ss-sys-600_e.doc

FOR OFFICIAL USE ONLY SS-SYS-600C SCN 001

FOR OFFICIAL USE ONLY

SS-SYS-600E

CI# MV0505F

Cage Code 2D605

17 July 2010

SYSTEM SPECIFICATION

FOR THE BLOCK IIF

NAVSTAR GLOBAL POSITIONING SYSTEM

REVISION E

CONTRACT NO F04701-96-C-0025

ADP NO. 109

(IMP/IMS AC# SE-107-05-08)

Prepared for:

U.S. Air Force

Space And Missile Systems Center Prepared by:

Boeing

Seal Beach, California Authenticated by Approved by Global Positioning Systems Wing GPS Programs Director Configuration Control Board Chairman Boeing Space and Missile Systems Center, AFSPC Navigation Systems Los Angeles Air Force Base, California El Segundo, California Date__________ Date ___________

DISTRIBUTION D. Distribution authorized to DoD and U.S. DoD contractors only (Reason: ADMINISTRATIVE OR

OPERATIONAL USE) (Date of Determination: 28 September 1995). Other requests for this document shall be referred to Air Force Space & Missile Systems Center (SMC), Global Positioning Systems Wing (GPSW).

WARNING--This document contains technical data whose export is restricted by the Arms Export

Control Act (Title 22, U.S.C. 2751, et seq.) or Executive Order 12470. Violation of these export-control laws is subject to severe criminal penalties. Dissemination of this document is controlled under DoD Directive 5230.25 and AFI 61-204.

Include this notice with any reproduced part of this document.

DESTRUCTION NOTICE--For classified documents, follow the procedures in DoD 5220.22-M, National Industrial Security Program Operating Manual, chapter 5, section 7., or DoD 5200.1-R, Information Security Program Regulation, chapter IX. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

REPRODUCTION - LOCAL REPRODUCTION IS AUTHORIZED

This Document contains information EXEMPT FROM MANDATORY DISCLOSURE UNDER THE FOIA

EXEMPTIONS (b)(4) and (b(5) apply.

REVISION RECORD

· IIF SV RAP allocation updates P00029

· Deletion of IIF SV L5 option P00029

· Update to classified IIF SV NDS requirements P00029

· Change of launch vehicle from MLV (Delta II 7925, Titan II , Atlas II) to EELV (Delta 4, Atlas V) P00029

· IIF SV “additional” payload accommodations updates P00029

· IIF SV “additional” payload accommodations and RAP allocation updates P00029

· IIF SV “additional” payload accommodations and RAP allocation updates P00029

· Addition of MA code and Flexible Data Message (FDM) P00029

· IIF SV “additional” payload accommodations updates

· Modification of sub-storm electrons environment definition P00029

· IIF SV “additional” payload accommodations and RAP allocation updates P00029

· General requirement and editorial updates

· Deletion of ADA programming language requirement P00182

· Direct Inject – IIF SV orbit insert trajectory changes

· Dual Integration – IIF integration with both EELV vehicles (Atlas V and Delta 4) P00055

· SAASM classified updates

· Updates SV processor throughput and memory margins P00065

· Removal of IIF SV Laser/LE-ASAT threat requirements

· Removed references to Appendix D P00182

· IIF SV Modernization – addition of L1M, L2M, L2C and L5 signals

· Deletion of IIF SV accommodations for RAP

· CS Modernization P00158

· Addition of LADO requirements

· Single Prime Initiative / CS consolidation P00182

· Addition of payload adapter requirements P00182

· Modernization SV development negotiated change – L2 power levels, L5 ellipticity, post delta-V recovery time

· General requirement and editorial updates P00247

· IIF SV Flexible Power change

· Standardization of URE definitions

· Addition of MMSRE to Control Segment

· General requirement and editorial updates N/A, see P00383

· URE requirement update P00383

· Removal of ICD-GPS-700, ICD-GPS-703, ICD-GPS-705 references from CS requirements

· Removal of ICD-GPS 323 references and removal of IIR ANE (Autonomous Navigation Emulator) interface requirements

· Removal of crosslink support (including generalized commanding) from CS requirements

· Removal of Autonav support from CS requirements.

P00309

· Update ICD references

· Finalize verification methods

· Incorporate CS Effectivities P00579

· Update of Appendix H verification methods and effectivities

· Updates to classified appendices wording and verification methods

· Administrative/grammatical updates P00652

· Replacement of IRS-SV-LV-07 references with those of the Atlas and Delta VCNs Pending

· Update of launch schedule requirement

· Replacement of SOPG and SPG with SCG Pending

· Incorporates SCN E001, E002R1 and E003 Pending

TABLE OF CONTENTS

11 Scope

1.1 Identification

1.2 System Overview

1.2.1 Interfaces

1.3 Document Overview

1.3.1 Document Conventions

2 Applicable Documents 3 Requirements

3.1 Definition

3.1.1 Physical Description

3.1.1.1 GPS IIF System

3.1.2 Deleted

3.1.3 IIF System States/Modes Description

3.1.3.1 IIF System Development State

3.1.3.2 IIF System Active State

3.1.3.3 IIF Mixed Constellation Mode

3.1.3.4 Full IIF Constellation Mode

3.1.4 Specification Tree

3.1.5 Missions

3.1.6 Threat

3.2 Capability / Performance Requirements

3.2.1 Develop System

3.2.1.1 General

3.2.1.2 Computer Resources

3.2.1.3 Environments

3.2.1.4 Communications

3.2.1.5 Materials, Processes, and Parts

3.2.1.6 Quality Assurance

3.2.1.7 Safety and Environmental

3.2.1.8 Security

3.2.2 Manufacture System

3.2.2.1 Manufacture System Components

3.2.3 Verify System

3.2.3.1 System Integrated Test Capability

3.2.3.2 System Testbed Configuration Fidelity

3.2.3.3 System Testbed Configuration Flexibility

3.2.3.4 Test Data Injection Capability

3.2.3.5 Mixed Constellation Test/Simulation Capability

3.2.3.6 Integrated Autonav Test Capability

3.2.3.7 CS to SV Prelaunch Compatibility Test

3.2.3.8 LV Compatible Test Capability

3.2.3.9 Operational Test and Evaluation

3.2.4 Train Operators

3.2.4.1 GPS Training

3.2.4.2 Personnel

3.2.4.3 Training

3.2.4.4 Training Equipment

3.2.5 Deploy System

3.2.5.1 Launch-On-Need

3.2.5.2 Flight Readiness

3.2.5.3 Activation Time

3.2.5.4 Operational Orbits

3.2.6 Support System Operations

3.2.6.1 Logistics

3.2.6.2 Maintenance Planning

3.2.6.3 Supply Support

3.2.6.4 Packaging and Handling

3.2.6.5 Storage

3.2.6.6 Transportability

3.2.6.7 Manpower and Personnel

3.2.6.8 Support Equipment

3.2.6.9 Computer Resources Support

3.2.6.10 Facilities and Equipment

3.2.6.11 GPS Simulation Capability

3.2.7 Perform Navigation Mission

3.2.7.1 GPS Navigation Performance

3.2.7.2 Mission Availability

3.2.7.3 Dual Frequency URE

3.2.7.4 Selective Availability & Anti-Spoofing

3.2.7.5 Single Frequency Accuracy

3.2.7.6 SV Navigation Health Status - Stationkeeping

3.2.7.7 Flexible Power

3.2.8 Perform NDS Mission

3.2.8.1 NDS Interface

3.2.9 Perform Other Missions

3.2.9.1 Additional Payload Accommodation

3.2.10 Dispose of System

3.2.10.1 Disposal

3.3 External Interface Requirements

3.3.1 GPS IIF to AFSCN

3.3.1.1 AFSCN Interface

3.3.2 GPS IIF to NGA

3.3.2.1 GPS IIF to NGA Interface Requirements

3.3.3 GPS IIF to HANU

3.3.3.1 GPS IIF to HANU Interface Requirements

3.3.4 GPS IIF to USNO

3.3.4.1 GPS IIF to USNO Frequency Requirements

3.3.4.2 GPS IIF to USNO Time Requirements

3.3.5 GPS IIA to GPS IIF System

3.3.5.1 GPS IIA System Interface

3.3.6 GPS IIR/IIR-M to GPS IIF System

3.3.6.1 GPS IIR/IIR-M System Interface

3.3.7 Launch Vehicle to GPS IIF

3.3.7.1 Launch Vehicle to GPS IIF Requirements

3.3.8 GPS IIF to ICADS

3.3.8.1 GPS IIF to ICADS Interface Requirements

3.3.9 DELETED

3.3.10 GPS IIF to IIR MTS

3.3.10.1 GPS IIF to IIR MTS Interface Requirements

3.3.11 GPS IIF TO IIR OSS

3.3.11.1 GPS TO IIR OSS Interface Requirements

3.3.12 GPS IIF TO NSA

3.3.12.1 GPS TO NSA Interface Requirements

3.3.13 GPS IIF TO TAD/SAGES

3.3.13.1 GPS IIF to TAD/SAGES Interface Requirements

3.3.14 GPS IIF TO GSIS

3.3.14.1 GPS IIF to GSIS Interface Requirements

3.3.15 GPS IIF TO User Support Community

3.3.15.1 GPS IIF to User Support Community Interface Requirements

3.3.16 GPS IIF to JSpOC

4 Quality assurance provisions

4.1 General Quality Assurance Provisions

4.2 Special Tests/Examinations

4.2.1 SV Prelaunch Compatibility Test

4.2.2 Operational Tests

4.3 Requirements Verification

5 REQUIREMENTS ALLOCATION/TRACEABILITY.

5.1 Segment Description

5.1.1 Control Segment

5.1.2 GPS IIF Space Segment

5.2 DELETED

5.3 Control Segment Performance Requirements

5.3.1 Develop Control Segment

5.3.1.1 System Allocated Development Requirements

5.3.1.2 Define Operational Concepts & Requirements

5.3.1.3 Develop Design

5.3.2 Manufacture System

5.3.2.1 Manufacture Elements

5.3.3 Verify System

5.3.3.1 System Allocated Verification Requirements

5.3.3.2 Verify Control Segment

5.3.3.3 Support Verification of SS

5.3.3.4 Support Government Verification

5.3.3.5 Support Independent Operational Testing

5.3.3.6 Provide Built in Test Capability

5.3.4 Train Operators

5.3.4.1 System Allocated Train Operator Requirements

5.3.5 Deploy System

5.3.5.1 System Allocated Deployment Requirements

5.3.5.2 Deploy Control Segment

5.3.5.3 Deploy Space Segment

5.3.6 Support System Operations

5.3.6.1 System Allocated Support Requirements

5.3.6.2 Provide Simulation Capability

5.3.6.3 Perform Constellation Management

5.3.6.4 Perform Space Vehicle Management

5.3.6.5 Perform Control Segment Management

5.3.6.6 Manage External Interfaces

5.3.6.7 CS to ICADS Interface Requirements

5.3.6.8 DELETED

5.3.6.9 Transmit SV Commands & Receive Telemetry

5.3.6.10 Perform Software Upload

5.3.6.11 Crosslink Support to System Operations

5.3.6.12 Reserved

5.3.6.13 Conduct Control Segment Logistics Support

5.3.6.14 Provide Secondary MCS

5.3.6.15 Provide IMOSC

5.3.6.16 RESERVED

5.3.6.17 Provide LADO Operations Centers

5.3.7 Perform Nav Mission

5.3.7.1 System Allocated Nav Mission System Requirements

5.3.7.2 RESERVED

5.3.7.3 Command & Control Nav Mission

5.3.7.4 RESERVED

5.3.7.5 Monitor SIS

5.3.8 Perform NDS Mission

5.3.8.1 System Allocated NDS Requirements

5.3.8.2 RESERVED

5.3.8.3 Command & Control NDS Mission

5.3.8.4 RESERVED

5.3.8.5 Monitor NDS SIS

5.3.9 Perform Other Missions

5.3.9.1 System Allocated Other Mission Requirements

5.3.10 Dispose Of System

5.3.10.1 Disposal

5.3.10.2 Support to SS Disposal

5.4 Space Segment Performance Requirements

5.4.1 Develop Space Segment

5.4.1.1 System Allocated Development Requirements

5.4.1.2 Define Operational Concepts & Requirements

5.4.1.3 Reserved

5.4.1.4 Develop Design

5.4.2 Manufacture System

5.4.2.1 Manufacture Elements

5.4.3 Verify System

5.4.3.1 System Allocated Verification Requirements

5.4.3.2 Support Verification of CS

5.4.3.3 Verify Space Segment

5.4.3.4 Support Government Verification

5.4.3.5 Support Independent Operational Testing

5.4.3.6 Provide Built in Test Capability

5.4.4 Train Operators

5.4.4.1 System Allocated Train Operator Requirements

5.4.5 Deploy System

5.4.5.1 System Allocated Deployment Requirements

5.4.5.2 Reserved

5.4.5.3 Deploy Elements

5.4.6 Support System Operations

5.4.6.1 System Allocated Support Requirements

5.4.6.2 Reserved

5.4.6.3 Perform Constellation Management

5.4.6.4 Perform Space Vehicle Management

5.4.6.5 Reserved

5.4.6.6 Receive Commands & Transmit Telemetry

5.4.6.7 Perform Software Upload

5.4.6.8 Crosslink Support to System Operations

5.4.6.9 Reserved

5.4.6.10 Conduct Space Segment Logistic Support

5.4.6.11 Reserved

5.4.6.12 Reserved

5.4.6.13 Reserved

5.4.6.14 Provide Mission Platforms

5.4.7 Perform Navigation Mission

5.4.7.1 System Allocated Nav Mission Requirements

5.4.7.2 Produce Navigation SIS

5.4.7.3 Command & Control Nav Mission

5.4.8 Perform NDS Mission

5.4.8.1 System Allocated NDS Mission Requirements

5.4.8.2 Produce NDS SIS

5.4.8.3 Command & Control NDS Mission

5.4.8.4 Exchange NDS Data With Constellation

5.4.9 Deleted

5.4.10 Dispose of System

5.4.10.1 Dispose of IIF SVs

6 Notes

6.1 Definitions

6.1.1 Control Segment

6.1.2 Deployment

6.1.3 Downing Event

6.1.4 Non-Operational

6.1.4.1 S-Band Link Data

6.1.4.2 SV-to-SV Communication

6.1.5 Error Value Confidence Level

6.1.6 Function Restoring Time

6.1.7 GPS Space Constellation

6.1.8 GPS SV Natural Environment

6.1.8.1 Trapped Electrons and Protons

6.1.8.2 Solar Protons and Alphas

6.1.8.3 Meteoroid Environment

6.1.8.4 Galactic Corpuscular Cosmic Rays

6.1.8.5 Sub-Storm Electrons

6.1.8.6 Energetic Particle Environment

6.1.9 Ground Antenna

6.1.10 Master Control Station

6.1.11 Mission Critical Failure

6.1.12 Mission Effectiveness (ME)

6.1.13 Monitor Station

6.1.14 NAV Payload Graceful Turn-on

6.1.15 OCS Operational Availability (Ao)

6.1.16 OCS Operational Dependability (Do)

6.1.17 OCS Support Capacity

6.1.18 Operationally Configured For Navigation Operations

6.1.19 Operational Control System

6.1.20 Operational Space Vehicle

6.1.21 “Red” Rating At OCS Site

6.1.22 “RED” Data

6.1.23 Sustainment of the Navstar Global Positioning System (GPS) Signal-in-Space

6.1.24 System Restoring Time

6.1.25 Simulator Fidelity

6.1.26 User Range Error (URE) Computation

6.1.27 Distance Root Mean Square (drms)

6.1.28 Design Goal

6.1.29 Interoperability

6.1.30 Methods of Verification

6.1.30.1 Control Segment Acceptance

6.1.31 Flight Readiness

6.1.32 Surge Mode

6.1.33 Selective Availability (SA)

6.1.34 Anti-Spoof (A-S)

6.2 Segment States and Modes Description

6.2.1 CS States

6.2.2 CS Modes

6.2.3 SS States Description

6.2.3.1 IIF SS Development State

6.2.3.2 IIF Mixed Constellation State

6.2.3.3 Full IIF constellation state

6.2.4 SS Modes Description

6.2.4.1 IIF SS Direct Upload Mode

6.2.4.2 IIF SS Crosslink Navigation Update Mode

6.2.4.3 IIF SS Autonav Mode

6.3 ABBREVIATIONS AND ACRONYMS

LIST OF FIGURES

2Figure 1.2.1-1 Interface Block Diagram

Figure 3.1.1 GPS IIF System Diagram Figure 3.1.4 Top Level Specification Tree Figure 6.1.8-1 LET Spectrum Figure 6.1.8-2 Solar Flare Proton Component Fluence

List of Tables

9Table 3.1 IIF System States and Modes

Table 3.2.1-1 Crosslink Required EIRP Table 3.2.1-2 - Block IIF S-Band Uplink Margin Requirements.

Table 3.2.1-3. Block IIF S-Band Downlink Margin Requirements.

Table I Example Orbital Position Assignments Table 3.2.7-1 -L-Band Signal Strengths (User Receive Power) Table 3.2.7-2 - L-Band Signal Ellipticity Table 3.2.7.3-1 System Constellation URE Requirements Table 3.2.7-3 L1 Flexible Power Configurations - EOL Received Signal Level (dBW) Table 3.2.7-4 L2 Flexible Power Configurations - EOL Received Signal Level (dBW) Table 3.3-1 Deleted Table 5-1 System Constellation URE Requirements Table 5.4.1-1 - Block IIF S-Band Uplink Margin Requirements.

Table 5.4.1-2. Block IIF S-Band Downlink Margin Requirements.

Table 6-1 GPS Mission Trapped Electrons and Trapped Protons Table 6-2 Solar Proton Table 6-3 Meteoroid Particle Environment Table 6.1: System and Space Segment States and Modes Table H-1 Requirements Verification and Traceability Matrix H-1

LIST OF APPENDICES

APPENDIX A Classified Requirements of the GPS Nav Mission (U) A-1 APPENDIX B Classified Requirements of the NDS Mission (U) B-2 APPENDIX C Classified Requirements, Spacecraft Nuclear Survivability (U) C-1

APPENDIX D DELETED

D-1 APPENDIX E Classified Requirements, Spacecraft Anti-Jam Features (U) E-1 APPENDIX F Deleted F-1 APPENDIX G Deleted G-1

APPENDIX H - REQUIREMENTS VERIFICATION AND TRACEABILITY MATRIX

H-1

The Block IIF sustainment effort includes the replenishment of the current constellation with IIF Space Vehicles (SVs) and modification and maintenance of the Control Segment to support the GPS constellation of II/IIA, IIR/IIR-M, and IIF SVs. This IIF sustainment effort does not include the User Segment. The Block IIF System requirements contained herein are allocated to the following segments:

a. Block IIF Space Segment (SS) which includes interfaces to the II, IIA, IIR and IIR-M SVs, Control Segment, Launch Vehicle, and the Users and

b. The Control Segment (CS) which includes interfaces to the II/IIA, IIR/IIR-M and IIF SVs, and to external agencies.

Requirements for the User Segment are not defined herein.

SYS600_M-8

SYS600_M-627

29 CFR

Occupational Safety and Health Administration

SYS600_M-86

40 CFR

40 Code of Federal Regulations, Protection of Environment

SYS600_M-87

49 CFR

49 Code of Federal Regulations, Department of Transportation

SYS600_M-88

ADPL# 056

GPS IIF Integrated Support Plan (ISP)

Draft 6-27-96

SYS600_M-5588

AFI 91-110

Nuclear Safety Review and Launch Approval for Space or

March 1994

Missile Usage of Radioactive Material and Nuclear Systems

SYS600_M-67

AFMAN 36-2108

Enlisted Classification

30 April 2003

SYS600_M-5590

CARDHOLDER

Functional Security Requirements Specification (FSRS)

FSRS

for Block IIF U/L, CARDHOLDER Device (U)

1 September 1995

SYS600_M-77

Draft

GPS Product Support Management Plan

April 2002

SYS600_M-5589

EWR 127-1

Eastern and Western Range Regulation 127-1;

As Tailored Range Safety Standards (Note 1)

SYS600_M-89

F04606-95-D-0239 GPS Operational Control Segment (OCS) Support Contract

SYS600_M-95

F04701-96-C-0025 Attach 4, GPS IIF Integrated Master Plan

SYS600_M-96

F04701-96-C-0025 Attach 1, SS-SYS-600 System Specification for the

Block IIF Navstar Global Positioning System (with Classified Appendices)

SYS600_M-97

GPS SCG 30 Sept 2008

Global Positioning System (GPS) Security Classification Guide (SCG)

SYS600_M-75

IS-GPS-200

Navstar GPS Space Segment/Navigation User

(Note 1) Interfaces

SYS600_M-45

ICD-GPS-201

Navstar GPS Space Segment/Control Segment (Note 1) Interfaces and classified Appendix A

SYS600_M-5380

ICD-GPS-202

Navstar GPS Control Segment/U.S. Naval Observatory (Note 1) Time Transfer Interfaces

SYS600_M-5383

ICD-GPS-203

Navstar GPS SA/AS Requirements (U) (Secret)

SYS600_M-47

ICD-GPS-205

Navstar GPS Telecommunications Simulator Interfaces

SYS600_M-5387

ICD-GPS-208

Navstar GPS Control Segment/Auxiliary User Interfaces

SYS600_M-5384

ICD-GPS-210

Interface Control Document for the Navstar Global (Note 1) Positioning System and Air Force Satellite Control

Network Interface

SYS600_M-5392

ICD-GPS-211

GPS Control Segment/NGA Interfaces

SYS600_M-5385

ICD-GPS-212

Navstar GPS Control Segment/ICADS Interfaces

SYS600_M-5386

ICD-GPS-215

Navstar GPS Space Tasking Control Interfaces

SYS600_M-5811

ICD-GPS-240

Navstar GPS Control Segment to User Support (Note 1) Community Interfaces

SYS600_M-5812

ICD-GPS-305

Navstar GPS Telecommunications Simulator Module (Note 1) Interface (Block IIR)

SYS600_M-5388

ICD-GPS-401

Navstar GPS Space to Control Segment

(Note 1)

(Block IIR/IIR-M) Interface and classified Appendix A

SYS600_M-2877

ICD-GPS-403

Interface Control Document for the Navstar Global (Note 1) Positioning System Control Segment/National Security

Agency

SYS600_M-5391

ICD-GPS-410

Navstar GPS Master Control Station/GPS - SISP (Note 1) Interface System (GSIS) Interfaces

SYS600_M-5813

ICD-GPS-602

NAVSTAR GPS Operational Control System / (Note 1) Operational Support System Interfaces

SYS600_M-5806

ICD-CS-605

Interface Control Document for the GPS Block IIF (Note 1) Satellite Telecommunications Simulator (STS)

SYS600_M-5846

ICD-GPS-620

Interface Control Document (ICD) for Navstar GPS (Note 1) Space Vehicle to Nuclear Detonation (NUDET)

Detection System Interface

SYS600_M-39

ICD-GPS-637

Interface Control Document (ICD) for Navstar GPS (Note 1) Space Vehicle to Space Vehicle Interfaces

SYS600_M-5587

ICD-GPS-700

Navstar GPS Military-Unique Space Segment/User (Note 1) Segment Interfaces

SYS600_M-49

IS-GPS-703

Navstar GPS Military-Unique Space Segment/User (Note 1) Segment Interfaces (U) (SECRET)

SYS600_M-51

IS-GPS-705

Navstar GPS Space Segment/User Segment L5

(Note 1) Interfaces

SYS600_M-53

ICD-GPS-206

Space Segment NDS User Interfaces (ICD-GPS-206) (Note 1) and classified Appendix A

SYS600_M-31

ICD-GPS-601

Space Segment-to-Control Segment Interfaces (ICD-(Note 1) GPS-601) and classified Appendix A

SYS600_M-33

ULA-Atlas-ICD-04-001, Global Positioning System IIF / Atlas V 401 Interface (Note 1) Control Document

MDC 01H0472, "Global Positioning Satellite (GPS) Mission Specification for (Note 1) the Delta IV Launch System

SYS600_M-41

KAG-30A/TSEC

Compromising Emanations Standard for Cryptographic

January 1971 Equipment (U)

SYS600_M-69

MIL-STD-461D

Electromagnetic Emission Susceptibility Requirements

As Tailored for the Control of Electromagnetic Interference 11 January 1993

SYS600_M-56

MIL-STD-462D

Measurement of Electromagnetic Interference

As Tailored Characteristics 11 January 1993

SYS600_M-58

MIL-STD-498

Software Development & Documentation

As Tailored

5 December 1994

SYS600_M-60

MIL-STD-1540C

Testing Requirement for Launch, Upper Stage, As Tailored and Space Vehicles 15 September 1994

SYS600_M-62

MIL-STD-1547B

Electronics Parts, Materials and Processes for Space As Tailored and Launch Vehicles December 1992

SYS600_M-64

MIL-STD-2401

Department of Defense World Geodetic System (WGS)

SYS600_M-5492

NACSIM 5203

National COMSEC Information Memorandum

SYS600_M-5779

PEGASUS

Functional Security Requirements Specification (FSRS)

FSRS

for Block IIF D/L, PEGASUS (KGV-227) Device (U)

1 September 1995

SYS600_M-80

Navstar

Telecommunications Security Requirements Document (TSRD) for TSRD the Embedment of the CARDHOLDER and

PEGASUS Cryptographic Chips into the Navstar Block 25 October 1995 IIF Satellite

SYS600_M-83

NGA TR8350.2

Department of Defense World Geodetic System 1984

SYS600_M-5491

SS01-0017

GPS IIF Specification Tree

SYS600_M-5490

Training

Block IIF System Training Requirements Document (STRD)

5 March 1996

SYS600_M-71

SYS600_M-107

SYSTEM STATE

SYSTEM MODE

IIF Development

State IIF Development Mode IIF Active State Mixed Constellation Mode Full IIF Constellation Mode

SYS600_M-146

SYS600_M-165

Position data shall be in Cartesian earth-centered, earth-fixed coordinates as specified in Department of Defense (DoD) World Geodetic System 1984 (WGS 84).

SYS600_M-180

Off Nadir Angle Required EIRP (dBW) 20.3 20.0 19.8 19.4 Objective EIRP (dBW) 21.0 20.9 20.8 20.7 20.6 19.1 14.0

SYS600_M-221

Launch & Early Orbit* Mission Orbit

RTS* RTS* GA**

Required Margins

Acquisition > 0.0 dB > 0.0 dB > 0.0 dB

Command > 11 dB > 11 dB > 20 dB

Ranging > 11 dB > 11 dB N/A

Margins apply prior to launch and after separation from the LV

* Based on a 33ft RTS antenna with a 105 dBm capability.

** Based on a GA antenna with a 102.5 dBm capability.

SYS600_M-5839

Telemetry Acquisition Ranging

500 bps 4 kbps

Signal Margin

Mission Orbit

RTS > 21.0 dB > 12.0 dB > 0.0 dB > 0.0 dB

GA > 21.0 dB > 12.0 dB > 0.0 dB N/A

Drift Orbit

RTS > 15.0 dB > 6.0 dB > 0.0 dB > 6.0 dB

GA > 15.0 dB > 6.0 dB > 0.0 dB N/A

* - Margins apply after separation from the LV

Note 1: 33 ft RTS G/T = 21.6 dB/deg-K-used in link margin analysis

SYS600_M-5841

Class 1 Ozone Depleting Substances (ODS) shall not be used in the design, manufacture, test, operation or maintenance of GPS IIF System components. The following are Class 1 ODS:

a. Halons: 1011, 1202, 1211, 1301, and 2402

b. Chlorofluorocarbons (CFC): CFC-11, CFC-12, CFC-13, CFC-111 thru 115, CFC-211 thru 217, and the blends R-500, thru R-503

c. Other controlled substances: Carbon tetrachloride, Methyl chloroform, and methyl bromide

SYS600_M-296