Attachment3SecurityClassificationGuide.pdf

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B-1 WEAPON SYSTEM

PROGRAM

SECURITY CLASSIFICATION GUIDE

1 October 1997 Revised 15 July 2001

Revised September 2005 Revised 1 June 2011

OKLAHOMA CITY AIR LOGISTICS CENTER (OC-ALC)

B-1 SUSTAINMENT DIVISION/GKB

TINKER AFB OK 73145

THIS GUIDE SUPERSEDES B-1 PROGRAM SECURITY CLASSIFICATION GUIDE,

DATED 1 OCTOBER 1997, REVISED 15 JULY 2001, REVISED SEPTEMBER 2005.

DISTRIBUTION LIMITED TO DOD EMPLOYEES AND DOD CONTRACTORS ONLY.

OTHER REQUESTS SHALL BE REFERRED TO OC-ALC/GKB, 3001 STAFF DRIVE,

SUITE 2AD77A, TINKER AFB OK 73145.

DESTRUCTION NOTICE: DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THIS GUIDE.

(LOCAL REPRODUCTION AUTHORIZED)

SECURITY CLASSIFICATION GUIDE 1 October 1997 B-1 Program Revised 15 July 2001 Revised September 2005 Revised 1 June 2011

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TABLE OF CONTENTS

Section Page

I General Instructions 1

II Release of Information 4

III Acronyms and Definitions 6

IV Funding, Procurement, and Production 10

V Administrative Data 11

VI Aircraft System 12

VII Propulsion Subsystem 23

VIII Offensive Avionics Subsystem 25

IX Defensive Avionics Subsystem 34

X General Avionics Subsystems 44

XI Controls, Displays, and Crew Accommodations 46

XII System Development Testing 47

XIII Ground Support Equipment 49

XIV Simulators and Training Equipment 50

XV Operational Data 51

XVI Towed Decoy System 54

XVII Sniper Targeting Pod 55

XVIII Distribution List 56

SECURITY CLASSIFICATION GUIDE 1 October 1997 B-1 Program Revised 15 July 2001 Revised September 2005 Revised 1 June 2011

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Section I

GENERAL INSTRUCTIONS

1. Purpose. To provide instructions and guidance on the classification and proper distribution of information involved on the B-1 program.

2. Authority. DoD 5200.1-R/AFI 31-401. Cite this guide as the basis for classifying, downgrading, or declassifying information about the B-1 Program.

3. Office of Primary Responsibility (OPR). This guide is issued by the B-1 System Program

Manager (SPM), B-1 Sustainment Division, 3001 Staff Drive, Suite 2AD77A, Tinker AFB OK 73145-6001; telephone: commercial (405) 736-2001, DSN 336-2001.

4. Classification Recommendations. Send completely documented and justified recommendations to the OPR if the security classifications or declassification instructions in this guide impose impractical requirements or when scientific or technological changes in the state of the art indicate a need for changes. Pending final decision, handle and protect the information at the highest of the present or the recommended classifications. All users of this guide are encouraged to assist in improving and maintaining the currency and adequacy of this guide.

5. Classification Currency.

a. Changes to this guide will be effected by the issuance of a letter, subject: Letter Change No. __ to the B-1 Security Classification Guide, 1June 2011. This letter will indicate the appropriate change(s) and will constitute the authority for such change(s). Upon receipt of a letter change, the appropriate change(s) will be made and the letter of authority will be inserted in back of the guide.

b. Changes in this guide identify specific downgrading declassification action. Changes in classification are identified by underlining the classification for each appropriate item. During routine use, review information classified under the previous security classification guide and remark in accordance with this security classification guide.

6. Reason for Classifying: The reason for classifying information is in accordance with Executive

Order (EO) 13526. The category for classification, as identified through the guide, is as follows:

Category 1.4g: Vulnerabilities or capabilities of systems, installations, infrastructure, projects, plans, or protection services relating to the national security.

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Section I (Continued)

7. Explanation of Declassification Instructions: Information classified by this guide has a specific date or event for declassification that is 10 years or less from the date of this guide. Information that must remain classified longer than 10 years is exempted IAW EO 13526 Section 1.4:

…unauthorized disclosure could reasonably be expected to cause identifiable or describable damage to the national security: (a) military plans, weapons systems, or operations. Information exempted will remain classified for 25 years from the date of the original decision (DOOD) as indicated throughout this guide, unless declassified earlier.

8. Prior Declassification Instructions: Information derivatively classified by the previous guide with a declassification instruction of OADR will remain classified for 25 years from the date of origin of the source document unless declassified earlier by this guide. Only information that has been declassified earlier by this guide will be remarked to reflect the new declassification date when used.

9. Use of Distribution Statement: In accordance with DoDD 5230.24, all technical data, classified and unclassified, shall be marked with a distribution statement to control secondary distribution. All users shall place the respective distribution statement on the cover or first page of technical data derived from the B-1 program:

a. Technical data requiring Distribution Statement D; utilize the following statement -

"Distribution authorized to the Department of Defense and U.S. DoD contractors only:

Administrative or Operational Use, 1 November 1994. Other requests shall be referred to the B-1 System Program Manager (SPM)."

b. For technical data requiring Distribution Statement F; utilize the following statement -

"Further dissemination only as directed by the B-1 SPM, OC-ALC/GKB, 3001 Staff Drive, Suite 2AD77A, Tinker AFB OK 73145-6001, or higher DoD authority."

For further guidance refer to DoDD 5230.24 , Distribution Statements on Technical Documents, or the B-1 Program Protection Plan (PPP).

10. Export Controlled Information: In addition to required distribution statements on DoD technical information, export controlled markings may also apply to classified and unclassified technical documents. For further guidance, refer to AFI 61-204, Disseminating Scientific and Technical Information, or DoDD 5230.24, Distribution Statement on Technical Documents.

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Section I (Continued)

11. Other Applicable Security Classification Guides:

a. Joint Direct Attack Munitions (JDAM) SCG OPR – AAC/YH, Eglin AFB FL.

b. AF Satellite Communications (AFSATCOM) System SCG

OPR - SSD/SPI, Los Angeles CA.

c. Expendable Airborne Infrared Countermeasures (IR Decoys and Devices) Joint Security Classification Guide OPR – NAVAIR Depot Jacksonville FL.

d. HAVE QUICK/II/IIA/Saturn. SCG

OPR - ESC/TGH, Hanscom AFB MA.

e. HAVE SYNC SCG OPR - ESC/TCV, Hanscom AFB MA.

f. Joint Air to Surface Standoff Missile (JASSM) SCG

OPR - AAC/YV, Eglin AFB FL.

g. Joint Tactical Information Distribution System (JTIDS) SCG OPR – ESC/DIGR, Hanscom AFB MA.

h. Air Force AN/ALE-50(V) Towed Decoy System SCG

OPR WR-ALC/LN-1, Robins AFB GA.

i. Air Force Support of Global Grid Minimum Essential Emergency Communications Network (MEECN) Program SCG OPR - ESC/NDM, Hanscom AFB MA.

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Section II

RELEASE OF INFORMATION

1. Public Release.

a. The fact that this guide shows certain details of information as unclassified does not permit automatic public release of them. Proposed public disclosures of unclassified information regarding the B-1 Program shall be submitted to 72ABW/PA, Tinker AFB OK 73145, telephone 405-739-2026, for review, a minimum of 45 days prior to the date of the actual release being proposed.

b. The term "information" applies, but is not limited, to: articles, speeches, photographs, brochures, advertisements, displays, and presentations on any phase of the B-1 Program.

c. Defense contractors and other agencies must screen all information they submit for determination of releasability to ensure it is both unclassified and technically accurate and non-proprietary. The letter of transmittal must certify this review. Copies of the material may not be released outside official channels until the review process is complete. If information found during the review process is suspected as classified, notify all holders of the document as to the degree of protection required. When doubt exists concerning the classified status of a proposed release pertaining to the program, B-1 Sustainment Division makes the final decision. The material submitted for review must include a valid suspense date, if applicable.

d. Only information reviewed and certified for public release may be released. Information for public release that is revised or developed after initial certification must be submitted for review and further processing as outlined in paragraphs a and b above.

e. Material which requires an export license will not be entered into security and policy review channels for public release approval in order to circumvent the licensing requirements of the Departments of State and Commerce.

f. Obtain approval for planned or contemplated visits of public media representatives from

B-1 Sustainment Division and 72ABW/PA.

2. Release of Program Data on the World Wide Web. Extreme care must be taken when considering information for release onto publicly accessible or unprotected World Wide Web Sites.

In addition to satisfying all of the aforementioned approval provisions, owners and/or releasers of information proposed for such release must ensure that it is not susceptible to compilation with other information to render sensitive or even classified data in the aggregate. The search and data mining .

SECURITY CLASSIFICATION GUIDE 1 October 1997 B-1 Program Revised 15 July 2001 Revised September 2005 Revised 1 June 2011

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Section II

RELEASE OF INFORMATION (Continued) capabilities of Web technology must be assessed from a risk management perspective. If there is any doubt, do not release the information.

3. Release of Classified and Unclassified Information to Foreign Governments or Their

Representatives. In accordance with AFI 16-201, Foreign Disclosure of Classified and Unclassified Military Information to Foreign Governments and International Organizations, advise a foreign national soliciting or requesting classified and/or unclassified USAF information to request it through their embassy in Washington DC. Any military activity or contractor receiving such a request from a foreign government, foreign contractor, or representative thereof must forward the request to 448 MSUG/GBMSI – FDO, 3501 D Avenue, Building 201W, Room 22, Tinker AFB OK 73145-3352. Any military activity desiring to release classified and/or unclassified information to a foreign government, foreign contractor, or representative thereof, must forward the request to 448 MSUG/GBMSI - FDO, according to AFI 16-201. Defense contractors desiring to release classified and/or unclassified information controlled by the International Traffic in Arms Regulation (ITAR) to a foreign government, foreign contractor, or representative thereof must request a munitions export license from the Department of State, Office of Defense Trade Control, PM/DTC Room 200, SA-6, Washington DC 20522.

4. Release of Unclassified Technical Information (Not Approved for Public Release) to US

Citizens Residing in a Foreign Country. A defense contractor must either obtain the approval of the OPR (B-1 Sustainment Division) 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 that requires an export license may not be entered into security review channels for public release approval in order to circumvent the licensing requirements for the Departments of State or Commerce.

5. Release of Collateral Intelligence to US Contractors: Intelligence information will not be released to US Contractors without written release approval of the Senior Intelligence Officer (SIO) or designated representative. The SIO for the B-1 Sustainment Division is OC-ALC/XP2. No Government official shall authorize contractor use of intelligence information on US contracts or release to subcontractors without express written authority from the SIO. Requests for intelligence material shall be submitted through the Program/Contract Manager to the Intelligence Office, OCALC/XP2, 3001 Staff Drive, Tinker AFB OK 73145-3314.

SECURITY CLASSIFICATION GUIDE 1 October 1997 B-1 Program Revised 15 July 2001 Revised September 2005 Revised 1 June 2011

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Section III

ACRONYMS AND DEFINITIONS

1. Explanation of Terms. The following is a list of abbreviations and designations used in this guide.

A/A Air-to-Air

ACC Air Combat Command

AFI Air Force Instruction

AFMC Air Force Materiel Command

A/GND Air-to-Ground

ALC Air Logistics Center

ANDVT Advanced Narrow-band Digital Voice Terminal

AOJ Angle-on-Jam

ASC Aeronautical Systems Center

C Confidential

CCI Controlled Cryptographic Item

CEP Circular Error Probable

DoD Department of Defense

DOOD Date of Original Decision

DT&E Developmental Test and Evaluation

DTU Data Transfer Unit

EA Electronic Attack (Formerly ECM)

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Section III (Continued)

ECM Electronic Countermeasures

EMP Electromagnetic Pulse

ERP Effective Radiated Power

FOT&E Follow-on Operational Test & Evaluation

GPS Global Positioning System

HOJ Home-on-Jam

HRGM High Resolution Ground Map

IAW In Accordance With

IFF Identification, Friend or Foe

ILS Integrated Logistics Support

IOT&E Initial Operational Test and Evaluation

IR Infrared

ITAR International Traffic and Arms Regulation

JEM Jet Engine Modulation

JTIDS Joint Tactical Information Distribution System

LPI Low Probability Intercept

LRU Line Replaceable Unit

NA Not Applicable

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NAF Number Air Force

OC-ALC Oklahoma City Air Logistics Center

OC-ALC

448 MSUG/GBMSI Foreign Disclosure Office

72ABW/PA Public Affairs Office

72ABW/IPI Information Protection, Tinker AFB

OPR Office of Primary Responsibility

ORS Offensive Radar System

PPP Program Protection Plan

PPU Precision Position Update

RAM/RAS Radar Absorption Material/Radar Absorption Structure

RCS Radar Cross Section

Representative of a Citizens or nationals of the U.S. or immigrant aliens who, in Foreign Interest their individual capacity, or on behalf of a corporation (whether as a corporate officer of official or as a corporate employee who is personally involved with the foreign entity), are acting as representatives, officials, agents, or employees of a foreign government, firm, corporation, or person.

RF Radio Frequency

RFS/ECMS Radio Frequency Surveillance/Electronic Countermeasures System

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RSAM Repeater Swept Amplitude Modulation

S Secret

SAR Synthetic Aperture Radar

SCG Security Classification Guide

TACAN Tactical Air Navigation

TF Terrain Following

TREE Transient Radiation Effects on Electronics

TWF Tail Warning Function

U Unclassified

VGS Velocity Gate Stealer

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Section IV

FUNDING, PROCUREMENT, AND PRODUCTION

INFORMATION REVEALING

CLASS/

REASON

DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

1. Program cost information U NA

2. Quantities and delivery schedules

U NA

3. Quantities and delivery schedules of aircraft subsystem and/or major aircraft components

U NA

4. Critical milestone plan including calendar dates and a delineation of prerequisite events

U NA

5. Program master schedule U NA

6. Planning or programming U e.g., budgeting or funding info NA Any other information U NA

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Section V

ADMINISTRATIVE DATA

Guidance on this page applies to all areas EXCEPT for any effort involving Special Access activities or other special security activities. For those cases, obtain classification guidance from that effort's SCG or security office.

DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

1. A complete list of contractors / subcontractors

U NA

2. Relationship between contractor / subcontractor and/or between contractor and government agencies

U See

Remarks

Unclassified unless classified by specific program SCG

NA

3. Company/Air Force project number/work unit titles and numbers/Air Force Project Element number

U NA

4. Contract numbers U NA

5. Contract model designations U NA

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Section VI

AIRCRAFT SYSTEM

DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

1. Specific Performance

a. Speed/altitude envelope U NA

b. Maximum un-refueled range

U NA

c. Basic mission range NA

(1) Climb U NA

(2) Cruise U NA

(3) Descents U NA

(4) Accelerations U NA

d. Combat ceiling U NA

e. Takeoff distance U NA

f. Landing distance U NA

g. Terrain following minimum altitude

U NA

2. Physical Characteristics:

a. Length, height, wing span, flight weight, takeoff weight, taxi weight, and landing weight

U NA

b. Weight empty, basic weight, operating weight

U NA

c. Fuel capacity U NA

3. Specific fuel consumption required for operation with respect to aircraft flight time and distance

U D

4. External configuration U D

5. Airframe Structural Design U D

6. Reliability

a. Operational impact analysis of information revealing a degradation of the fleet's ability to perform its assigned operational mission

S/1.4g 1 October

D

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Section VI (Continued)

DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

b. Any information which does not reveal a degradation of the fleet’s ability to perform its assigned operational mission

U D

7. Survivability/vulnerability

a. Survivability (nuclear and non-nuclear) pre-launch, en-route, missile launch area, gravity bomb release area and recovery route survivability

S/1.4g 1 October

Applies to data that reveals aircraft system survivability in the context of an identified threat scenario that includes mission objectives, threat definition, and encounter probabilities. Survivability info that identifies and describes intelligence data will be classified consistent with the source document from which the data are extracted.

D

b. Vulnerability (nuclear and non-nuclear)

C/1.4g 1 October

Applies to data relating to overall aircraft system vulnerability. Vulnerability information, which details weapons effects of specific threats, will be classified consistent with documents from which the data are extracted.

D

c. Nuclear Effects Requirements/Response

(1) Blast (gust and overpressure)

(a) Specification nuclear blast pulses

See

Classify IAW AFNW SCG F

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

(b) Nuclear gust loads (i.e., bending moments, shears, torsion’s) derived from the specification or other threat gust pulses

U D

(c) Factors of safety based on the loads

U D

(d) Gust velocities that reveal the capability of the structure, based on the compiled loads and factors of safety

C/1.4g 1 October

D

(2) Nuclear Thermal Radiation

(a) Specification thermal pulse

S/1.4g 1 October

F

(b) Temperature data based on the specification or other threat pulses

U D

(c ) Margins and factors of safety based on the temperature data

U D

(d) Thermal fluences, that reveal the capability of the structure, based on the compiled temperatures and factors of safety

C/1.4g 1 October

D

(e) Thermal fluences representing the vulnerability of the system to the specification or other specific threat warhead yields

S/1.4g 1 October

F

(3) Nuclear blast overpressure

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

(a) Specification blast overpressure pulse

S/1.4g 1 October

F

(b) Equivalent static loads based on the specification or other threat pulses

U D

(c) Margins and factors of safety based on the loads

U D

(d) Free field overpressures that reveal the capability of the structure, based on the loads and factors of safety

S/1.4g 1 October

F

(e) Overpressure pulses representing the vulnerability of the system to the specification or other specific threat warheads

S/1.4g 1 October

F

(f) Thermal fluences representing the vulnerability of the system to the specification or other specific threat warhead yields

S/1.4g 1 October

F

(4) Electromagnetic Pulse

(EMP)

(a) Specification EMP pulse

S/1.4g 1 October

F

(b) Skin current data based on the specification or other threat EMP pulses

U D

(c) Internal wire and surface currents based on the skin current data

U D

(d) Equipment hardness based on analysis data, test data, and equipment description

U D

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(e) Design margins based on internal, wire and surface currents, and equipment hardness

U D

(f) Compilations of EMP hardness data that reveal system vulnerability to external EMP fields

C/1.4g 1 October

D

(g) EMP time and frequency domain pulses that represent the aircraft vulnerability to the specification or other specified threats

C/1.4g 1 October

D

(5) Transient radiation effects on electronics (TREE) vulnerability data

(a) Specification TREE levels

S/1.4g 1 October

F

(b) Component TREE test and analysis data and circuit descriptions not associated with the specification and which do not reveal specification levels

U D

(c ) Component failure and hardness levels derived from the test data, analysis data, and circuit descriptions

U D

(d) Equipment hardness levels derived from component hardness levels

U D

(e) Compilations of component and equipment TREE hardness data that establish system vulnerability

S/1.4g 1 October

F

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

(f) Equipment and component design margins for TREE from which the specification levels can be derived directly from the margins using unclassified data

S/1.4g

1 October

F

(g) TREE levels representing the vulnerability of the system to the specification in other specific threat warheads

S/1.4g 1 October

F

d. Non-nuclear effects requirements/response

(1) Component vulnerability data expressed as a function of fragment or projectile mass and velocity

U D

(2) Compilations of component vulnerability data that establish system vulnerability to fragment or projectile masses and velocities

C/1.4g 1 October

D

(3) Vulnerability data that establish system vulnerability to a specific threat and include a description of that threat

S/1.4g 1 October

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

8. Signature Characteristics:

a. Radar or Infrared (IR) signature performance specification, i.e., specific numerical design-to-requirements (applies to components as well as overall weapon system)

S/1.4g 1 October

D

b. Radar Cross Section (RCS), Jet Engine Modulation (JEM) or IR signature and signature reduction effectiveness

S/1.4g

(1) Measured or calculated numerical or quantitative data revealing aircraft or aircraft component RCS/JEM/IR signature characteristics

S/1.4g 1 October

D

(2) Test equipment, procedures, and frequencies

U

UNCLASSIFIED provided that aircraft signature characteristics are not highlighted in any way. If highlighted, classify at same level as revealed information.

D

c. Sensors

(1) Specific detailed electrical and mechanical design data relating to the RCS reduction features

S/1.4g 1 October

D

(2) RCS or IR signature and signature reduction effectiveness

S/1.4g 1 October

D

(3) Commonly known design techniques and concepts for RCS reduction of sensors

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

d. Commonly known design techniques and concepts for RCS or IR signature reduction on an aircraft which does not reveal specific quantitative performance or specific methods from a classified source

U D

9. Radar Absorption Material (RAM)/Radar Absorbing Structures (RAS)

a. Performance specification or quantitative measurements of RAM/RAS revealing absorption capability as a function of thickness, incidence angle, or frequency

S/1.4g 1 October

Material property data on commercially available materials is unclassified.

D

b. Specific electrical design data, such as specifications, processes, or formulations of the absorbing features of RAM/RAS or RAM/RAS components which reveal the quantitative performance parameters

S/1.4g 1 October

Material property data on commercially available materials is unclassified.

D

c. General structural and/or environmental design data which does not reveal the above classified information

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

d. Material samples

(1) If composition and performance are identifiable

S/1.4g 1 October

Material property data on commercially available materials is unclassified.

D

(2) If composition and performance are not identifiable

U D

e. Visual views of RAM/RAS applications on aircraft which reveal location, attachment, or installation details, but do not reveal specific performance of

RAM/RAS

U

RAS must be deformed, cut up, compacted or crushed before placing in unclassified waste

D

f. Raw materials

(1) Complete quantitative listing for RAM composition or partial quantitative listing when identified in any way with the B-1 program

S/1.4g 1 October

Material property data on commercially available materials is unclassified.

D

(2) General description which does not reveal the above classified information

g. Exterior surface coverings U D

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

10. Navigation

a. Operating modes U D

b. System Level performance U D

(1) In air alignment with Doppler and Offensive Radar System (ORS) High Resolution Ground Map (HRGM) precision position updates (PPU) mode

U D

(2) Ground alignment followed with ORS HRGM PPU mode

U D

(3) Global Positioning System (GPS) only/GPS aided inertial

U D

c. Position update accuracy

(1) Using ORS HRGM PPU mode via the Kalman Filter

U D

(2) Using ORS Ground Map Beacon PU Mode via the Kalman filter

U D

(3) Other modes U D

11. Terrain Following (TF)

a. Compiled data showing TF vertical flight profile revealing operational restrictions or vulnerabilities

S/1.4g 1 October

D

b. Raw flight test data that is transmitted over unclassified data links or recorded on aircraft

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DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

c. Processed, calibrated or analyzed flight test data

Data will be classified based on the test content, as classified per other direction in this SCG

D

d. Minimum set clearance setting of the TF system

U D

e. Simulation/parametric analysis

U D

f. Information revealing TF capability over actual or simulated wartime routes

S/1.4g 1 October

D

12. Weapon Release and/or Delivery Accuracy

a. Unguided weapon CEP requirements and analyses

U D

b. Guided weapon CEP using predefined target coordinates

Classify IAW specific weapon SCG

D

c. Guided weapon CEP using GPS aided SAR Relative Targeting System

(1) Predicted values not substantiated by tests

U D

(2) Specification requirements

S/1.4g 1 October

D

(3) Test/operational data S/1.4g 1 October

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Section VII

PROPULSION SUBSYSTEM

DECLAS

DOOD

REMARKS

DISTRIBUTION

STATEMENT

1. Engine Model designation and manufacturer

U NA

2. Design Information U NA

3. Performance/operating characteristics

a. Which reveal degraded performance as an overall fleet deficiency

S/1.4g 1 October

D

b. Which do not reveal degraded performance as an overall fleet deficiency

U D

4. Specific fuel consumption required for operation with respect to aircraft flight time and distance

U D

5. Engine Weight U NA

6. Internal design information or details of the complete engine

U D

7. Reliability/Maintainability

a. Which reveal degraded performance as an overall fleet deficiency

S/1.4g 1 October

D

b. Which does not reveal degraded performance as an overall deficiency

U D

8. Infrared signature suppression and radar cross section signature suppression

a. Commonly known design techniques and concepts for RCS or IR signature reduction on an aircraft which does not reveal specific quantitative performance or specific method from a classified source

S/1.4g

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Section VII (Continued)

PROPULSION SUBSYSTEM

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9. Hardware

a. Assembled engine U NA

b. Components and subassemblies unassembled and during engine assembly

U NA

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Section VIII

OFFENSIVE AVIONICS SUBSYSTEMS

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1. Offensive Radar System

a. Accuracy air-to-air (A/A) and air-to-ground (A/GND) to include:

Navigation and Weapons Delivery simulations will be classified at the highest classification of data within the computer system

D

(1) The following position fix accuracies:

(a) Real Beam Ground Map Performance

U D

(b) High Resolution Ground Map

U D

(c) Ground Map beacon range performance

U D

(2) Accuracy of On-Board Targeting using GPS aided SAR Relative Targeting System

(a) Predicted values not

U D

(b) Specifications requirements

S/1.4g 1 October

D

(c) Test/operational data S/1.4g 1 October

D

(3) TF/TA accuracies D

(a) Including minimum and maximum range, range gates, scan limits, scan rates, and beam width

U D

(b) Azimuth angular accuracy

U D

(c) Elevation Accuracy U D

(4) Velocity update accuracy U D

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Section VIII (Continued)

(5) Ground Moving Target Identification

S/1.4g 1 October

D

(6) High altitude calibrate accuracy

U D

b. Detection range in A/A and A/Gnd Modes when associated with target sizes

(1) Map resolution U D

(2) Map range U D

(3) Map sizes and scan angles U D

(4) Map integration times U D

(5) When sigma zero, signal to noise, range, angle and velocity are combined

U D

(6) Weather range performance U D

(7) Ground moving target indicating and tracking

S/1.4g 1 October

D

(8) Beacon range U D

c. Signal characteristics for normal (non-EP) operation

(1) Doppler bandwidth U D

(2) Receiver noise figure U D

(3) Pulse repetition frequency U D

(4) Power output (peak and average)

U D

(5) Pulse width U D

(6) Pulse compression C/1.4g 1 October

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(7) Specific frequency and frequency band limits to include transmit and receive frequencies, frequency separation between channels, wideband or narrow band command frequencies, beacon transmit and receive frequencies when associated with equipment or function.

C/1.4g

(8) Number of commandable frequencies

U D

(9) First local oscillator frequency

U D

(10) First IF frequency C/1.4g 1 October

D

(11) IF bandwidth U D

(12) During ORS testing or normal operation, those signal characteristics detectable through open loop radiation

U e.g., bench test, preflight and flight test, etc., are

UNCLASSIFIED

D

d. Antenna Characteristics

(1) Null depth (difference pattern)

C/1.4g 1 October

D

(2) Antenna gain C/1.4g 1 October

D

(3) Sidelobe levels S/1.4g 1 October

D

(4) Beam Width (sum pattern) U D

(5) Polarization U D

(6) Low observable antenna freespace radar cross section signature characteristics

S/1.4g 1 October

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e. Burn through range S/1.4g

Range at which the ORS will burn through any enemy countermeasures

D

f. Complete ORS computer source program (software)

(1) All operational and support software object code

Classify consistent with the information revealed as directed by guidance in this SCG

D

(2) Source code which describes mechanization of classified parameters and implementation the information revealed as directed by guidance in this SCG

D

(3) Computer storage capacity U D

(4) Computer input/output information

U D

(5) Computer clock rates U D

(6) EP software mechanization descriptions

S/1.4g 1 October

D

g. System warm-up time U D

h. Electronic-Protection

(1) Capability/performance S/1.4g 1 October

D

(2) Generic EP terms: Angle- On-Jam (AOJ), Home-On-Jam (HOJ), Velocity Gate Stealer (VGS), Range Gate Stealer (RGS), Repeater Swept Amplitude Modulation (RSAM)

U D

i. Vulnerability to countermeasures

S/1.4g 1 October

D

j. Operational deficiency as applies to degraded performance at the installed system level

S/1.4g 1 October

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k. Weight, cooling, volume, power requirements

U D

l. Test equipment

Classify IAW guidance in this SCG, as applicable to the test equipment addressed

D

m. Test data

(1) Sensitive characteristics the information revealed, as directed by guidance in this SCG

D

(2) Recorded ORS Flight Test Data

U D

(3) Recorded Navigation System and INS Data

U D

n. Hardware

(1) Assembled AN/APQ-164 Radar Set

U D

(2) AN/APQ-164 Components U D

o. Display imagery U

Includes recorded data.

Only when over-flown areas are not classified by imagery classification guides.

D

p. AN/APQ-164 display imagery

U D

2. Navigation Subsystems

a. Inertial Navigation

(1) Performance parameters revealed during check-out or uninstalled test of the Inertial Navigation Unit

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(2) ORS HRGM PPU aided-inertial navigation performance when installed in the B-1 Weapon System

U D

(a) Aided-inertial performance data when ORS HRGM PPU mode are applied via the Kalman filter

U D

(b) Performance data from ORS ground map beacon PPU mode update

U D

(c) Global Position System (GPS) aided-inertial navigation performance

U D

(d) Aided-inertial performance applied any other way

U D

b. Global Position System See

Remarks Classify IAW GPS SCG D

3. AN/APN-224 Altimeter U D

4. AN/APN-230 Strategic Doppler Radar

U D

5. Conventional Station Logic Unit

(SLU)

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6. Mass Storage Unit

a. Hardware with inserted mission-related data and/or computer program(s) inserted data and/or computer program(s)

D

b. Hardware after the operational computer program data erase function is performed

U D

7. Radar Data Terminal

a. Hardware with inserted computer program(s) inserted computer programs

D

b. Hardware after the operational computer program data erase function is performed

U D

8. Avionics Control Unit

a. Hardware with inserted mission related data and/or computer program(s) inserted data and/or computer program(s)

D

b. Hardware after mission related data has been erased

U D

9. Data Transfer Unit (DTU)

a. Hardware with inserted and/or recorded mission related data inserted and/or recorded data

D

b. Hardware after mission related data has been erased

DTU receptacles and controller and the Digital Transfer Interface Unit (DTIU) are unclassified upon power off and the Data Transfer Cartridge (DTC) will retain the highest level of classification recorded.

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10. Operational Flight Software

Classify information based on guidance in other portions of this SCG

D

11. Flight Test Instrumentation inserted and/or recorded data

D

12. Low Probability of Intercept

(LPI)

a. Discussion of general techniques

U e.g., power management coherent integration

b. Discussion of specific LPI related capabilities, ranges of operation, performance specifications, or measured performance

S/1.4g 1 October

D

13. MIL-STD-1760 Interface Equipment

a. Hardware where classified data are stored or processed

Classify hardware based on inserted data. (Data as classified per other portions of this SCG)

D

b. Hardware which does not contain classified data

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14. Weapon Release and/or Delivery Accuracy

a. Unguided weapon CEP requirements and analyses

U D

b. Guided weapon CEP using predefined target coordinates

Classify IAW specific weapon SCG

D

c. Guided weapon CEP using GPS aided SAR Relative Targeting System

(1) Predicted values not

U D

(2) Specification requirements S/1.4g 1 October

D

(3) Test/Operational data S/1.4g 1 October

D

15. Reliability/Maintainability

a. Which reveal degraded performance as an overall fleet deficiency

S/1.4g 1 October

D

b. Which does not reveal degraded performance as an overall fleet deficiency

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Section IX

DEFENSIVE AVIONICS SUBSYSTEM

This section addresses the complete Defensive Avionics Subsystem, which is made up of the ALQ-161A to include the TWF and the ALE 48/49 (not to include expendable towed decoys). (See Section X and Section XVII. In addition, any Electronic Attack (formerly ECM) parameter that relates to performance on the B-1 shall be classified as described below. Furthermore, any performance data that reveals potential or current performance related to the B-1 Defensive Avionics Subsystem, whether the data is modeled, tested or done by analysis shall be classified as described below.

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1. AN/ALQ-161A Radio Frequency Surveillance/ Electronic Countermeasures Subsystem (RFS/ECMS)

Includes Tail Warning Function (TWF)

a. Design characteristics

(1) Weight U D

(2) Volume U D

(3) Input Power U D

(4) Dimensions D

(a) Antenna U D

(b) Radome U D

(c) Line Replaceable Unit

U D

(5) Association of AN/ALQ-161A with threat list for which the system is designed or programmed

Classify in accordance with source material. (NOFORN caveats may be required if intelligence information is the source).

D

(6) Operating frequencies

(a) Upper and lower limits of band designation in conjunction with specific frequencies

S/1.4g 1 October

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(b) Upper and lower limits of frequency range the RFS/ECMS can operate

S/1.4g 1 October

Refers to the range of operating frequencies when associated with the ALQ- 161A or its function and/or purpose. These ALQ-161A related frequency references may be UNCLASSIFIED by use of the standard ALQ- 161A band designators (i.e., 1, 2, 3, etc.)

D

(c) Frequencies used to test operations of the RFS/ ECMS during ground and flight tests

(1) Frequencies that reveal ALQ-161A functions, purpose, or limitations

S/1.4g 1 October

Tests using classified frequencies must be done in the appropriately cleared, restricted-access laboratory/facility/test range

D

(2) Non-threat specific RF/EAS test frequencies that do not reveal ALQ-161A functions, purpose, or limitations

U Non-Emitter-Associated Jamming (NEAJAM)

D

(3) Threat specific frequencies

Classify consistent with the threat frequency

D

(d) Specific polarizations associated with specific frequencies or ranges of frequencies

S/1.4g 1 October

The same polarization data are UNCLASSIFIED when not associated with the ALQ- 161A or its function and/or purpose

D

(e) TWF-Pulse Repetition Frequency/Pulse Width

S/1.4g 1 October

D

(f) TWF Pulse Repetition Frequency

C/1.4g 1 October

When standing alone D

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(g) TWF Pulse Width C/1.4g 1 October

When standing alone D

(7) Technique capability or effectiveness, jam modulation in conjunction with threats

S/1.4g 1 October

D

(8) Technique characteristics or names in conjunction with B-1

(a) Specific operational technique characteristics

S/1.4g 1 October

Specific operational Electronic Attack (EA) technique parametric design characteristics that would allow someone to derive technique effectiveness, limitations, or threat system(s) the technique is designed or programmed to counter

D

(b ) Specific training or test-driven technique characteristics

U

Identifying a technique or modulation designed to provide training or test and evaluation against simulator provided parameters that do not represent or imply actual operational settings

D

(c) Generic technique nomenclature

U

Generic EA nomenclature such as repeater, transponder or noise jamming that does not characterize specific operational implementation or purpose

D

(d) Coded Technique Description

S/1.4g 1 October

Correlation of EA technique description with its coded name

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(9) Radiation of operational techniques:

Technique capability is classified in accordance with paragraph 1a(7) and technical characteristics in accordance with paragraph 1.a.(8)

D

(10) Typical EA Parameters

(a) Azimuth accuracy S/1.4g

Data which reveals measurements of system Azimuth accuracy at certain frequencies or ranges of frequencies other than sector determination

D

(b) Emitter capacity/ Pulse density capacity

S/1.4g 1 October

Upper limit of signal density which determines system/ subsystem operating limits

D

(c) Response time S/1.4g 1 October

Response time to Tracker/YIG assignment

D

(d) Detection/Sensitivity S/1.4g 1 October

D

(e) False alarm rate S/1.4g 1 October

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b. Performance characteristics

(1) Response time S/1.4g 1 October

The time it takes to respond to a threat. Includes TWF auto-dispense.

D

(2) Ranging capability or accuracy

(a) All other RFS/ECMS ranging capability

C/1.4g 1 October

D

(b) Ranging accuracy S/1.4g 1 October

Includes TWF dispense timing and ranging

D

(3) Power Output MAX Effective Radiated Power (ERP)

S/1.4g 1 October

D

(a) Burn-thru range S/1.4g 1 October

D

(4) Sensitivity

(a) System Level S/1.4g 1 October

D

(b) Line Replaceable Unit Level

C/1.4g 1 October

D

(5) Reliability/ Maintainability

S/1.4g 1 Oct

UNCLASSIFIED only when it does not relate to degraded performance as an operational aircraft deficiency or limitation, which could be exploited by an adversary

D

(6) Multiple threat handling capability

S/1.4g 1 October

The number of threats the system can handle simultaneously.

D

(7) Receive polarization sense

C/1.4g 1 October

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(8) Antenna gains

(a) 1122 and TWF gain versus spatial coordinates

S/1.4g 1 October

D

(b) All other RFS/ECMS antenna relative gain data

U D

(c) All other RFS/ECMS antenna absolute gain data

C/1.4g 1 October

D

(9) Performance parameters or design characteristics which could be used to derive system effectiveness or limitations

S/1.4g 1 October

D

(10) EA effectiveness against threat systems

D

(a) Effectiveness measurements of any technique or modulation against a specific threat, replica, surrogate, or simulator, based on detailed analyses or test data

S/1.4g

May be classified higher if source threat data revealed warrants

D

(b) Effective estimates made by observations not supported by analyses, instrumental data, or collection of test data, when the OA technique parameters to not represent, imply or in any way resemble actual operating settings

U

(11) EA effectiveness against U.S. systems

Classify IAW U.S. system's

SCG

D

(12) Performance limitations against threat systems

S/1.4g 1 October

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(13) Threat-Handling capability

S/1.4g 1 October

D

(14) Parameters which could be used to derive system limitations

S/1.4g 1 October

D

c. End item hardware

(1) External views of the completely assembled Line Replaceable Unit (LRU) which do not reveal any of the foregoing information

U D

(2) Completely assembled RFS/ECMS with loaded software loaded software

D

(3) Physical Characteristics U D

(4) Line Replaceable Units U D

(5) Components & Shop Replaceable Units

U D

(6) Cables & wave guides U D

(7) Preprocessor Avionics Control Unit (PACU)

U D

d. End Item Software

(1) Computer program Documentation

(a) Entire computer program processing algorithms with EID mission data

Classify IAW EID mission data utilized.

PFS data is UNCLASSIFIED

(b) Single program elements (subroutine) processing algorithms

Classified IAW mission data utilized.

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(2) Computer Program

(a) Source code

D

(b) Object code

D

(3) Programmable Read Only Memory (PROM) firmware information, contained, per guidance in this SCG

D

(4) Data Transfer Cartridge

Classify consistent with the inserted mission related data and/or computer program(s)

D

e. Systems Parameters

(1) System Delay/Repeater Delay

S/1.4g 1 October

D

(2) Power Output MAX Effective Radiated Power

S/1.4g 1 October

D

(3) Antenna Patterns/Polarization

S/1.4g 1 October

D

(4) System Level Sensitivity S/1.4g 1 October

D

(5) LRU Level Sensitivity C/1.4g 1 October

D

(6) Dynamic range S/1.4g 1 October

D

(7) Reliability/ Maintainability

S/1.4g 1 October

UNCLASSIFIED only when it does not relate to degraded performance as an operational aircraft deficiency or limitation, which could be exploited by an adversary

SECURITY…