives are revealed.

S

1.5.g (X2)

General objectives not identifying performance or design specifications criteria are UNCLASSIFIED
 
  • (2) Target case input.

S-FRD

1.5.g (X2)

 
 
  • (3) Results and conclusions which reveal weapon system capabilities, limitations, accuracy or reliability:

S

1.5.g (X2)

Results/conclusions/analyses or reports indicating causes or possible causes of test failures/anomalies including specific failed components will be classified SECRET until it can be proven that there is no force-wide impact on weapon system capability, vulnerability, limitations, accuracy or reliability.  The determination of force-wide impact and the decision to declassify or upgrade applicable data will be made by HQ AFSPC/DOT prior to reclassifying the data. 
 
  • (a) Mention of in-silo or in-flight abort or failure

U

With no clarification.
 
  • (b) Cause or possible causes of failures occurring either in-silo or in-flight, or real-time anomalies/failures revealed during investigations associated with such operations.

S

1.5.g (X2)

Every effort must be made to protect the identification of the failure/anomaly cause or possible cause including specific failed weapon system components as SECRET unless the revelation is required for safety purposes.  Western Test Range flight data will be processed and classified in the same manner whether or not a weapon system anomaly/failure occurred.  Final reports derived from the test range data will be classified SECRET.
 
  • (c) Causes of failures either in-flight or in-silo revealed during anomaly/failure/ investigation reports subsequent to real time operations.

S

to

TS-RD

1.5.g (X2)

See Section XIII and remarks in 1.h.(3) and 1.h.(3)(b) above.
 
    • 1 If RV performance is included.
  See RV guides
 
    • 2  If RV performance is   not included.

S

1.5.g (X2)

 
 
  • (d) Test results or conclusions which identify and impact weapon system capabilities, vulnerabilities, limitations, accuracy or reliability.
  See Section XIII and remark in 1.h.(3) above.
 
  • (e) Weapon system vulnerabilities.
  See Section XIV
 
    • 1 If sure-kill vulnerabilities are not revealed:
  Sure-kill vulnerabilities normally concern nuclear hardness and/or Pen Aids.  See Section XIV, XVII, and XVIII.
 
    • a And RV performance is not included

S

1.5.g (X2)

 
 
    • b And RV performance is included
  See RV guides
 
    • 2 If sure-kill vulnerabilities are revealed.

TS-FRD

1.5.g (X2)

 
 
  • (f) Objectives of test when specific weapon system performance capabilities or limitations:
   
 
    • 1 Are not stated

U

 
 
    • 2 Are stated:
   
 
    • a If RV performance  is included
  See RV guides
 
    • b If RV performance  is not included

S

1.5.g (X2)

 
 
  • (4) Complete schedules.

U

For example, program schedules and complete missile test schedules for entire test program.
 
  • (5) Dates of planned individual R&D tests.

U

For example, planned HQ AFSPC operational flight test dates.  For public disclosure, see Section II (Administrative Details).
 
  • (6) Test Launch site locations.

U or S

1.5.g (X2)

UNCLASSIFIED when World Geodetic System (WGS) coordinates for the LF are not provided.  SECRET when WGS coordinates are provided.
 
  • (7) Number of test missiles to be flown from either range.

U

 
 
  • (8) Telemetry frequencies of Mod 7 or Mod 8.

U

 
 
  • (9) Command destruct receiver frequencies, range or sequencing logic required to trigger destruct.

U

 
 
  • (10) Data.

U to

TS-FRD

1.5.g (X2)

Includes all magnetic visicorder charts, test conductor logs, etc.  See Section III (Performance Data).
 
  • (11) Unannotated raw data.

U

See Section III (Performance Data).
 
  • (12) Flight test data transmissions.

U

Real time radar and telemetry data measured and recorded by test range instrumentation is UNCLASSIFIED until processed.  When such data is subsequently processed or analyzed, it will be classified IAW the provisions of this Guide.  Specifically, all MM booster trajectory data up to thrust termination is UNCLASSIFIED.  For classification of data after thrust termination, refer to the appropriate RV guide.  Post launch analysis and trajectory reconstruction will be classified SECRET-FRD if precise target location, WGS, coordinates are derived and/or depicted.  Analysis of abnormal/anomalous trajectory will be classified IAW this Guide.
 
  • (13) Radar and telemetry sensor look angles on each flight test.

U

                     
  i. Missile target range.

U

Distance to test range.  See 1.h. above.
  j. Target location:    
 
  • (1) Precise WGS coordinate of RV targets (i.e., bullseye).

S-FRD

1.5.g (X2)

 
 
  • (2) Approximate target location on a wide-area map indicating target location.

U

To an accuracy not closer than one nautical mile.
  k. Booster trajectory:    
 
  • (1) If launch site WGS coordinates are included.

S

1.5.g (X2)

See Section XIII.
 
  • (2) If propulsion table is included.

C

1.5.g (X2)

 
 
  • (3) Without (1) and (2) above.

U

 
 
  • (4) MM III Telemetry Inertial Guidance (TMIG) data real time and postflight.

U

Refer to appropriate RV guides where TMIG is post-thrust termination.
  l. RV reentry angle azimuth.

U

Operational Test Launches only.  See RV guides.
  m. Range azimuth envelope and missile alignment.

U

For example, launch time, azimuth and site location (if no WGS coordinates are indicated).
  n. Range azimuth limits.

U

 
  o. Specific launch azimuth

U

 
  p. Telemetry:    
 
  • (1) Telemetry package, antennas and detailed schematic drawings.

U

Unless they reveal classified aspects of the system being measured.
 
  • (2) Telemetry signal conditioning equipment, schematics, and detailed drawings.

S

1.5.g (X2)

If they reveal classified aspects of the system being measured.
 
  • (3) Telemetry data measurement format:
   
 
  • (a) Specific format relationship between raster position (time slot) and measurement  code or measurement description for other than RV or Pen Aids measurements.

U to C

1.5.g (X2)

See Section III (Performance Data) and appropriate RV guide.
 
  • (b) Specific format relationship between raster position (time slot) and measurement code or measurement description for RV or Pen Aids measurements.

U to

S-FRD

1.5.g (X2)

See Section III (Performance Data) and appropriate RV guide.
 
  • (c) General format.

U

For example, number of words per frame, number of frames per second and sampling.
 
  • (d) Calibration information used to convert test data from telemetry units to engineering units.

U

When calibration information and test data are together and will reveal classified information on the weapon system, it is classified by this Guide according to the information revealed
 
  • (e) Plot trace arrangements  for data strip outs which identify measurements recording  performance data.

U

See para 4. for classification of missile performance information.
 
  • (f) Tabulation of measurements  active on a specific test (even if associated with complete descriptions).

U

Provided information requiring classification by para 1.p.(3)(a) or (b) above is not revealed.
 
  • (4) Measurement response whether a single sample or time history.

U to

S-RD to

TS-FRD

1.5.g (X2)

See para 4 of this Section for classification of missile performance information.
  q. Telemetry frequencies:    
 
  • (1) With references to purpose.

U

 
 
  • (2) When associated with air frame missile system.

U

 
2 Operational test launch history reports showing only success or failure:    
  a. A single operational test history report when an indication of failure or test objectives and/or details of the results are shown.

C

to

TS-RD

1.5.g (X2)

May be CONFIDENTIAL to TOP SECRET-RD when otherwise required by this Guide depending upon information revealed.  This applies to para 1.h.
  b. A compilation of two or more operational test launch history reports when an indication of failure of test objectives and/or details of the test results are shown.

C

to

TS-RD

1.5.g (X2)

See remarks 2.a. above.
3 Special tests   Governed by classification guidance provided for that specific test.
4 Missile performance test data:    
  a. Specific performance of propulsion subsystems (Stages 1, 2, or 3)   See Section III.
  b. Specific performance of PBV.

S

to

TS-FRD

1.5.g (X2)

If sequencing and or deployment of Pen Aids to RVs is revealed (Includes PSRE performance which requires classification of the guides, such as the MK 12 Guide).  See Sections IV, XVII, and XVIII for subsystem performance classification requirements or applicable RV guide.  TOP SECRET only if specific vulnerability is revealed.
  c. G&C subsystem performance

S

1.5.g (X2)

When such information reveals missile or subsystem operational capability or limitations, i.e., accuracy, vulnerability, etc.  See Section XIII.
  d. RV performance   See appropriate RV guide.
  e. Pen Aids performance   See Sections XVII and XVIII.
  f. PSRE performance.

U to S

1.5.g (X2)

See Section III.
  g. Test launch narration:    
 
  • (1) Real time - MM II or III
   
 
  • (a) Up to and including Stage 3 TT.

U

 
 
  • (b) After Stage 3 TT.

S-FRD

1.5.g (X2)

See Section V  and RV guides
  h. Weapon system accuracy, predicted or actual:   Measured in Circular Error Probable (CEP).  The CEP is defined as the radius of a circle, centered about the aimpoint, within which 50 percent of the RVs are expected to impact.  (Sometimes referred to as miss distances).
 
  • (1) Total weapon system

S-FRD

1.5.g (X2)

For either individual launches or any compilation of launches.
 
  • (2) RV subsystem contribution to CEP.
  See appropriate RV guide
 
  • (3) Contribution of any subsystem, except the RV subsystem, to the CEP.

S

1.5.g (X2)

See remark in para 4.h. above.
 
  • (4) MM III only
   
 
  • (a) RV to RV in flight separation distance at any time during reentry.
  See appropriate RV guide
 
  • (b) RV to RV impact pattern, with or without actual dimensions.
  See appropriate RV guide
  i. Uprange optical data:   MM II or III
 
  • (1) Up to and including TT.

U or S

or

S-FRD

1.5.g (X2)

See remarks in 1.h.(3).  Nonanomalous uprange video at the time of TT is UNCLASSIFIED.
 
  • (2) After TT:
  See remarks in 1.h.(3).  Low light level TV data from WSMD AN/ASQ-145 (gunship) sensors is SECRET-FRD
 
  • (a) Non-Pen Aids mission

S-FRD

1.5.g (X2)

 
 
  • (b) Pen Aids mission

S-FRD

to

TS-FRD

1.5.g (X2)

Classify SECRET-FRD until evaluation determination is made.  If evaluation finds that a Pen Aids vulnerability is detectable, upgrade film to TOP SECRET-FRD
5 Other tests:   Excluding flight tests but including status, short duration and subscale tests.
  a. Test directives.   Classified according to content as determined by this Guide.
  b. Test results and conclusions.   Classified according to content as determined by this Guide.
  c. Dates of individual tests

U

With or without test number and unclassified test objectives.
  d. Location of tests, including test stand designation.

U

 
  e. Significant progress on/or completion of major objectives in the test program   UNCLASSIFIED provided classified design or performance parameters are not revealed
6 In-place survivability testing.   In-place survivability test information will be classified in accordance with Section XIV.
7 Test data pertaining to RV.   See RV guides.

 
 

SECTION XI 

OPERATIONAL GROUND EQUIPMENT (OGE) 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Ground handling and support equipment, test equipment, training equipment or programs, instrumentation (internal and external), maintenance, repair and overhaul (as contained in handbooks, etc.) reentry and penetration program.

U

to

S-RD

1.5.g (X2)

See applicable sections of this guide.
2 All terminal equipment other than operational coding equipment for communications-electronics.

U

 
3 Launch Control System for Wings†I, III, V, VI.

U

to

TS-CRYPTO

1.5.g (X2)

When the Status Authentication System equipment drawers are installed in the Launch Control System, SECRET-CRYPTO; when operational launch and inhibit codes are inserted in Launch Control System, TOP SECRET-CRYPTO; otherwise UNCLASSIFIED.  See Section II.  Also see USSTRATCOM SD 501-12
4 All terminal equipment other than operational coding equipment for communications-electronics

U

 
5 OGE and/or production schedules.

U

See Section XIII
6 Reliability

U or S

1.5.g (X2)

If no equipment or system performance or CRYPTO information requiring classification by other sections is revealed.  SECRET if survival period reliability or OGE strategies alert reliability can be determined.

 
 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XII 

FACILITIES 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Views of the LF and/or MAF.

U

 
2 LFs and MAFs:   If hardness is revealed, see Section XIV.
  a. Plans and specifications for construction contract purposes.

U

Unless locations of and/or design "hardness" modifications are identified therein, then classify according to other sections of this Guide.
  b. The number of LFs and/or MAFs

U

Not under "Operational Readiness."
  c. Maintenance requirements and procedures.

U

 
  d. Type of configuration for a squadron upon completion of construction.

U

Example:  5X10, i.e., 5 LCCs with 10 launchers per LCC.
3 LF and MAF subsurface conditions:    
  a. Information which discloses the geological subsurface conditions existing at a specific LF or MAF.

U or S

1.5.g (X2)

Information providing complete dynamic test results of subsurface geologic conditions which allow the determination of ground motion from a nuclear blast at a LF or MAF is SECRET.
  b. Information which discloses the geological subsurface conditions for the general area in which a flight, squadron or wing is located.

U

 
  c. Information which correlates an LF or MAF attack response to a specific geological subsurface condition.

S to TS

1.5.g (X2)

Responses at an individual LF or MAF are classified SECRET; responses allowing a qualitative force assessment by squadron or wing are TOP SECRET.
4 Documents related to training programs at Air Force or contractor facilities.   Classified according to contents as determined from this Guide.
5 Load and stresses resulting from missile emplacement and launches that launchers are designed to withstand.

U

 
6 General performance of Real Property Installed Equipment (RPIE).

U

Information does not reveal the operational limitations or capabilities of the facility.
7 Reliability.

U or S

1.5.g (X2)

SECRET is survival period reliability can be determined.

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XIII 

OPERATIONAL DATA 
 

 

Information Revealing

Classification

Reason

Date

Remarks

face="Times" size="1">  face="Times" size="1">  face="Times" size="1">  face="Times" size="1"> 
1 Operational capability date for additions to the ICBM force and/or planned operational readiness dates of individual squadrons

S

1.5.g (X2)

The operational force date is defined as the officially planned date by which a given operational force is tactically deployed under the operational control of an operating command.
2 The total number of missiles in HQ AFSPC that are committed to the SIOP at any point in time:

S

1.5.g (X2)

 
  a. The number of ICBMs in  HQ AFSPC that are on alert at the current time.

U

 
3 Weapon system reaction time.

S

1.5.g (X2)

Weapon system reaction time is the time required to launch any number of missiles; this should not be confused with preplanned commit or delay times which are classified by GATI (Generation and Targeting Instructions)
  a. Planned reaction time for any one or more squadrons of an operational force.

U

 
  b. Demonstrated reaction time for any one or more squadrons of an operational force.

U

 
4 Number of MM missiles planned or authorized for:    
  a. The ICBM force:

U

 
  b. A tactical squadron

U

 
  c. The total number of MM III missiles for the entire MM force.

U

 
  d. Number of MM III missiles for a specific MM wing, squadron or flight.

U

 
5 Actual rates of delivery of MM missiles to the ICBM force.

U

 
6 Location of operational force support bases.

U

 
7 Geodetic, astronomic and geometric parameters required for publication of the missile launch site data catalog:    
  a. The following classification directives apply to Point X and Point A geodetic, astronomic and gravimetric parameters.   Point X and Point A were locations used for early MM targeting procedures
 
  • (1) WGS coordinates ( face="Greek Symbols" size="2">> face="Times" size="2">, face="Greek Symbols" size="2">S)

U or S

1.5.g (X2)

UNCLASSIFIED when given to no better than the closest minute.
 
  • (2) North American Datum Coordinates ( face="Greek Symbols" size="2">> face="Times" size="2">, face="Greek Symbols" size="2">SN) by:
   
 
  • (a) Degree, minute, and second

C

1.5.g (X2)

 
 
  • (b) Given to no better than the closest minute.

U

 
 
  • (3) Astronomic angles ( face="Greek Symbols" size="2">> face="Times" size="2">,a , face="Greek Symbols" size="2">Sa)

C

1.5.g (X2)

 
 
  • (4) Astronomic azimuth ( face="Greek Symbols" size="2">I)

U

 
 
  • (5) WGS deflection of the vertical components.

S

1.5.g (X2)

 
 
  • (6) Absolute acceleration of gravity.

U

 
 
  • (7) Height above mean sea level.

U

 
 
  • (8) North American Data deflection of the vertical components.

C

1.5.g (X2)

 
  b. Parameters when given to no better than closest minute.

U

 
  c. The following classification directives apply to any permanent marker employed in determining requisite parameters for Point X and Point a.    
 
  • (1) WGS coordinates.

C

1.5.g (X2)

Except coordinates rounded to the nearest one-tenth of a minute or worse.
 
  • (2) North American Datum coordinates

U

 
 
  • (3) State plane or grid system coordinates

U

 
 
  • (4) As above 7.a.(3), (4), (6), and (7).
   
 
  • (5) Astronomic angles and North American Datum coordinates of any permanent marker closer than one-half mile from Point X or Point A.

C

1.5.g (X2)

 
  d. The following classification directives apply to statements of parameter accuracy requirements and parameter accuracies achieved:    
 
  • (1) Geodetic and astronomic parameter accuracy requirements and achieved accuracies for Point X and Point A

C

1.5.g (X2)

 
 
  • (2) Geodetic, astronomic and gravimetric parameter accuracy requirements and achieved accuracies for a permanent marker other than Point X and Point A.

U

 
  e. Other pertinent materials.

C

1.5.g (X2)

Classification policy for other pertinent materials, e.g. WGS, 1972 transformation formulas, will be coincident with Defense Mapping Agency Technical Report, ìDepartment of Defense World Geodetic System 1972 (U), íí 1 Jan 1974.
  f. Parameter accuracy requirement and/or the accuracy data published on the MISDS.

S

1.5.g (X2)

When revealed in conjunction with the effects on MM subsystem performance classify SECRET.  The relationship of geodetic, astronomic, and gravimetric parameters errors and/or uncertainties to subsystem or to total weapon system performance that reveals operational capability or limitations will be classified SECRET.
8 Complete concept of weapon system employment

S

1.5.g (X2)

May be RD or FRD.  See RV guides.  The term ìconceptî includes associating Pen Aids with their mission.  See Sections XVII and XVIII.
9 Official weapon system command control and communications plan for operational units.

S

1.5.g (X2)

 
10 Preliminary target system and priority recommendations.

S

1.5.g (X2)

 
11 Target system and priorities based on USAF war plans.

TS

1.5.g (X2)

 
12 Preliminary estimates of weapon system capabilities and effectiveness.

S

1.5.g (X2)

May be RD or FRD.  See RV guides.
13 Weapon system capabilities and effectiveness based on USAF war plans.

TS

1.5.g (X2)

May be RD or FRD.  See RV guides.
14 Location of Alternate Command Post (ACP).

U

 
15 Target selection capability (the number of targets a missile may select):    
  a. Of the missile alone:

U

 
  b. When coupled with other missile capabilities.

S

1.5.g (X2)

The term ìother missile capabilitiesî specifically includes associated Pen Aids with their mission.  See Section XVII and XVIII.
16 Operational mode periods.   The time duration that the System is expected to operate in the indicated operational mode.
  a. Normal mode

U

Normal operation on commercial power.
  b. Standby AC mode

S

1.5.g (X2)

Diesel generated ac power.  Operating requirements such as, total operating time or extended survival operating time are SECRET.
  c. Survival mode periods:   The time periods under specified attack environments that missiles could still be launched successfully.
 
  • (1) Emergency mode period:
  The required time period prior to launch and under specified attacks that the system will operate on emergency (batteries) power.
 
  • (a) Time period that emergency power batteries are designed to provide launch capability.

S

1.5.g (X2)

 
 
  • (b) Time period that environmental control system will maintain equipment within acceptable temperature limits.

S

1.5.g (X2)

 
 
  • (2) Extended survival mode period.

S

1.5.g (X2)

The required time period under specified attacks that the system will operate on extended survival power.
 
  • (3) Survival period.  This includes:
   
 
  • (a) Time period that equipment will provide uncontaminated air supply for personnel.

S

1.5.g (X2)

 
 
  • (b) Time period that food supplies are planned to last.

S

1.5.g (X2)

 
 
  • (4) Human factors, physical and psychological, with which personnel must contend during normal operation, emergency period or extended survival period.

S

1.5.g (X2)

 
 
  • (5) Weapon system reliability during survival period

S

1.5.g (X2)

Survival period reliability refers to strategic alert reliability during the survival period.
17 Target azimuth when associated with the location or designation of the LF.

S

1.5.g (X2)

 
18 Target azimuth not associated with the location or designation of the LF.

U

 
19 Launch azimuth not associated with the location or designation of the LF.

U

 
20 Autocollimation positioning azimuth for Safeguard System Test Target Program (SSTTP) flights.

U

 
21 Firing order

S

1.5.g (X2)

Sequence in which missiles would be fired in an operational flight.
22 External configuration of the MM missile.

U

 
23 Fig ìAî or CI list   Classified according to the nature of the equipment and/or content, as determined from this Guide.
24 Force Modernization/Force Improvement Programs

U

Schedules disclosing planned deployment/delivery dates for modifications to the MM Program are UNCLASSIFIED except when classification is required by the classification guide covering the modified hardware (MK12A, etc.)
25 Weight data of stages or the assembled missile (less RS).

U

See Section V  and RV guides
26 Complete design of missiles (less RS).

S

1.5.g (X2)

See Section V  and RV guides
27 Specific military performance, planned or actual.

U to

S-FRD

1.5.g (X2)

See RV guides and appropriate sections of this Guide.
28 General performance.

U

Such as ìintercontinental rangeî, ìsupersonic reentryî but excluding performance generalities about impact speed.
29 Specific performance of MM missile.

U to

S-FRD

1.5.g (X2)

See RV Guides and Section X of this Guide
30 Estimate or proven conclusions as to weapon system capability or operational limitations.

S

to

TS-RD

1.5.g (X2)

See Section X, Section III (Performance Data) and Section XIV.
31 Vulnerability of the MM weapon system to countermeasures proven or unproven:    
  a. LFs and MAFs

S to TS

1.5.g (X2)

For hardness, see Section XVII
  b. MM missile.

S to TS

1.5.g (X2)

See RV guides and appropriate sections of this Guide.  May be RD or FRD if nuclear weapon information is revealed.
32 Handbook of Weight and Balance data

C

1.5.g (X2)

 
33 Reliability:    
  a. Weapon System

S

or

S-FRD

1.5.g (X2)

Reliability data of RV is SECRET-FRD.  See RV guides
  b. Missile

S

to

S-FRD

1.5.g (X2)

 
  c. Weapon system strategic alert, countdown or flight reliability 

S

1.5.g (X2)

 
  d. Strategic alert reliability of operational ground equipment

S

1.5.g (X2)

 
34 Command control:    
  a. Command control receiver package

U

 
  b. Assigned operational frequency.

U

 
35 Location of RV/payload   The term ìLocationî refers to the fact of existence of the RV/payload at a given location or in a specified area of LF.  The term ìRV/payloadî refers to any MM-related RV, warhead, nuclear weapon or payload whether it is war reserve, operational or a training item.  This includes MK12, MK12A, W56, W62, 78 (all types) payloads, both operational and training.  See para 36 below for more guidance.  Full consideration of Appendix III of the AF Security Classification Guide for Nuclear Weapons has already been taken.
  a. Training RV/Payload:    
 
  • (1) Nuclear type training items at any location
  Such as MK11 Type 3/3A, W62 Type 3, etc.
 
  • (a) When clearly identified as training items.

U

 
 
  • (b) When not clearly identified as training items

U or

C-FRD

1.5.g (X2)

Classify as if a WR item.  See RV guides
 
  • (2) Payload on an operational training LF

U

 
  b. Location of WR or operational RV/payload

U

 
 
  • (1) At MM LFs

U

The location of MM sites standing nuclear alert is UNCLASSIFIED.  However, national policy is that the presence of nuclear weapons, at any location, will neither be confirmed nor denied.  Therefore, extreme caution must be exercised when making public statements or comments to nongovernment personnel.
 
  • (2) At MM support bases.

U

National policy is that the presence of nuclear weapons at any location will neither be confirmed nor denied.  Therefore, extreme caution must be exercised when making public statements or comments to nongovernment personnel.
 
  • (3) Intransit locations:
  Classify at the highest level, as appropriate, listed below.
 
  • (a) Payload identification for any payload transport

U to

S-FRD

1.5.g (X2)

Classify locations and planned primary and alternate convoy routes IAW AFI 31-101 series regulations.
 
  • (b) Other intransit locations.

U to

S-FRD

1.5.g (X2)

Classify locations and planned primary and alternate convoy routes IAW AFI 31-101 series regulations.
 
  • (4) The location of WR MK11, MK12, or MK12A RVs or W56, W62, or W78 warheads for any location not covered under 35b(1) through (4)

C-FRD

1.5.g (X2)

See RV Guides and AF SCG for Nuclear Weapons.
36 Quantities of RVs/payloads   See  Remark for paragraph 35 above for definition of ìRVs/payloads.î
  a. All MM units    
 
  • (1) The total number of nuclear warheads planned, authorized or stockpiled for the ICBM operational force

S-FRD

1.5.g (X2)

See topics 1571, 1533, 1560-63 and 1573 of CG-W-4, Joint ERDA/DOD Nuclear Classification Guide for additional guidance.
 
  • (2) Total number of nuclear warheads planned, authorized or stockpiled for individual operational units (Wings)

S-FRD

1.5.g (X2)

See Remark 36.a.(1) above.
37 Operation Readiness Inspection (ORI) evaluation results.

U

 

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XIV 

NUCLEAR HARDNESS & SURVIVABILITY (NH&S) 
 

Due to sensitivity of ICBM nuclear hardness, survivability, and vulnerability, the following procedures will be applied to all classification levels of hardness information: 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 General    
  a. Nuclear weapon effects studies or the fact that nuclear weapons effects are being studied.

U to TS to

TS-RD/FRD

1.5.g (X2)

Requires special guidance from HQ AFSPC/DOMN for each circumstance
  b. System hardness    
 
  • (1) Mechanical and electronic systems are hardened against nuclear effects

U

This specific information has been officially released.
 
  • (2) The fact that NH&S changes are being made to the system.

U to

TS-RD/FRD

1.5.g (X2)

For RV hardening, see RV guides.  Requires special guidance from HQ AFSPC/DOMN for each circumstance.
 
  • (3) MM II and III missiles have been hardened against radiation and nuclear EMP experienced in flight.

U

This specific information has been officially released.
  c. Hardness impacts and discrepancies:   Hardness impacts may affect mission critical functions.
 
  • (1) Assessed or suspected hardness impacts identified during testing, surveillance programs, system modifications, and analysis.

U to TS RD/FRD

1.5.g (X2)

Requires special guidance from HQ AFSPC/DOMN for each circumstance.  Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction.
 
  • (a) Impacts that affect overall system hardness or survivability.

S-RD/FRD

to

TS-RD/FRD

1.5.g (X2)

Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction  SECRET - RD if relating to the design or fabrication of weapons and FRD if external characteristics, including size, weight and shape, yields and effects, and systems employed in the delivery or use thereof.  TOP SECRET - RD if impact on survivability is related to the design or fabrication of weapons, and FRD if external characteristics, including size, weight and shape, yields and effect, and systems employed in the delivery or use thereof, and if survivability of similar configuration (e.g., wing, force) can be inferred.
 
  • (b)  Impacts that affect subsystem or component hardness but would not affect overall system hardness.

S

1.5.g (X2)

Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction.
 
  • (2) Discrepancies in components or subsystems which do not reveal  defined hardness levels.

U

 
 
  • (3) Discrepancies in components or subsystems which reveals a  vulnerability.

S

1.5.g (X2)

If mission completion is jeopardized, treat as a hardness impact  in accordance with para 1.c.(1) above.
  d. Hardness design criteria:    
 
  • (1) Hardness design criteria or design level, as applied to system, subsystem, or components levels

S or S-RD/FRD

1.5.g (X2)

Examples are numerical specifications that reveal the extent of protection provided against each particular nuclear effect.  SECRET RD if quantified in terms related to criteria for nuclear weapons effects. 
 
  • (2) Hardness design safety margins, as applied to subsystem/ components which do not reveal the specification hardness levels.

U

 
 
  • (3) Hardness qualification or acceptance test levels for individual nuclear weapons effects as applied to subsystems/ components, which do not reveal the specification hardness levels. 

U/S

1.5.g (X2)

If relationship to design criteria or threat criteria is given or supplied, refer to para†(1.d.(1).  If any Hardness qualification or acceptance test levels reveal ground shock environment for hard mounted or shock isolated subsystems/components refer to paragraph (1) and paragraph (2) (will be classified SECRET).
  e. Design considerations/materials:    
 
  • (1) The identification or description of materials used to harden weapon system components.  This includes design information revealing shape, density, weight, thickness, chemical or structural formula, generic names, common names or brand names, except as noted below:

U

to

C-RD

to

S-RD-CNWDI

1.5.g (X2)

UNCLASSIFIED if material is normally used in a nonhardened design application, and the hardening application is not specifically referred to.  Normally, and unless classified information is revealed, material, shielding, or hardening techniques used against all effects except X-Ray are UNCLASSIFIED in generic texts.  The design of special materials for X-Ray hardening is CONFIDENTIAL-RD.  The fact of use of special materials by name or type for X-Ray hardening is also CONFIDENTIAL-RD. (per -WT-1)  SECRET-RD if materials are described or identified for X-Ray hardening.  SECRET-RD (CNWDI) if nuclear weapon design information is revealed.
 
  • (a) The use of the nickname "Brand X" to refer to hardening materials

U

 
 
  • (2) Hardness Critical Item design information and function.

U

Except when revealed in conjunction with hardness levels.  See para 6.b.
  f. RS hardening materials.

C-RD

to

S-RD

1.5.g (X2)

See para 1.e.(1) above.
  g. Funding requirements for proposed or approved hardness or survivability program.

U or S

1.5.g (X2)

SECRET if changes in hardness levels can be inferred.
  h. Planning and schedule

U or S

1.5.g (X2)

Complete planning, programming or scheduling for any proposed or approved hardness activity.  SECRET if changes in hardness levels are defined or can be inferred.
2 Weapon system ground facilities:    
  a. General information.

U or S

to

TS-RD/FRD

1.5.g (X2)

Refer to para 1.
  b. Nuclear weapons effects testing.

U or S

to

S-RD/FRD

1.5.g (X2)

Refer to para 5.
  c. Assessment:    
 
  • (1) Assessed hardness, survivability and vulnerability

U or S

to

TS-RD/FRD

1.5.g (X2)

Refer to para 6.
 
  • (2) Vulnerability numbers.

TS-RD/FRD

1.5.g (X2)

These are quantitative statements of assessed hardness, distinct from vulnerability statements.
  d. Endurability:   Except as otherwise noted, endurable hardness equipment and survivability information will be classified as launch-essential/mission-critical weapon system ground facilities hardness and survivability information
 
  • (1) Weapons effects to which endurable equipment is hardened.

S

1.5.g (X2)

SECRET if hardness level or hardness design level is revealed.
 
  • (2) Designed or assessed Endurability time period.

S (X2)

The time period that the system will remain operational on Emergency (battery) or Extended Survival (battery and diesel generator) power
3 Missile:    
  a. G&C:

U or S

1.5.g (X2)

 
 
  • (1) Specific reference to nuclear environment levels that  components, circuits, modules are hardened to

U or S

1.5.g (X2)

UNCLASSIFIED if the level of environment is not specified.
 
  • (2) Definition of techniques and component substitutions designed to prevent or minimize effects on the subsystem when reference is made to levels of environment

S -RD-FRD or TS-RD-FRD

1.5.g (X2)

SECRET if the level of environment is specified.  See 1.c. (1).(a) above.
  b. Pen Aids    
 
  • (1) Hardening of Pen Aids components.

U to S-RD

See para 1.e. (1) above
  c. RS:    
 
  • (1) The fact that RS components are hardened against:
   
 
  • (a) An unspecified threat

U

 
 
  • (b) Nuclear threats.

U

See para 1.b.
 
  • (c) Other threats.

U to S

1.5.g (X2)

Requires special guidance from HQ AFSPC/DOMN for each circumstance.
 
  • (2) Physical characteristics, e.g., density or weight, or hardening materials associated with or for RS components.

C-RD to S-RD

1.5.g (X2)

See para 1.e (1) above.
 
  • (3) Access to hardening material, including scrap, when its use for hardening any RS component is disclosed

S-RD

1.5.g (X2)

Visual access is UNCLASSIFIED when appearance does not disclose use of the material. A part number on or associated with an item discloses use and is therefore classified SECRET-RD.
 
  • (4) Quantity of hardening materials purchased for each RS component

C

1.5.g (X2)

 
 
  • (5) Performance, capability, reliability, or vulnerability of hardening materials in RS components.

S-RD

1.5.g (X2)

 
 
  • (6) RS hardware design for protection against EMP and radio frequency (RF) radiation.

C-RD

or

S-RD

1.5.g (X2)

SECRET-RD if design  level of hardness is revealed.
 
  • (7) RS hardware design for protection against X-rays and other radiation

C-RD

or

S-RD

1.5.g (X2)

SECRET-RD if design  level of hardness is revealed.
  d. Nuclear weapons effects testing.

U or S-RD/FRD

1.5.g (X2)

Refer to para 5.
  e. Assessed hardness, survivability  or vulnerability

U to TS-RD/FRD

1.5.g (X2)

Refer to para 6.
4 Communications system:    
  a. Communications equipment:   Includes all receivers, transmitters, and antennas or connectors collocated with the weapon system.
 
  • (1) General information

U to TS-RD/FRD

1.5.g (X2)

Refer to para 1.
 
  • (2) Nuclear information effects testing.

U or S-RD-FRD

1.5.g (X2)

Refer to para 5.
 
  • (3) Assessed hardness, survivability, and vulnerability.

U to

TS-RD-FRD

1.5.g (X2)

Refer to para 6.
  b. Connectivity:   Refers to message transmission paths not collocated with and not part of the  weapon system.
 
  • (1) Degradation of hardened radio link connectivity due to nuclear weapons effects

U to

TS-RD/FRD

1.5.g (X2)

Requires special guidance from HQ AFSPC/DOMN for each circumstance.
 
  • (2) Degradation of hardened intersite cable connectivity due to nuclear weapons effects.

U to TS-RD/FRD

1.5.g (X2)

Requires special guidance from HQ AFSPC/DOMN for each circumstance.
5 Nuclear weapons effects testing:   Encoding provisions of para 6.b.(3) apply.  Testing may be of a weapon system unique component, which is a part, subassembly, drawer rack or subsystem manufactured or configured in such a way as to be unavailable to the general public; or testing may be of a generic component, which is a part, subassembly, drawer, rack, or subsystem which is either a) regularly used for other than Government purposes, or b) is available for purchase or trade to non-Government entities or the general public.  As a general rule, test information, including fragility levels, of a generic component is easily reproducible by other organizations and is UNCLASSIFIED.
  a. Tester performance:    
 
  • (1) Simulation capability of a tester.  Planned, required, or actual test drive level at the tester interfaces.

U

Test levels at test equipment interfaces are not classified unless information requiring classification by other provisions of this Guide are revealed
 
  • (2) The relationship between tester capabilities as stated in para (1) above and the design hardness criteria of operational hardware.

S

1.5.g (X2)

 
 
  • (3) The relationship between tester capabilities as stated in para (1) above and the criteria for nuclear weapons effects

S-RD/FRD

1.5.g (X2)

 
  b. Test configuration.

U

Includes physical test data and configuration drawings, including test measurement, which do not reveal hardness design criteria or nuclear weapons effects criteria. Test levels by themselves are not classified unless their relationship to the specification hardness levels is stated or implied.
  c. Calibration data.

U or S

1.5.g (X2)

SECRET when data reveals information from which hardness design criteria can be deduced
  d. Weapon system test data/ results:   Including measured test responses; excluding tester performance data.
 
  • (1) Analytical or inferred pretest predictions for generic components

U

Generic components include (but are not limited to) integrated circuits, transistors, silicon controlled rectifiers, diodes and other electronic piece-parts.  UNCLASSIFIED if the annotation does not reveal any potential impact and test predictions do not state their relationship to any classified criteria levels.
 
  • (2) Analytical or inferred pretest predictions for weapon system components.

S

to

S-RD/FRD

1.5.g (X2)

Weapon system unique components include tailored electrical circuits, modules, drawers,  subsystems, and overall system.  SECRET-RD when related to restricted data RD criteria levels.
 
  • (3) Predicted or observed upset levels where permanent damage is not incurred.

U or S to

S-RD/FRD

1.5.g (X2)

UNCLASSIFIED for generic components if the relationship of test levels to specification hardness levels is not stated or implied.  SECRET for weapon system unique components.  SECRET-RD when related to RD critical levels.  If damage is incurred, see para 5.e.
 
  • (4) Predicted or observed integrated circuit latch-ups

U or S

to

S-RD/FRD

1.5.g (X2)

UNCLASSIFIED if the relationship of test levels to specification hardness levels and potential impacts is not stated or implied.  SECRET-RD when related to RD criteria levels.
 
  • (5) Annotated test data for generic components.

U

Annotated data is data which 1) identifies or implies use of the tested item in the weapon system either by part number (or other weapon system unique identifier) or by stating use or location, and 2) identifies the tested parameter(s) or test condition(s). UNCLASSIFIED if the relationship of test levels to specification hardness levels and potential impacts is not stated or implied.
 
  • (6) Annotated test data for weapon system unique component or the overall system.

S

to

S-RD/FRD

1.5.g (X2)

Refer to para 5.d.(2) above, and para 5.e.
 
  • (7) Unannotated raw data.

U

UNCLASSIFIED subject to the provisions of Section III (Performance Data).
 
  • (8) Detailed hardness test schedules and locations of hardness tests at or inside of operational sites.

U

 
 
  • (9) Still or motion pictures of test results identified to the test program.

U

UNCLASSIFIED if hardness design criteria, nuclear effects criteria, and/or level at which any item being tested failed is not revealed.
 
  • (10) Test data revealing hardness level or failure level of any item being tested.

U or S

1.5.g (X2)

UNCLASSIFIED if the level are not related to hardness levels.
  e. Test fragilities:    
 
  • (1) Test fragility levels for generic components, tested as generic parts.

U

See para 6.b.(3)
 
  • (2) Test fragility levels for weapon system unique components.

U or S to S-RD/FRD

1.5.g (X2)

UNCLASSIFIED if levels are not related to specification hardness levels. 
 
  • (3) Failure reports from hardness testing of weapon system unique components.

S to

S-RD/FRD

1.5.g (X2)

See para 5.d.(6) and 6.b.(3).
 
  • (4) Statistical inferences made for fragility levels based on weapon system unique component testing.

U or S

to

S-RD

1.5.g (X2)

See para 5.d.(6) and 6.b.(3).
  f. Test survivability.  Inferred probability of survival of weapon system unique components under nuclear environments simulated by testing.

S

1.5.g (X2)

If overall weapon system survivability is affected, see para 1.c.(1).(a).
6 Assessment:    
  a. Threats and environments:    
 
  • (1) Attack scenarios showing weapon laydown or timing or burst locations relative to weapon system posture.

S

to

S-RD/FRD

1.5.g (X2)

SECRET-RD if weapon design criteria can be obtained.
 
  • (2) Relationships among design criteria, weapon yields or other parameters, ranges or burst locations, and critical nuclear weapons effects.

S-RD/FRD

1.5.g (X2)

 
 
  • (3) Predicted free field nuclear weapons effects environments.

U

to

S-RD/FRD

1.5.g (X2)

SECRET-RD if weapon design criteria can be obtained.
 
  • (4) Predicted nuclear weapons effects coupled into and appearing in the weapon system.

U or S

to

S-RD/FRD

1.5.g (X2)

UNCLASSIFIED if levels are not related to hardness environment levels.  SECRET- RD if weapon design criteria can be obtained. 
  b. Assessed hardness or fragility levels:   Hardness levels are assumed to affect critical mission accomplishment.
 
  • (1) Assessed hardness level, probability of failure/ survival as a function of equivalent total nuclear environment, particular nuclear weapon effects levels, or environment level for each individual LF or MAF as well as for a squadron, wing, or for the entire force.  This includes assessed VNTKs.

TS-RD/FRD

1.5.g (X2)

Official hardness assessment will be made only as directed by the Chief of Staff, USAF.  The release or dissemination of any assessment data will be by HQ AFSPC/DOMN.
 
  • (2) Assessed hardness either individually or collectively, given in terms of equivalent total nuclear environment or in terms of particular nuclear weapons effect levels.

TS-RD/FRD

1.5.g (X2)

See remarks in para 6.b.(1) above.
 
  • (3) Hardness or fragility levels for components where no effect on overall system hardness or survivability is given or can be inferred

U or S

to

S-RD/FRD

1.5.g (X2)

UNCLASSIFIED if component and function in the weapon system is not referred to and the hardness environment levels  can not be derived.  SECRET if potential mission consequences of failure are given or can be inferred.  SECRET-RD if related to RD criteria levels
 
  • (4) Hardness or fragility levels for components, configurations, drawers, or subsystems

S

or S-RD/FRD

or TS-RD/FRD

1.5.g (X2)

TOP SECRET-RD if assessed system hardware level can be inferred and quantified in terms related to weapon criteria & if hardness or fragility levels of similar configurations (e.g. wing, force) can be inferred.
 
  • (5)  Hardness or fragility levels, identified by means of code, for a weapon system component.

U

UNCLASSIFIED if the guidelines of para 6.b.(3) above are used to classify the code document
  c. Threat responses from predictions and assessments:    
 
  • (1) Assessed responses within the weapon system due to criteria for nuclear weapon effects.

S

to

S-RD/FRD

1.5.g (X2)

SECRET-RD if related to RD criteria levels.
 
  • (2) Analytical response predictions within the weapon system, identified by code.

U

UNCLASSIFIED if responding equipment, location in the weapon system, and mission-critical function are not revealed.  Code documents must be classified IAW guidance in this section.
 
  • (3) Assessed or predicted responses at the free-field coupling interface due to criteria for nuclear weapons effects.

S

to

S-RD/FRD

1.5.g (X2)

Direct-coupled responses are not to be coded.  SECRET-RD if related to RD criteria levels. 
 
  • (4) Comparison of assessed or predicted threat at component to the component fragility

S

or S-RD/FRD

or TS-RD/FRD

1.5.g (X2)

See paragraph 6.b.
 
  • (5) Analytical coupling models by means of which free-field weapon effects are reduced to internal system responses, or transfer functions, which relate internal system responses at two different locations

U

UNCLASSIFIED if hardness environment levels can not be derived. 
 
  • (6)  Assessed or predicted equipment upset levels for threat responses, where permanent damage is not incurred.

U

to

TS-RD/FRD

1.5.g (X2)

Upset/Recovery times UNCLASSIFIED if mission completion is not jeopardized. 
  d. Assessed survivability:    
 
  • (1) Overall system survivability assessments

TS-RD/FRD

1.5.g (X2)

Official survivability assessment will be made as directed by the Chief of Staff, USAF.  The release or dissemination of any survivability data will be by HQ AFSPC/DOM.
 
  • (2) Component and subsystem survivability assessment

S

to

TS-RD/FRD

1.5.g (X2)

Classify IAW appropriate paragraphs within this section on weapon system threat responses and fragility levels used to derive the survivability distribution
 
  • (3) Uncertainties such as variances and higher order statistical moments associated with survivability distribution.

U

Distribution parameters are UNCLASSIFIED if distribution means or survivability or other critical tolerance limits are not revealed.
 
  • (4) Operational timing studies and vulnerability time windows used to quantify timing factors of survivability.

S

1.5.g (X2)

 
 
  • (5) Survivability and confidence levels  established for hardness surveillance, validation, or verification.

S

to

S-RD/FRD

1.5.g (X2)

SECRET-RD if levels  are expressed which reveal restricted data criteria.
  e. Vulnerability   The term vulnerability usually refers to operation in a hostile environment rather than in a benign environment.  The term includes susceptibility to fragment or projectile penetration, nuclear radiation, blast loadings, RF transmissions, etc.
 
  • (1) Vulnerability to countermeasure environments:
  For RV vulnerability see RV guides
 
  • (a) Suspected vulnerability.

S

to

S-RD/FRD

1.5.g (X2)

If countermeasure environments  specify nuclear criteria characteristics, then SECRET-RD.
 
  • (b) Demonstrated vulnerability.

S

to

TS - RD/FRD

1.5.g (X2)

SECRET if demonstrated vulnerability is for one missile.  TOP SECRET if vulnerability is for more than one missile.
 
  • (2) Enemy defense model based on:
   
 
  • (a) U.S. nuclear technology.

S-RD/FRD

1.5.g (X2)

Technology to include nuclear weapons effects criteria.  See RV guides
                                           
  • (3) Any actual or potential vulnerability to either defensive action or natural phenomena that could restrict or reduce system effectiveness.

U to TS

or TS-RD/FRD

1.5.g (X2)

UNCLASSIFIED if status is Partial Mission Capable (PMC) for individual or combined  facilities.  SECRET if application is to a single strategic missile, MAF or LF.  TOP SECRET if application can be extended to similar configurations, such as squadron, wing, MM II or III missile, or entire force.  TOP SECRET-RD if vulnerability is to criteria nuclear weapons effects.
  f. Criticality.

C

1.5.g (X2)

Criteria for mission criticality of hardened components or subsystem, expressed in terms of mission consequences.

 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XV 

SYSTEM SAFETY FAULT TREE ANALYSIS RESULTS 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Results of fault tree analysis probability IND, FL, and AMI.IPL

S-FRD

1.5.g (X2)

For example:  Probability of AMI is

10-xx per squadron in ten years.

2 That fault tree analysis is being accomplished to determine the probability of:    
  a. Faulty Launch (FL)

U

 
  b. Inadvertent Nuclear Detonation (IND)

U

 
  c. Accidental Motor Ignition (AMI)

U

 
  d. Inadvertent Programmed Launch IPL)

U

 
3 The specification level numerical probability that must be met:    
  a. Faulty Launch (FL)

U

Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included.
  b. Inadvertent Nuclear Detonation (IND)

U

Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included.
  c. Accidental Motor Ignition (AMI)

U

Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included.
  d. Inadvertent Programmed Launch (IPL)

U

Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included.
4 The actual or calculated numerical probability:    
  a. Faulty (FL)

S

1.5.g (X2)

To include Fault Tree formats to support development
  b. Inadvertent Nuclear Detonation (IND)

S-FRD

1.5.g (X2)

To include Fault Tree formats to support development
  c. Accidental Motor Ignition (AMI)

S

1.5.g (X2)

To include Fault Tree formats to support development
  d. Inadvertent Programmed Launch (IPL)

S

1.5.g (X2)

To include Fault Tree formats to support development
5 Results of fault analysis identifying the probability of:   The preferred format is:  The Probability of AMI or IND etc. is 10-xx (super script) per squadron in XX years.
  a. Faulty Launch (FL)

S

1.5.g (X2)

To include Fault Tree formats used to support development.
  b. Inadvertent Nuclear Detonation (IND)

S-FRD

1.5.g (X2)

To include Fault Tree formats used to support development.
  c. Accidental Motor Ignition (AMI)

S

1.5.g (X2)

To include Fault Tree formats used to support development.
  d. Inadvertent Programmed Launch (IPL)

S

1.5.g (X2)

To include Fault Tree formats used to support development.

 
 
 

SECTION XVI 

UNAUTHORIZED LAUNCH

AND

LAUNCH ACTION STUDIES 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       

1

A compilation of unauthorized launch (UL) scenarios of any WS-133 system covering multiple areas of vulnerabilities.

TS

1.5.g (X2)

Basic or revised studies for each weapon system configuration.

2

A single complete UL scenario with detailed procedures.

TS

1.5.g (X2)

 

3

A single or compilation UL scenario(s) limited to a single area of vulnerability but not revealing  detailed procedures. 

S

1.5.g (X2)

Such as studies for modifications when an addendum is written.

4

Partial UL scenario(s).

S

1.5.g (X2)

Usually during UL Study preparation or in briefings.

5

Detailed procedures for accomplishing a portion of an UL scenario or information revealing a system or component vulnerability.

S

1.5.g (X2)

 

6

A complete launch action study with detailed procedures.

S

1.5.g (X2)

 

7

A partial launch action study with detailed procedures.

C to S

1.5.g (X2)

Dependent upon extent of detail in the launch action study.  Classify per special guidance from AFSC/SEW for each case.

8

A complete launch action study without detailed procedures but revealing a component vulnerability

C

1.5.g (X2)

 

9

A partial launch action study without detailed procedures and not revealing a component vulnerability.

U

 

10

That UL studies and launch action studies exist.

U

 

11

Vulnerabilities to communication security keys, codes or algorithms.

TS

1.5.g (X2)

Applies to all systems using nuclear command and control.

 

Note:  Access to these documents is strictly controlled by  AFSC/SEW.  AFI 91-106 Unauthorized Launch and Launch Action Studies is the controlling directive and provides information on authorized access, preparation, use of cover sheets, and storage requirements and distribution and destruction restrictions.

 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XVII 

MM II PEN AIDS (MK I/MK IA PEN AIDS) 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
      Even though it has been phased out, MK I Pen Aids system information remains classified due to its similarity with the MK IA Pen Aids system.
1 Use of acronyms or abbreviations.   Classify the same as the information that would be revealed if not abbreviated.
2 Complete engineering.

U or S

1.5.g (X2)

MK I or MK IA subsystem engineering or operational mock-ups.  UNCLASSIFIED when Pen Aids Countermeasure System (PACS) units are not included
3 Pen Aids spacer.

S

1.5.g (X2)

Visual access is UNCLASSIFIED
4 Mating details of Pen Aids:    
  a. Element with canister

S

1.5.g (X2)

An element is any dipole or reflector carried within the Pen Aids canister.
 
  • b. Canister with spacer.

S

1.5.g (X2)

This subject concerns any information detailing the orientation of the canister within the launch tubes and their positioning in the dispersal sequence.
  c. Spacer with missile

U

A spacer is the structural section which contains the canisters and ordnance.
5 Data on minor hardware and ordnance items from which internal canister details, mating details or RV position in clouds cannot  be determined

U

 
6 Payload information revealing:    
  a. Type of Pen Aid payload such as chaff, wire, exhaust plume, etc.

S

1.5.g (X2)

 
  b. Total number of Pen Aid canisters carried.

U to S

1.5.g (X2)

SECRET:  Individual operational sortie.
  c. Number of salvos or number of Pen Aids per salvo.

S

1.5.g (X2)

A salvo describes the dispersal of the Pen Aids canisters.  A salvo may consist of one or more chaff puffs ejected at one time.
7 Infrared signature

S

1.5.g (X2)

 
8 Existence of a threat cloud or threat tube.

U

 
9 Threat cloud size, density or pattern

S

1.5.g (X2)

 
10 In-flight spacing or accuracy of spacing.

S

1.5.g (X2)

 
11 Screening:    
  a. Type or extent.

S

1.5.g (X2)

 
  b. Dispersion operating rates and survival altitude.

S

1.5.g (X2)

 
  c. Altitude of ejection.

S

1.5.g (X2)

 
  d. Operational flight characteristics or performance.

S

1.5.g (X2)

 
  e. System reliability.

S

1.5.g (X2)

 
  f. Signature characteristics:    
 
  • (1) Radar frequency band

S

1.5.g (X2)

 
 
  • (2) Radar cross section.

S

1.5.g (X2)

 
 
  • (3) Reflective or response frequencies

S

1.5.g (X2)

 
 
  • (4) Any other signature characteristics

S

1.5.g (X2)

 
12 Type of enemy radar encountered; e.g., range or frequency band.

S

1.5.g (X2)

 
13 Specific vulnerability information for subsystems or components

TS

to

TS-RD

1.5.g (X2)

 
14 Specific and detailed information on countermeasures or protection from enemy countermeasures.

TS

to

TS-RD

1.5.g (X2)

 
15 Pen Aids flight test and performance information.  Evaluation of operational Pen Aids performance against design requirements or postulated threat.

S

or

TS-FRD

1.5.g (X2)

 
16 Known or suspected anomalies and possible relationship to MM II force-wide impact.

S

or

TS-FRD

1.5.g (X2)

 
17 Flight test times and locations.

U

 
18 Production data.

U or S

1.5.g (X2)

 
19 Manufacturing data.

S

1.5.g (X2)

 
20 Chaff (whether or not identified as such):    
 
  • a. Visual access to external package assembly (with or without ejection device).

U

 
  b. Dipoles, wire, etc:    
 
  • (1) Material (generic title).

C

1.5.g (X2)

 
 
  • (2) Prior to cutting to desired lengths.

C

1.5.g (X2)

 
 
  • (3) Diameter

C

1.5.g (X2)

 
 
  • (4) Lengths

S

1.5.g (X2)

 
21 The MK11 RV position in chaff train on any test mission.

S-FRD

1.5.g (X2)

 
22 Association of MM II Pen Aids with their mission.

S

1.5.g (X2)

See Section XIII.

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XVIII 

MM III PEN AIDS (MK12/MK12A PEN AIDS) 

PART A 

COMPLETE PEN AIDS SYSTEM 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Any association or cross association of the terms, MM III, MK12, MK12A RS, MK12/MK12A Pen Aids, chaff, decoys or dipoles.

U

 
2 Pen Aids production data:    
  a. Total quantities to be produced or contracted for.

U

 
  b. Planned or actual rates of delivery to any operational site

S

1.5.g (X2)

The number of RVs or decoys postured on or planned for any operational missile is SECRET-FRD.
  c. Funding

U

or

S-FRD

1.5.g (X2)

SECRET-FRD if War Reserve RVs (WR RV) quantities can be determined
3 Number of chaff dispensers per operational missile.

S

1.5.g (X2)

 
4 Pen Aid system reliability.

S

1.5.g (X2)

 
5 Targeting accuracy of Pen Aids system

S

1.5.g (X2)

 
6 Maximum or minimum range of Pen Aids system.

S

1.5.g (X2)

 
7 Vulnerability to countermeasures.

TS

1.5.g (X2)

If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required
8 Missile discrete or analog signal characteristics (voltage and duration of signal) used to initiate events or control Pen Aids components

U

or

S-FRD

1.5.g (X2)

When total number of signals is revealed, SECRET-FRD.
9 DC power allotment or utilization of Pen Aids system.

U

 
10 Trajectory information:    
  a. Exoatmospheric point mass

S

1.5.g (X2)

 
  b. Exoatmospheric dynamic trajectories

S

1.5.g (X2)

 
  c. Reentry trajectories.

S-FRD

1.5.g (X2)

See RV guides.
11 Mission sequence of Pen Aid events including timing and deployment altitudes.

S

1.5.g (X2)

 
12 Evaluation of operational Pen Aids performance against design requirements or postulated threats

S

or

TS-FRD

1.5.g (X2)

TOP SECRET-FRD if a method of discrimination is revealed,  HQ AFSPC/DOM approval for release or dissemination is required.  If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required.
13 Hardening of MK12/MK12A Pen Aids

U

or

S-FRD

1.5.g (X2)

See Sections V and XIV.
14 Number of chaff reentry trains

U

or

S-FRD

1.5.g (X2)

UNCLASSIFIED for Operational Test (OT) missiles, otherwise SECRET-FRD.
15 Geometry of reentry train.    
  a. Train to train distances.

S-FRD

1.5.g (X2)

 
  b. Cloud to cloud distances.

S-FRD

1.5.g (X2)

 
16 Known or suspected anomalies and possible relationship to MM III force-wide impact.

S

or

TS-FRD

1.5.g (X2)

If impact is or is suspected to be Minuteman III force-wide, classify TOP SECRET-FRD and submit to OO-ALC/LM and HQ AFSPC/DOM for classification determination.

 
 
 

PART B 

CHAFF SUBSYSTEM 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Chaff subsystems:    
  a. Max quantity of clouds that can be loaded or deployed.

S

1.5.g (X2)

 
  b. Quantity of chaff dispensers on an operational missile

S

1.5.g (X2)

 
  c. Max quantity of chaff clouds per chaff dispenser.

S

1.5.g (X2)

 
2 Chaff dispensers:    
  a. Chaff dispenser excluding boats

U

 
  b. Chaff boats excluding dipoles

S

1.5.g (X2)

Visual and physical access
3 Chaff attachment kit:    
  a. Power distribution panel.

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  b. Converter (setting module).

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  c. Dispenser controller.

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  d. Hardness material

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

4 Complete chaff subsystem (actual or engineering mockup):    
  a. With carriers or dipoles    
 
  • (1) If dipoles are visible.

S

1.5.g (X2)

Visual and physical access
 
  • (2) If dipoles are not visible.

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  b. Without carriers or dipoles.    
  c. Dipoles alone.

S

1.5.g (X2)

Visual and physical access
5 Chaff subsystem:    
  a. Wire lengths

S

1.5.g (X2)

 
  b. Wire diameters

S

1.5.g (X2)

 
  c. Wire materials.

C

1.5.g (X2)

 
  d. Weight.

C

1.5.g (X2)

 
6 Broad Band Unit (BBU) radar cross section:    
 
  • a. Static.

S

1.5.g (X2)

 
 
  • b. Dynamic.

S

DECLAS

1.5.g (X2)

 
  c. Operating characteristics

S

1.5.g (X2)

 
  d. Cloud geometry (length, width).

S

1.5.g (X2)

 
  e. Composition of BBU.

S

1.5.g (X2)

 
7 Physical unmasking altitude.

S

1.5.g (X2)

 
8 Doppler unmasking altitude.

S

1.5.g (X2)

 
9 Chaff survival altitude.

S

1.5.g (X2)

 
10 Chaff deployment parameters    
 
  • a. Ejection velocity range.

S

1.5.g (X2)

 
 
  • b. Deployment angle.

S

1.5.g (X2)

 
 
  • c. Time of puff range.

S

1.5.g (X2)

 
 
  • d. CEP (specific flight).

S

1.5.g (X2)

 
 
  • e. Lateral separation accuracy.

S

1.5.g (X2)

 
  f. Chaff ejection velocity.

S

1.5.g (X2)

 
11 Reliability.

S

1.5.g (X2)

 
12 Chaff test configuration designed for development tests, flight-proof tests and qualification tests   Classify per this Guide according to information revealed.
13 Vulnerability to countermeasures    
  a. Techniques for discrimination between the RV/decoy-bearing chaff cloud and non-RV/decoy- bearing chaff clouds.

TS

or

TS-FRD

1.5.g (X2)

If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required.  TOP SECRET-FRD if nuclear weapon information is revealed.  See RV guides.
  b. Ways of discriminating between decoys and RVs.

TS-FRD

1.5.g (X2)

 
14 Weight:    
  a. Chaff dispenser including chaff

S

1.5.g (X2)

 
  b. Chaff dispenser excluding chaff.

U

 
  c. Chaff attachment kit.

U

 
  d. Weight of puff or BBU.

S

1.5.g (X2)

 
15 Fact that there is a chaff-masking design requirement.

U

If design requirements are revealed, classify per this Guide, as appropriate.

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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PART C 

DECOY SUBSYSTEM 
 

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 Decoy subsystem:    
  a. The fact that the Pen Aid system can contain more than one decoy.

U

 
  b. Max quantity of decoys that can be loaded or deployed.

S-FRD

1.5.g (X2)

Could reveal max RVs which could be loaded or deployed
2 Decoy assembly:

S

1.5.g (X2)

 
  a. Nose.

U  to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  b. Ballast.

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  c. Aft section.

U  to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

  d. RF Enhancer.

S

1.5.g (X2)

 
  e. Seeding ring.

U to S

1.5.g (X2)

Visual access UNCLASSIFIED

Physical access SECRET

3 Decoy erection and ejection mechanism:    
  a. Platforms.

S

1.5.g (X2)

 
  b. Ejection mechanism.

U

 
4 Complete decoy subsystem engineering mockup (including decoys and decoy platform kit).

S

1.5.g (X2)

 
5 Physical characteristics:    
  a. External configuration.

S-FRD

1.5.g (X2)

 
  b. External dimensions

U

 
  c. Weight

S-FRD

1.5.g (X2)

 
  d. Center of gravity.

S-FRD

1.5.g (X2)

 
  e. Moments of inertia.

C-FRD

1.5.g (X2)

 
  f. Products of inertia.

U

 
  g. Ballistic coefficient.

S-FRD

1.5.g (X2)

 
6 Materials:    
  a. Heat shield

U

to

TS-FRD

1.5.g (X2)

If hardness information is revealed, then classify CONFIDENTIAL to TOP SECRET-FRD.  See Section XIV.
  b. Nose.

U

to

TS-FRD

1.5.g (X2)

See para 6.a. above.
  c. Structure.

U

 
  d. Enhancer

S-FRD

1.5.g (X2)

 
  e. Ballast plating.

S-FRD

1.5.g (X2)

 
7 Radar cross section

S

to

S-FRD

1.5.g (X2)

Includes design requirements.  SECRET-FRD if RV data is revealed
8 Aerodynamics performance.

S

to

S-FRD

1.5.g (X2)

SECRET-FRD if RV performance revealed
9 Fluid dynamics performance

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
10 Thermodynamics performance.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
11 Performance altitude    
  a. Simulation of RV signature and trajectory.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  b. Survival.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
12 Reliability.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
13 Decoy test configuration for:    
  a. Radar range measurements

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  b. Vacuum chamber, wind tunnel or arc jet tests.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  c. Flight-proof tests.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  d. Qualification tests.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
14 Vulnerability to countermeasures.

S-FRD

to

TS-FRD

1.5.g (X2)

Up to TOP SECRET-FRD if RV information is revealed. See RV guides.
15 Deployment parameters    
  a. Decoy ejection velocity

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  b. CEP

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  c. Lateral separation accuracy.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
  d. Spin rate.

S-FRD

1.5.g (X2)

Simulates RV performances.  See RV guides.
16 Complete design, operating performance of the operational ejection mechanism.   Classify per this Guide according to information revealed.
17 Weight:    
  a. Decoy.

S

1.5.g (X2)

 
  b. Platform kit.

U

 
  c. Components.

U

 
18 Operational evaluations of decoy performance against design requirements.

S

to

TS-FRD

1.5.g (X2)

Up to TOP SECRET-FRD if RV information is revealed. See RV guides.
19 Association of MM III Pen Aids with their mission.

S

1.5.g (X2)

See paras 9 and 16

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

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SECTION XIX 

SOFTWARE AND DATA 
 

References:   
a. CJCSI 3231.01, “Safeguarding the Single Integrated Operational Plan, dated 30 November 1993.  Classified by:  Director, J-3, Declassify on: 1.5.g (X2) 
b. CG-W-5, Joint DOE/DoD Nuclear Weapon Classification Policy Guide, dated January 1994.  Classified by:  Robert T. Duff, J-3 Director, Office of Classification, Department of Energy. 
c. Strategic Target Planning Security Classification Guide, dated 3 February 1997.  Classified by:  Vice Admiral Dennis A. Jones, Deputy Commander in Chief, United States Strategic Command .  Reason:  1.5a.  Declassify on:  X4.  

 

Information Revealing

Classification

Reason

Date

Remarks

       
1 ICBM target cases.

S-FRD or

TS-FRD SIOP-ESI

(Cat 06)

1.5.a

Classified by references a, b, and c.  Target cases for an entire unit (a missile squadronÂ’s on-alert sorties) are TOP SECRET-FRD/SIOP-ESI (Cat-06).
2 ICBM execution plan cases

S

1.5.a (X4)

Classified by reference c.  Execution plan cases do not reveal launch times, penetration times, or times on target.
3 ICBM target verification response delay times.

U

Mark and protect as FOUO.
4 Execution plan program

U

Two-person concept material.
5 MM Targeting Program:    
  a. MM II:    
 
  • (1) MM F target kit:
   
 
  • (a) Command trajectory data sheet

S

1.5.g (X2)

 
 
  • (b) Munitions trajectory data sheet

S

1.5.g (X2)

 
 
  • (c) Monthly climatology sheet

U

 
 
  • (d) Target tape

S

1.5.g (X2)

EWO target tapes are two-person concept material.  Special/Training target tapes are not two-person concept material.
 
  • (2) Master LF data base tape

S

1.5.g (X2)

Handle as two-person concept material
  b. MM III CDB:    
 
  • (1) Operational targeting program tapes

S-FRD

1.5.g (X2)

Two-person concept material.  Engineering version copies are not two-person concept material.
 
  • (2) Master LF data base tape

S

1.5.g (X2)

Handle as two-person concept material
 
  • (3) MOTP data base tape

S-FRD

1.5.g (X2)

Handle as two-person concept material
 
  • (4) Execution Plan Program (EPP)

U

Two-person concept material.
 
  • (5) EPP data base

TS

1.5.g (X2)

Handle as two-person concept material
  c.  HQ AFSPC production programs:    
 
  • (1) MM F OTP.

S-FRD

1.5.g (X2)

 
 
  • (2) MM F verification program

S-FRD

1.5.g (X2)

Two-person concept material.
 
  • (3) Silo-Upgrade Addressing and Verification Program (SUAVE).

S-FRD

1.5.g (X2)

Two-person concept material.
 
  • (4) Strategic Targeting Support Software (SSTS) Programs:
   
 
  • (a) Monitor subsystem

U

 
 
  • (b) Simulator subsystem

U

 
 
  • (c) Missile Trajectory Simulation Program.

S

1.5.g (X2)

 
 
  • (5) Forecast constant generation program.

U

 
6        Program tapes:    
  a. Program Tape, Fig A 13001 (Grd/FL WS-133B)

S

1.5.g (X2)

Tape P/Ns 20032-309-11, -211 and -401
  b. Program Tape, Fig A 13001M (Grd/FL WS-133A-M)

C

1.5.g (X2)

Tape P/N 20264-309-11 pre-ARSIP, ARSIP, P/Ns 20264-309-1 and -21 (SASS)
  c. Fig A 13001M

C

1.5.g (X2)

Tape P/N 20264-309-201 (ILCS) Flight Tape Only).  Pre-ARSIP P/N 20264-309-31.
  d. Wing Code Processing System Master Program Tape CI 0045871

S

1.5.g (X2)

Tape P/N 10803-309-41 (CCOS PROG EXE)
  e. Operational Flight (IMU) Tape, Fig A 17913 and CI 19243.

S

1.5.g (X2)

Tape P/Ns 20208-309-11 and 20346-309-1
  f. CMSC Program Tape, Fig A 13229 (WS-133B)

S

1.5.g (X2)

Tape P/N 10061-309-11
  g. CMSC Program Tape, Fig A 13229M (WS-133A-M).

C

U

1.5.g (X2)

Tape P/N 10079-309-7
  h. Overwrite Program Tape, CI 19230.

C

1.5.g (X2)

Tape information content is UNCLASSIFIED.  Access is CONFIDENTIAL to preclude unauthorized access and tampering due to potential to cause incomplete overwrite.  Tape P/N 20364-309-11.
  i. Certification Program, Fig A 17841.

C

1.5.g (X2)

Tape P/N 10394-309-1 and -11
 
  • j. Operational Ground Tape, MM III Fig A's  17818, and CI 19241 and CI 19250.

S

DECLAS

31 DEC 2007

WS-133A-M, Tape P/N 20149-309-1, -11 (Basic); 20343-309-201, -301, -1, -11 (CDB); 20382-309-1, -11, -21 (HEG).  WS-133B Tape P/N 20151-309-1, -11 (Basic); 20370-309-1 (CBD), -11 (HEG)
  k. Program Tape Fig A 14250

U

 
  l. MAF Encryption Program Tape (SSAS)

S

1.5.g (X2)

Controlled COMSEC Item.  Tape P/N 25-76579-1.
  m. LF Encryption Program Tape (SSAS), USKAF-9, Fig A 17797.

S

1.5.g (X2)

Controlled COMSEC Item.  Tape P/N 20268-309-1.
  n. Overwrite Program Fig A 13231 (ILCS Configuration)

C

1.5.g (X2)

Tape information content is UNCLASSIFIED.  Access is CONFIDENTIAL to preclude unauthorized access and possible tampering due to potential to cause incomplete overwrite.  Tape P/Ns 20294-309-1, -11, and -21.
  o. Operational Ground Program Tape, CI 19236 (ILCS) Configuration) - pre-ARSIP.  ARSIP CI 19236AA

U

ARSIP Tape P/Ns 20283-309-1, -11, -21, and -31
  p. Assembly and Checkout Program Tape, CI 19237 (ILCS Configuration).

U

Tape P/N 20286-309-1
  q. Operational Ground Program Tape, CI 19240 (WS-133A-M) - pre-EEP EEP CI 19240AA.

C

U

1.5.g (X2)

Tape P/Ns 20277-309-1 (GIP) and -11 (MESP) and -21 (EEP)
  r. Operational Ground Program Tape CI 19241 (WS-133B)-Pre-EEP EEP CI 19241AA

C

1.5.g (X2)

Tape P/N 20280-309-1 (GIP) and -11 (MESP) and -21 (EEP)
  s. Operational Flight Program (OFP) Tape, CI 19220

S

1.5.g (X2)

Tape P/Ns 20376-309-1 and -11
  t. MM III OFP Tape CI 19243.

S

1.5.g (X2)

Tape P/N 20289-309-1
  u. Operational Ground Program Tape, CI 19244 (ERCS/ILCS).

U

Tape P/N 20241-309-1.
 
  • v. Operational Flight Program Tape, Fig A 19277AA CPCI0019275, CPCO 19277.

S

1.5.g (X2)

Tape P/Ns 20099-309-5 and 20274-309-1, -201, and -211
 
  • w. Flight Program Constants Tape, CI 19275AA, CI 19277AA, CPCI0019275, CPCI 19277.

S

1.5.g (X2)

Tape P/Ns 20379-309-1 (OP) and -201 (OTL) (MK12); 20292-309-1 and 201 (MK12A); 20379-309-11 and 211 (SRV); 20292-309-11 and 211 (SRV).
 
  • x. SPCS Application Program CI 0045872.

U

Tape P/N 10806-309-41
  y. MM Application Program CI 0045874.

U

Tape P/N 10812-309-61
  z. MMIII GRP Operational Ground Program WS-133AM, WS-133B CI S-133-19251

U

No separate tape.  GRP OGP combined both AM and B system programs into a single program that supports both configurations.  CPIN No. 82A-NS50/LGM30G-F001-00D.
  aa. MMIII GRP Operational Flight Program WS-133AM, WS-133B CI S-133-19252.

U

No separate tape.  CPIN No. 82A-NS50/ LGM30G-F002-00D.
  ab. MMIII GRP Operational Ground Flight Program CI S-133-19250

U

Tape P/N 20426-309-().  OGP/OFP combined for both AM and B Systems.
  ac. MMII GRP MK12A Flight Program Constants Tapes CI S-133-19253.

S

1.5.g (X2)

Tape P/N 20429-309-() (Type I), DC300 cartridge magnetic tape for the Operational Program.  Tape P/N 20429-309-() (Type 2) DC300 cartridge magnetic tape for the Operational Training Launch program at VAFB. 

CPIN No. 82A-NS50/MK12A/F001-00A (Operational)

CPIN No. 82A-NS50/MK12A/F002-00A (Operational Training Launch)

  ad. MMIII GRP MK12 Flight Program Constants Tapes CI S-133-19254

S

1.5.g (X2)

Tape P/N 20433-309-() (Type 1) DC300 cartridge magnetic tape for the Operational program.  Tape P/N 20433-309-() (Type 2) DC 300 cartridge magnetic tape for the Operational Training Launch program at VAFB. 

CPIN No. 82A-NS50/MK12/F001-00A (Operational).

CPIN No. 82A-NS50/MK12/F002-00A (Operational Training Launch

7. Execution/Targeting Software and Databases    
  a. Console Operations Program (COP EXE) CSCI 0036000

U

WSP main program - provides command, control, communication.  P/N C006839-02
  b. COP Database, CSCI 0036000

U

COP screen templates, etc.  P/N C006839-03
  c. COP User ROM (Firmware), CSCI 00360; COP FDM Format CSCI 0036000

U

WSP firmware.  P/Ns C006839-04 and C006839-05, respectively.  Included in initial Computer Memory Security (CMSC).
  d. COP Boot ROM, CSCI 0036000

U

WSP boot firmware, P/N C006839-06.  Included in initial CMSC.
  e. Execution Plan Program (EPP) Exe.  CSCI 19291

U

Provides execution plan processing.  P/N 103-1929111-01
  f. MOTP3 Exe.  CSCI 19215

S-FRD

1.5.g (X2)

The MOTP3 provides targeting processing
  g. Trajectory and Missile Parameters (TAMP)

S-FRD

1.5.g (X2)

The TAMP provides trajectory and missile parameters
  h. Operational Ground Program Offload Tape

U

Loaded to the WSCE for transfer to the LF.  Executable in the MM flight computer, not in the console
  i. EPP/Message Analysis (MA) Databases (DBs)

TS-FRD SIOP-ESI

Cat 10

1.5.g (X2)

The EPP portion provides the execution plan database (DB) for the EPP and COP.  The MA portion provides the database for the COP.  TOP SECRET for training values, TOP SECRET SIOP-ESI for actual values as provided by OL-B, HQ AFSPC/DO.
  j. MOTP3 DB

S-FRD

1.5.g (X2)

Targeting database for the MOTP3.
  k. Force Direction Message (FDM) Format DB

U

Format database for force direction messages.
  l. TCI/EPCI DB (Also Case Image Data)

S

to

TS-FRD SIOP-ESI

Cat 6 and 10

1.5.g (X2)

Target cases provide case input data for targeting and execution plans.  Classification is dependent upon targeting data and number of sorties as provided by OL-B,  625 MOF/TAB.  For upload via Floppy diskette, diskette retain original classification if write-protect tab is set during upload.
  m. Tech Order DB

U

to

TS-FRD SIOP-ESI

Cat 6 and 10

1.5.g (X2)

Technical order database uploaded to COP via Floppy disk.  Floppy diskette remains UNCLASSIFIED if write-protect tab is set during upload, otherwise diskette assumes the highest classification of information in the system.
  n. Transmission Integrator (TI) CSCI 00500

U

Prepares messages for transmission over different HA communications systems.
  o. Communications Integrator/Backup (CI/CIB) CSCI 00400

U

Prepares messages received over different HA communications systems for processing by the MP.  As backup, transfers incoming message text to WSCE for printing.
  p. Message Processor (MP) CSCI 00300

TS-SIOP-ESI,

Cat 6 and 10

1.5.g (X2)

Performs rapid message processing functions
  q. Code Change Upload Floppy diskette (CMSC Control words)

U

Floppy disk is generated at the WCPS for upload at the LCC, NSA supplied control words for the computer memory security check are encrypted.  Floppy diskette remains Unclassified if write-protect tab is set during upload.
8 Trainer Software    
  a. Operations Trainer Software    
 
  • (1) RSX-11M (RY, LE)

U

PDP-11/34 operating system.  Resident on diskpack.
 
  • (2) C3 Simulation Program

U or S

1.5.g (X2)

Simulates AFSATCOM, SLFCS, and SACDIN communications system functions, Also used to generate and execute instructor messages and system parameters that can be classified SECRET.  UNCLASSIFIED or SECRET depending on level of information loaded.  Resident on diskpack
 
  • (3) C3 Instructor Data (RY, LE)

U or S

1.5.g (X2)

Comprised of instructor databases that are either UNCLASSIFIED or SECRET.  Resident on diskpack.
 
  • (4) Status and Command Simulation (RY)

U or S

1.5.g (X2)

Simulates operational status and command systems.  Operates on the MPC-1624 computer.  Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET.  UNCLASSIFIED or SECRET depending on the level of information loaded.  Resident on floppy diskettes.
 
  • (5) Auxiliary Program (RY)

U or TS

1.5.g (X2)

Operates on the MPC 1624 computer.  Basic software is UNCLASSIFIED however it is used to generate instructor databases that can be classified TOP SECRET.  Resident on floppy diskettes.
 
  • (6) Instructor Data (RY)

U or TS

1.5.g (X2)

Comprised of instructor databases that are UNCLASSIFIED, SECRET, or TOP SECRET.  Resident on floppy diskettes.
 
  • (7) VMS (LE/PH)

U

VAX-11/750 and 751 operating system.  Resident on diskpack.
 
  • (8) Simulation Program (LE)

U to TS

1.5.g (X2)

Simulates operational status and command systems.  Operates on VAX-11/751 computer.  Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET and execution data that can be TOP SECRET.  Resident on disk pack.
 
  • (9) MS-DOS (LE)

U

Instructor terminals operating system.
 
  • (10) Instructor Data (LE)

U

to

TS

1.5.g (X2)

Comprised of instructor databases that are either UNCLASSIFIED, SECRET or TOP SECRET.  Resident of floppy diskettes.
 
  • (11) Simulation Program (PH)

U to TS

1.5.g (X2)

Simulates operational status and command systems.  Operates on VAX-11/750 computer.  Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET and execution data that can be TOP SECRET.  Resident on diskpack.
 
  • (12) Instructor Data (PH)

U to TS

1.5.g (X2)

Comprised of instructor data bases that are either UNCLASSIFIED, SECRET or TOP SECRET.  Resident on diskpack.
  b  Procedures Trainer Software    
 
  • (1) MPT-COP
  • 82J-REACT/COP–F001–06A 
  •    CSCI:  00360000.12

U

Used in the AM System RY MPT and MEPT.  Resident on RSE.
 
  • (2) MPT-COP
  •    82J-REACT/COP-F001-07A
  •    CSCI:  0036000.22

U

Used in the B System LE MPT and MEPT.  Resident on RSE.
 
  • (3) MPTCP
  •    84L-GSQT14/MPTCP-F001-00A  CSCI:  0036002

TS

1.5.g (X2)

Used in the AM System RY MPT, B System LE MPT and MEPT.  Same as operational EPP/MA database, except contains training values.  Part of MPTCP program - resident on RSE.
 
  • (4) HAC/RMPE, executable
  •    TK-70 magnetic tape;
  •    P/N 2592957-02

TS

1.5.g (X2)

Used in the AM System RY MPT, B System LE MPT and MEPT. 
 
  • (5) Audio Simulation, 3.5” floppy disc P/N 25-92957-03

U

to

TS

1.5.g (X2)

Used in the AM System RY MPT B System LE MPT.  Classified upon use.
 
  • (4) VMS

U

VAX operating system resident on RSE.
 
  • (5) MS-DOS

U

Audio controller computer operating system resident on RSE and downloaded to audio buffer.  Also on floppy diskettes.
 
  • (6) TO database

U

Resident on RSE.
 
  • (7) Instructor training records

U

Resident on RSE and on tape.
 
  • (8) Simulated load disks

U

to

TS

1.5.g (X2)

 
 
 
  • (9) MPT diagnostic data

U

Data generated to test the floppy disk drive.  Resident on diskette

 
 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

This page intentionally left blank. 

 

SECTION XX 

RAPID MESSAGE PROCESSING 
 


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1146  
 
 
 

MEMORANDUM FOR DISTRIBUTION 

FROM: OO-ALC/CC

       7981 Georgia St.

       Hill AFB, UT 84056-5824 

SUBJECT:  Change 1, ICBM Security Classification Guide (SCG), 30 Sep 97  

1.  The changes which comprise change 1 to the current ICBM SCG are identified below. They should be posted in the SCG and this letter retained in the SCG.

(a)  Attachment 1, page 34, paragraph 3.e.(2)  to read: 

       Number of RVs on an operational                          S-FRD                      See 3.e.(5)

       missile in any given LF                                         1.5.g (X2) 

(b)  Attachment 1, page 34, add sub-paragraph 3.e.(5) 

       For the 90th Space Wing only,                                 U                              START 1 compliance

       the fact that any LF has only      

       one RV, or that it is SRV.  

(c)  Attachment 1, page, 50, paragraph 1.h.(3).(f).(6) to read: 

       Test Launch site coordinates                                  U or C                       UNCLASSIFIED when World

                                                                                      1.5.g (X2)                  Geodetic System (WGS)

                                                                                                                         coordinates for the LF are not

                                                                                                                         provided. CONFIDENTIAL 

                                                                                                                         when WGS coordinates are

                                                                                                                         provided. 

(d)  Attachment 1, page 50, paragraph 1.k.(1) to read: 

       If launch site WGS coordinates included               C                               See Section XIII. 

(e)  Attachment 1, page 60, paragraph 7.a.(1) to read:

      

       WGS coordinates (>, S)                                           U or C                     UNCLASSIFIED when given

                                                                                       1.5.g (X2)                 no more precisely than the

                                                                                                                         closest minute.

(f)  Section V, Distribution, page 19 to read:

     HQ USSTRATCOM

        J005, Ste 1H9, -6005      

        J312/331/334/362/441/443, Ste BA3, -6300

        J511/ 523/541, Ste 2E8, -6500

        J613, Ste 2B9, -6600

      901 SAC Blvd

      Offutt AFB NE 68113-xxxx

(g)  Section V, Distribution, page 18 to read:

   

      HQ AFSPC/

             DOM         -4180

             DOTO       -4240

             DRM         -4670

             LGM         -4470

             SCOMG    -4400

             SEWM      -4260

             SFPON      -4560

      150 Vandenberg St, Ste 1105

      Peterson AFB, CO 80914-xxxx     

(h)  Section V, Distribution, page 13 to read: 

       791 MXS/CC

       319 SPS/SPAI

       MAIL ALL COPIES TO

       450 G St,  STE 321

       Grand Forks AFB, ND 58205-6023 

       341 LG/CC

              LSS/CC             

              MXS/CC

              OG/CC

       43 SPS/SPAII

       MAIL ALL COPIES TO

       341 LG, BLDG 500, STE 148, 2177 St N.

       Malmstrom AFB, MT 59402-7538              

(i)  Section V, Distribution, page 14 to read: 

      90 LG/CC

           LSS/CC

           MXS/CC

           SSS/SPAI

     MAIL ALL COPIES TO

     5305 Randall Ave

     Francis E Warren AFB, WY 82005-2274 

     91 LG/CC

          LSS/CC

         MXS/CC

         OS

         5 SPS/SPAI

     MAIL ALL COPIES TO

     5 MSS/MSIAC, 220 Peacekeeper PL

     Minot AFB, ND 58705-5000 

(j)  Section V, Distribution, pages 16 and 17 delete the following: 

     ‘DefenseTechnical Information Center ‘ and ‘DTICÂ’

      Cameron Station

      Alexandria, VA 22304-6100/-6145 
 

(k)  Section V, Distribution, page 16 add: 

                “ Defense Logistics Agency

                    8725 John J Kingman  Road

                    STE 2533

                    Fort Belvoir, VA 22060-6221” 

(l)  Section V, Distribution, page 14 to read:

     

      Change AFLC to AFMC

      Wright Patterson AFB, OH 45433-5260

          MME

          SFX

          SCWM 

(m)  Section V, Distribution, page 20 change as follows: 

        Under OO-ALC change 75 SFS/SFAI TO 75 SFS/SFA 

(n) Section V, Distribution, page 15 change Capital Hill Area, DIS location Alexandria to; 

        Greater Baltimore/Washington, D.C.

        Defense Security Service Location

        Hoffman Building

        2461 Eisenhower Avenue, Room 744

        Alexandria, VA 22331-1000 

(o)  Section V, Distribution, page 15 change Central Region, DIS location Chicago to: 

        Midwest

        Defense Security Service Location

        610 South Canal Street, Room 800

        Chicago, IL 60607-4599 

(p)  Section V, Distribution, page 15 change Central Region, DIS location Irving to: 

        Texas/Oklahoma

        Defense Security Service Location

        5800 E. Campus Circle Drive

        Suite 110A

        Irving, TX 75063-2739 

(q)  Section V, Distribution, page 20 change Northeast Region, DIS location to:

        Mid-Atlantic

        Defense Security Service Location

        770 Wood Lane

        Suite 12

        Mt. Holly, NJ 08060-3802 
 

(r)  Section V, Distribution, page 21 change Pacific Region, DIS location to: 

        Southern California

        Defense Security Service Location

        One World Trade Center

        Suite 622

        Long Beach, CA 90831-0622 

(s)  Section V, Distribution, page 22 change Southeastern Region, DIS location to: 

       Gulf Coast

       Defense Security Service Location

       2300 Lake Park Drive

       Suite 250

       Smyrna, GA 30080 

2.  Point of contact is Mr. Milton Johnson, LMEA, DSN 777-7799, FAX 777-4643. 
 
 

ORIGINATING OFFICIAL:                                                     COORDINATING OFFICIAL: 
 
 
 
 

CARL B. OVERALL, Col, USAF                                             TIMOTHY G. HARDY, Lt Col, USAF

Program Director                                                                        Commander, 75th Security Forces Squadron

ICBM System Program Office 
 
 
 
 

APPROVING OFFICIAL: 
 
 
 
 

RICHARD H. ROELLIG, Major General, USAF

Commander 
 
 


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1146  

DEPARTMENT OF THE AIR FORCE

HEADQUARTERS OGDEN AIR LOGISTICS CENTER (AFMC)

HILL AIR FORCE BASE, UTAH

25 Jan 2001 
 
 

MEMORANDUM FOR DISTRIBUTION 

FROM: OO-ALC/LM

                    6014 Dogwood Avenue

                    Hill AFB UT 84056-5816 

SUBJECT:  Change 2, ICBM Security Classification Guide (SCG), 30 Sep 97 

1. The changes which comprise change 2 to the current ICBM SCG are identified below. They should be posted in the SCG and this letter retained in the SCG. 

      (a) Section IV, page 11, add a new paragraph ac: SERV. Safety Enhanced Reentry Vehicle.

             Renumber remaining paragraphs accordingly. 

      (b)  Section V, Distribution, page 14 add: 

             90 OG/CC

             91 OG/CC 

      (c)  Attachment 1, Section XIV, page 67, paragraph c change XOFS to XONO. 

      (d)  Attachment 2, Section X, page 31, paragraph c change XOFS to XONO. 

      (e)  Section V, Distribution, page 14 add: 

             HQ AFDO/CC

             1720 Air Force Pentagon

             Washington DC 20330-1720 

             HQ AFHRA/RSA

             600 Chennault Circle

             Maxwell AFB AL 36112 

      (f) Section V, Distribution, page 16 add: 

             Defense Technical Information Center

             8725 John J. Kingman Road, Suite 944

              Fort Belvoir VA 22060-6218 

      (g)  Section V, Distribution, pages 15, 20, 21, and 22 delete the following: 

             AFWL/SP and all DSS locations 

      (h) Section V, Distribution, page 14 delete the following: 

             AFSAA/SAI 

      (i) Section V, Distribution, page 14 to read: 

             HQ AFMC/SFXP

             Bldg 266, Rm N208

             4225 Logistics Ave

             Wright Patterson AFB OH 45433-5760 

             HQ AFMC/XRS, STE 6

             4315 Chidlaw Rd

             Wright Patterson AFB OH 45433-5006 

             ASC/SP, Rm 103A

             1801 10th ST

             Wright Patterson AFB OH 45433-6825 

             FASTC/SP, STE 1, Bldg 11A, Rm 013

             1970 3rd St

              Wright Patterson AFB OH 45433-6504 

             HQ USAF/XOFI

             1340 Air Force Pentagon

             Washington DC 20330-1340 

      (j) Section V, Distribution, page 22, change as follows: 

             Was: 

             TRW Strategic Systems Division

             Systems Integration Group

             1104 Country Hills Drive

             Ogden UT 84403-2400 

             Is: 

             TRW ICBM Systems

             ATTN: Security

             P.O. Box 804

             Clearfield UT 84089-0804 

      (k) Add attachment 1 to appropriate sections of the SCG as noted. 

      (l) Add attachment 2 to appropriate section of the SCG. 

2. The above changes consist of revising the IMPSS security and Hardware Classification sections and updating the distribution list. The information contained herein is not to be released on the Internet. 

3. Point of contact is Mr. Milton Johnson, LMEI, DSN 777-6933, FAX 777-4643. 
 
 
 

COORDINATING OFFICIAL: ORIGINATING OFFICIAL:

WARREN L. KEITHLEY, Major, USAF  CARL B. OVERALL, Colonel, USAF

Commander, 75th Security Forces Squadron  Program Director

      ICBM System Program Office 

Attachments:

1. ICBM Security Classification Guide Weapon System Security Section

2. ICBM Security Classification Guide Attachment 1 (Minuteman), Section II 

      APPROVING OFFICIAL: 
 
 

SCOTT C. BERGREN, Major General, USAF

Commander, Ogden Air Logistics Center