2006 SYSTEMS HANDBOOK 

A Mess

age Fro

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taff, United 

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A Message from the Chief of Staff, United States Air Force 

This year, as we commemorate 60 years as 

America’s Air Force, we must look to history to guide us through the many diverse 

challenges that lie ahead as we transform 

and streamline to meet future challenges. 

Today, we are a force unmatched by anyone 

in the world, seasoned by over 16 years of continuous combat 

operations. We are the leaders in Global Vigilance, Global 

Reach, Global Power, and most importantly, highly skilled and 

motivated Airmen.

Our Airmen are the most important piece to execute our Air, 

Space, and Cyberspace power and the key to the success of the 

Total Force. From the front lines of the Global War on Terror to 

Homeland Defense and humanitarian missions, our Total Force 

accomplish amazing tasks everyday amidst the stressful situations in which they are deployed—everyday, everywhere.

This handbook highlights the tools and capabilities that empower our Airmen, both on the ground and in the air to be successful in their warfighting endeavors and the defense of the nation. 

The systems and equipment highlighted in the following pages 

showcase the technological lengths to which we will go to ensure 

that we will now and in the future continue to be the world’s 

most capable Air Force as we fly and fight in Air, Space, and 

Cyberspace.

This handbook is a tool just like the equipment listed within its 

pages. Use it as the resource for which it was intended and together we will continue to focus on winning the Global War on 

Terror and ensuring the safety and security of our great nation 

and its citizens.

 T. Michael Moseley

 General, USAF 

Chief of Staff

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THE AIR FORCE HANDBOOK 2007 III

A Message From the Chief of Staff, United States Air Force _ I

How to use this book _________________________VII

The Chief’s Priorities __________________________1

Meeting the Global Security Challenge ______________7

2006 Air Force Crisis Response and Combat Actions _____ 17

Key Air Force Personnel________________________ 25

Systems __________________________________ 26

A-10/OA-10 Thunderbolt II __________________________ 26

AC-130H Spectre ________________________________ 28

AC-130U Spooky ________________________________ 30

Advanced Extremely High Frequency (AEHF) System___________ 32

AGM-65 Maverick _______________________________ 34

AGM-86B Air Launched Cruise Missile (ALCM)_______________ 36

AGM-86C/D Conventional Air Launched Cruise Missile (CALCM) ____ 38

AGM-88 High Speed Anti-Radiation Missile (HARM) ___________ 40

AGM-129A Advanced Cruise Missile (ACM)_________________ 42

AGM-130 Standoff Attack Weapon _____________________ 44

AIM-7M Sparrow________________________________ 46

AIM-9M Sidewinder ______________________________ 48

AIM-9X Sidewinder ______________________________ 50

AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM) ___ 52

Air Force Combat Identification (AFCID) __________________ 54

Air Force Satellite Control Network _____________________ 56

Air Force Weather Weapon System (AFWWS) _______________ 58

Airborne Laser (ABL)______________________________ 60

AN/GSQ-272 Air Force Distributed Common Ground System

(AF DCGS) ____________________________________ 62

AN/USQ-163 Falconer Air and Space Operations CenterWeapon System 

(AOC-WS) ____________________________________ 64

B-1B Lancer___________________________________ 66

B-2 Spirit ____________________________________ 68

B-52H Stratofortress______________________________ 70

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TABLE OF CONTENTS

IV UNITED STATES AIR FORCE

C-5 Galaxy____________________________________ 72

C-9C _______________________________________ 74

C-12C/D/F/J___________________________________ 76

C-17 Globemaster III______________________________ 78

C-20B/H _____________________________________ 80

C-21A ______________________________________ 82

C-32A ______________________________________ 84

C-37A ______________________________________ 86

C-40B/C _____________________________________ 88

C-130 Hercules _________________________________ 90

C-130 Senior Scout_______________________________ 92

C-130H Scathe View ______________________________ 94

C-130J ______________________________________ 96

CBU-87/103 Combined Effects Munition (CEM) ______________ 98

CBU-89/104 Gator ______________________________ 100

CBU-97/105 Sensor Fused Weapon (SFW) ________________ 102

Combatant Commanders Integrated Command and Control System 

(CCIC2S) ____________________________________ 104

Combat Survivor Evader Locator (CSEL)__________________ 106

Control and Reporting Center (CRC)____________________ 108

Counterspace Systems____________________________ 110

CV-22B_____________________________________ 112

Defense Meteorological Satellite Program (DMSP) ___________ 114

Defense Satellite Communications System (DSCS) III__________ 116

Defense Support Program (DSP) _____________________ 118

Deliberate Crisis and Action Planningand Execution Segments

(DCAPES) ___________________________________ 120

Distributed Mission Operations (DMO) __________________ 122

E-3 Sentry Airborne Warning and Control System (AWACS)______ 124

E-4B National Airborne Operations Center (NAOC) ___________ 126

E-8C Joint STARS _______________________________ 128

EC-130H Compass Call ___________________________ 130

Evolved Expendable Launch Vehicle (EELV) _______________ 132

Expeditionary Combat Support System (ECSS) _____________ 134

F-15A–D Eagle ________________________________ 136

F-15E Strike Eagle ______________________________ 138

F-16 Fighting Falcon ____________________________ 140

F-16 HARM Targeting System (HTS) R6 and R7 _____________ 142
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THE AIR FORCE HANDBOOK 2007 

F16-TARS (Theater Airborne Reconnaissance System) _________ 144

F-22A Raptor _________________________________ 146

F-35 Lightning II Joint Strike Fighter ___________________ 148

F-117 Nighthawk ______________________________ 150

GBU-31/32/38 Joint Direct Attack Munition (JDAM) __________ 152

GBU-39/B Small Diameter Bomb (SDB) _________________ 154

Global Broadcast Service (GBS) ______________________ 156

Global Positioning System (GPS)______________________ 158

Halvorsen (formerly Next Generation Small Loader [NGSL]) _____ 160

HC-130P/N King _______________________________ 162

HH-60G Pave Hawk _____________________________ 164

Hypersonic Technology Vehicle (HTV)___________________ 166

Joint Air-to-Surface Standoff Missile (JASSM) _____________ 168

Joint Helmet Mounted Cueing System (JHMCS)_____________ 170

KC-10 Extender _______________________________ 172

KC-135 Stratotanker ____________________________ 174

Launch & Test Range System (LTRS) ___________________ 176

LGM-30G Minuteman III __________________________ 178

MC-130E Combat Talon ___________________________ 180

MC-130H Combat Talon II _________________________ 182

MC-130P Combat Shadow _________________________ 184

Medium Launch Vehicle (MLV) ______________________ 186

MH-53J/M Pave Low III/IV _________________________ 188

Military Satellite Communication (MILSATCOM) Terminals ______ 190

Military Strategic and Tactical Relay (Milstar) ______________ 192

Mission Planning Systems (MPS) _____________________ 194

MQ-1 Predator ________________________________ 196

MQ-9 Reaper _________________________________ 198

National Polar-orbiting Operational Environmental Satellite System 

(NPOESS) ___________________________________ 200

Operationally Responsive Space (ORS) __________________ 202

Polar Military Satellite Communications (MILSATCOM) ________ 204

RC-26B_____________________________________ 206

RC-135S Cobra Ball _____________________________ 208

RC-135U Combat Sent ___________________________ 210

RC-135V/W Rivet Joint ___________________________ 212

Regional Sector Air Operations Center (RSAOC) _____________ 214

Rocket Systems Launch Program (RSLP) _________________ 216
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VI UNITED STATES AIR FORCE

RQ-4A/B Global Hawk ___________________________ 218

Space Based Infrared System High (SBIRS High) ____________ 220

Space Radar (SR)_______________________________ 222

Space Situation Awareness (SSA) Systems ________________ 224

Space Test Program (STP) _________________________ 226

T-1A Jayhawk ________________________________ 228

T-6A Texan II _________________________________ 230

T-37B Tweet _________________________________ 232

T-38A/AT-38B/T-38C Talon _________________________ 234

T-43A _____________________________________ 236

Tactical Air Control Party (TACP)

and Air Support Operations Center (ASOC)________________ 238

Theater Battle Management Control Systems (TBMCS) ________ 240

Transformational Satellite Communications System (TSAT)______ 242

Tunner 60K Loader______________________________ 244

U-2S Dragon Lady ______________________________ 246

UH-1N Helicopter (Variants: 1H/Vm, UV-18B) _____________ 248

VC-25A ____________________________________ 250

WC-135 Constant Phoenix _________________________ 252

Wideband global satcom (WGS) system _________________ 254

Wind Corrected Munitions Dispenser (WCMD

and WCMD-Extended Range (WCMD-ER) ________________ 256

Appendices_______________________________ 259

Air force Demographics_______________________ 261

Air Force Units of Operation____________________ 265

Combat wings_____________________________ 267

Air force installation locations __________________ 269

Glossary of Terms/Acronyms ___________________ 279

Systems by Contractor _______________________ 287

Systems by State Of Manufacture________________ 307
THE AIR FORCE HANDBOOK 2007 VII

This book is designed for clear and easy reference to critical information about Air Force systems.

MI SS ION

29 UNITED ST AT ES AIR FOR CE

RAPID STRIKE

2006 SY STEMS HANDBOOK 30 

A10/OA-1 0 THUNDERBOL T I I STRA TEGIC CAP ABILITY

A- 10/OA-1 0 THUNDERBOL T I I

MI SS IO N

Pr ovide Close Air Suppor t (CAS) and Fo rward Air C ontrol (F AC) suppor ting 

the ground battle including Special F orces; C ombat Search and Rescue

(CSAR) and perform interdiction under cer tain circumstances .

DE SCRIPTION 

Th e A-10/O A-10Th underbolt II has e xce llent maneuv erability at low air speeds and

highly accurate w eapons-delivery platform s.Using Night Vi sion Imaging Systems

(NVIS), A-10/O A-10 pilots can conduc t their missions during darkness . T hunderbolt IIs

are designed for su rv ivability during close air suppor t and can sur vive dir ect hits fr om

armor-piercing and high- explosive pr ojectiles up to 23mm. Sophisticated avionics

equipment includes communications , iner tial na vigation systems ,  r e contr ol and

we apons deliv ery system s,tar get penetration aids and night vision goggles . W eapons

delivery systems include a 30mm GA U-8/A Gatling gun that  r es 3,900 r ounds a

minute. In the GulfWa r, A-10s had a mission capable rate of 95.7 per cent,  e w 8,100

sorties, and launched 90 per cent of the A GM-65 Mav erick missiles . T hey w ere r esponsible for 60 per cent of AF  g hter- destroyed targets in O peration Iraqi F reedom.

CONTRACTOR S

Prime:System Integration, EM D, 

Production and Sustainment 

- L ockheed Mar tin Systems 

Integration (N Y) 

Su bcontractor(s): Integration and 

Analysis/Structures - South we st

Research Institute ( TX); Operational

Flight Programs/A vionics - British 

Aerospace Systems (N Y) 

SPECIFICA TION S

We ight 51,000 lb . (22,950kg. )

Range 800 miles (695 nautical miles) 

Armament

One 30 mm GA U-8/A sev en-barre l Gatling gun with o ve r

1150 r ounds of ammunition. Up to 16,000 lb . (7,200kg. )

of mix ed or dnance on eight under-wing and thr ee under -

fuselage pylon stations , including 500 lb . (225kg. ) M k- 82

and 2,000 lb . (900kg. ) Mk -84 series low/high drag bombs ,

incendiary cluster bombs , combined e e cts munitions ,

mine dispensing munitions , A GM-65 Ma ve rick missiles and

laser-guided/electro- optically guided bombs; infrar ed countermeasure  ares; ele ct ronic countermeasur e cha ; jammer 

pods; 2.75-in. (6.99 cm.) r ockets; illumination  ares; and

AIM-9 Sidewinder missile s. 

Dimensions Le ngth: 53 ft ., 4 in. (16.16 m); Height: 14 f t. , 8 in. (4.42 m); 

Wi ngspan: 57 ft ., 6 in. (17.42 m )

Po we r Plant Tw o General Elec tric T F34-GE-100 turbofans 

Thrust 9,065 lb . each engine 

Spee d 420 miles per hour (Mach 0.56) 

Ceilin g 45,000 ft . (13,636 m) 

Cr ew On e

ACQUISITION S TA TUS

Program Statu s Modi cation and sustainment; p ro ject ed in ve ntor y - 356 

Unit Assignment Wo rldwide

Current Inv entory 356 (58 per cent A ct ive, 14 percent Air F orce Reser veC ommand ( AFRC), 28 per cent Air National Guard ( ANG)

Future Upgrade s

Precision Engagement (PE) Spiral 2, Ex tended Infrared

CounterMeasures (IRCM), Situational A wareness Data Link

(SADL), Multi-F unctional Information Distribution Systems 

JointTa ctical Radios (MIDS- JTRS), and Mode S/5.T he P ro pulsion Upgrade Pr ogram (PUP) will enter Systems Design and

Demonstration (SDD) phase in FY06. 

MISSION

26 UNITED STATES AIR FORCE

GLOBAL

POWER

THE AIR FORCE HANDBOOK 2007 27

A-10/OA-10 ThundERBOLT II STRATEGIC CAPABILITY

A-10/OA-10 ThundERBOLT II

mIssIOn

Provide Close Air Support (CAS) and Forward Air Control (FAC) supporting 

the land battle, including Special Forces, and provide Combat Search 

and Rescue (CSAR) and interdiction under certain circumstances.

dEscRIPTIOn

The A-10/OA-10 Thunderbolt II has excellent maneuverability at low air speeds and is 

a highly accurate weapons delivery platform. Using Night Vision Imaging Systems 

(NVIS), A-10/OA-10 pilots can conduct their missions during darkness. Thunderbolt IIs 

are designed for survivability during close air support and can survive direct hits from 

armor-piercing and high-explosive projectiles up to 23mm. Sophisticated avionics 

equipment includes communications, inertial navigation systems with embedded 

GPS capability, fire control and weapons delivery systems, target penetration aids, 

and night vision goggles. Weapons delivery systems include a 30mm GAU-8/A 

Gatling gun that fires 3,900 rounds per minute. In the Gulf War, A-10s had a mission 

capable rate of 95.7 percent, flew 8,100 sorties, and launched 90 percent of the AGM65 Maverick missiles used. These aircraft were responsible for 60 percent of Air Force 

fighter-destroyed targets in Operation Iraqi Freedom (OIF). All A-10s are being 

upgraded to A/OA-10C models by incorporation of the Precision Engagement modification, which extends through FY09. This modification integrates the A-10 avionics 

systems with a digital data link and a targeting pod. Other added capabilities include 

Joint Direct Attack Munition (JDAM) and Wind Corrected Munitions Dispenser 

(WCMD) weapons employment, a MIL-STD-1760 data bus, a digital stores management system, and Hands On Throttle And Stick (HOTAS) controls.

cOnTRAcTORs

Prime:System Integration, EMD, 

Production and Sustainment

- Lockheed Martin Systems 

Integration (NY)

Subcontractor(s): Integration 

and Analysis/Structures - Northrop 

Grumman (NY)

sPEcIfIcATIOns

Weight 51,000 lb. (22,950 kg )

Range 800 miles (695 nautical miles)

Armament

One 30 mm GAU-8/A seven-barrel Gatling gun with over 

1,150 rounds of ammunition. Up to 16,000 lb. (7,200 kg ) 

of mixed ordnance on eight under-wing and three underfuselage pylon stations, including 500 lb. (225 kg ) Mk-82 

and 2,000 lb. (900 kg ) Mk-84 series low/high drag bombs, 

GBU-31/32/38 Joint Direct Attack Munitions, incendiary 

cluster bombs, combined effects munitions, Wind Corrected 

Munitions Dispensers, mine dispensing munitions, AGM-65 

Maverick missiles and laser-guided/electro-optically guided 

bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-in. (6.99 cm) rockets; 

illumination flares; and AIM-9 Sidewinder missiles.

Dimensions Length: 53 ft., 4 in. (16.16 m); Height: 14 ft., 8 in. (4.42 m); 

Wingspan: 57 ft., 6 in. (17.42 m)

Power Plant Two General Electric TF34-GE-100 turbofans

Thrust 9,065 lb. each engine

Speed 450 miles per hour (Mach 0.75)

Ceiling 45,000 ft. (13,636 m) 

Crew One

AcquIsITIOn sTATus

Program Status Modification and sustainment; projected inventory—356

Current Inventory 356 (58 percent Active, 14 percent Air Force Reserve Command (AFRC), 28 percent Air National Guard (ANG))

Future Upgrades

Precision Engagement (PE), Extended Infrared CounterMeasures (IRCM), Situational Awareness Data Link (SADL),Wing 

Replacement Program, and Mode S/5. 

TITLE: All systems are in alphabetical order. OPERATIONAL ROLES: 

See detailed explanation below. MISSION: How the system benets 

Airmen, combatant commanders, 

support personnel, and the overall 

achievement of Air Force strategies

CONTRACTORS: A listing of 

prime and subcontractors 

DESCRIPTION: A general explanation 

of the system and its key capabilities 

SPECIFICATIONS: A listing of technical 

and functional parameters 

ACQUISITION STATUS: The status of 

the system program, including the 

locations assigned, the current 

inventory, and a listing of key future 

upgrades to the system 

OPERATIONAL ROLES (explanation of icons)

The Air Force is leveraging its core strategic capabilities—Global Power, Global Reach, Global 

Vigilance, and Agile Combat Support—to ensure joint air, space, and cyberspace dominance; 

strengthen joint warfighting capabilities; and implement Total Force Integration.

Global Power

Global Power is the Air Force’s ability to control air and space—exploiting the medium to deliver 

a precise, tailored effect anywhere on the planet. Stealthy platforms and the precision-guided 

munitions they deliver provide a capability that is persistent, precise, survivable, and able to 

produce tactical, operational, and strategic effects.

THE AIR FORCE HANDBOOK 2007 VII

How to use this book

How to 

use this 

book
VIII UNITED STATES AIR FORCE

Global Reach

Global challenges demand global responses. Whether they are humanitarian, military, or a mix 

of both, the Air Force meets these demands with an airlift and tanker fleet that has global reach. 

Global Reach provides the capability to move people and equipment across the world quickly, 

ensuring the right force—anywhere, anytime.

Global Vigilance

An accurate picture of the battlespace is critical to understanding and confronting challenges to 

our national security. Roughly 33 percent of the Air Force budget is dedicated to the sensors that 

collect imagery, de-conflict air and space assets, listen to adversary communications, enable 

precise navigation, and develop actionable intelligence. Global Vigilance provides the “network” 

that binds together joint and interagency players, ensuring our Nation’s ability to see first, think 

first, and act first.

Agile Combat Support

Agile Combat Support refers to systems that enable the Air Force to provide the key strategic 

capabilities (Global Power, Global Reach, Global Vigilance) to the Joint Team.

How to use this book
United States Air Force 

The Chief’s Priorities

We are at a critical juncture in the history of the United States Air Force. We find 

our service, our department, and our Nation in a transition period that will shape 

the nation’s security for years to come. Tomorrow’s expeditionary Air Force will be 

even greater than today’s—more agile, more compact, and more effective than 

ever—ensuring global Air, Space, and Cyberspace dominance for the United States in 

the 21st Century.

America’s Air Force, as a total force of Active Duty, Air National Guard, Reserve, and 

Civilian, continues to prosecute the Global War on Terror while remaining ready to 

engage whatever enemy chooses to confront the world’s preeminent Air, Space, and 

Cyberspace force. 

 In order to continue our legacy as the world’s best Air Force, we have developed 

and instituted a set of priorities that are central to our Joint warfighting success. By 

focusing on these priorities—Winning the Global War on Terror, Developing Airmen, 

and Recapitalizing and Modernizing the Total Force—we are prepared to face the 

challenges of today and the uncertainties of tomorrow.

Winning the Global War on Terror

The Global War on Terror (GWOT) constitutes a U.S.-led response to global terrorism. 

Our mission within this war is to defeat terrorists whose tactics and global vision 

encompass extremism, tyranny, and oppression. Our enemies in this conflict are 

constantly evolving. To fight them, we must remain vigilant in our pursuit of ensuring the continued safety and security of our nation and her citizens. The Air Force is 

THE AIR FORCE HANDBOOK 2007 
 UNITED STATES AIR FORCE

committed to this mission and will continue to project its many unique capabilities 

to defeat our enemies anywhere in the world. Maintaining combat readiness is a key 

factor in supporting the GWOT. We must sustain our critical mission areas of Global 

Vigilance, Global Reach, and Global Power, while continually maintaining an agile, 

adaptable, persistent, lethal, and surge-ready air, space, and cyber force. 

For more than 16 consecutive years, the Air Force has taken the fight to hostile forces 

around the world while maintaining a constant combat posture. We continue our 

combat contributions through ongoing actions in Operation Noble Eagle (ONE), 

Operation Enduring Freedom (OEF), Operation Iraqi Freedom (OIF), and the GWOT.

This “Long War,” with its ongoing support to the Combatant Commander is changing 

the way we operate. While continuing to support the nation’s efforts at home and 

abroad, we must continue to learn through Joint lessons how to further fight and 

defeat terrorism globally. The character and capabilities of our enemies are increasingly uncertain, veiled, growing, and constantly changing. Air, Space, and Cyberspace 

must wield the capabilities necessary to dissuade potential adversaries and rapidly 

overcome them if needed. The Air Force maintains and continues to reinforce these 

global capabilities to secure America’s future security. 

Developing Airmen

Today’s challenging global environment necessitates capable leaders at all levels to 

ensure the success of our force. Our Airmen are engaged in a dizzying array of missions today, ranging from operating satellites in deep space, applying air power to 

the battlefields of Afghanistan and Iraq, maintaining air defense of the skies over 

the United States, launching Air Mobility Command aircraft approximately every 90 

seconds, 24/7, 365 days a year, to directly supporting humanitarian missions around 

the globe. The methodical steps to develop these well-rounded Airmen begin the 

moment they take the oath of office, accepting the Core Values—Integrity First, 

Service Before Self, and Excellence in All We Do. These core values are what defines us 

as Airmen and empowers us to learn from our forefathers and accept the responsibilities and challenges of the future. 

In place or deployed, our Airmen and their families are our most important priority 

and the key to our continued success. Maintaining peak combat capability begins and 

ends with smart, healthy, motivated, trained, and well-equipped Airmen. To this end, 

we have a continued need to recruit, retain, equip, and train our entire force. These 

challenges are great and the stakes are incredibly high. While we give Airmen leaders 

the tools they need to overcome even the greatest odds, we must continue to look for 

new and innovative ways to maintain and improve our training, personal and professional education, and quality of life to meet today’s commitments while preparing for 

the challenges of tomorrow. 
THE AIR FORCE HANDBOOK 2007 

We are a seamlessly integrated and expeditionary Total Force transparently composed 

of Active Duty, Air National Guard, Air Force Reserve, and Civilians. Our Total Force is 

what makes the Air Force unique. Flying high over our cities are fighter, refueling, and 

airlift aircraft providing everything from Presidential support, Homeland Defense, 

Humanitarian relief, GWOT support, to training missions; all fly the same aircraft and 

all aircrew wear the same uniform. There are subtle differences. These Airmen can be 

active duty Airmen, airline pilots, teachers, doctors, or your neighbors performing 

part-time duty as Air Force Reservists or Air National Guard Airmen. 

To continue our expeditionary success, we deliberately develop Airmen with international insight, foreign language proficiency, and cultural understanding to enhance 

our effectiveness in a dynamic international environment. All Airmen must have the 

right skill sets to understand the specific regional context in which Air,Space, and 

Cyberspace power may be applied. 

Knowledge is power and empowering our Airmen is what sustains the United States 

Air Force as the world’s premier Air Force.

Recapitalization and Modernization

Since the drawdown shortly after the Cold War, the size and shape of the Air Force 

has changed considerably. This new force demands high-tech, highly reliable weapon 

systems and equipment to meet the requirements of the Combatant Commanders. 

Due to continuing wartime engagement and new requirements in the Global War 

on Terror, the Air Force has been forced to make tough fiscal decisions. Since the 

early 1990s, the Air Force has been forced to contend with aging, less capable, more 

resource-intensive equipment which reduces the available resources with which 

more modern, maintainable, deployable, survivable, and lethal systems can be 

procured. This cycle continues to strain the most effective Air Force in the world, and 

we struggle to find the optimal balance between providing capability to fight today 

while transforming and modernizing our force to meet the challenges of tomorrow.

Within the Department of Defense (DoD), it is the Air Force’s unique responsibility 

to provide the nation true Global Vigilance, Global Reach, and Global Power. The Air 

Force supplies to the nation a global expeditionary force that is persistent, focused, 

and predictive. That force retains its reliable, rapid, and agile reach and power 

through precisely directed stealthy and decisive tactics. Our job as Airmen is to fight 

the ongoing GWOT while being able to reach anywhere on the planet, dramatically 

dislocating an enemy’s tactical options, strategic posture, and decision-making. To 

continue to make this happen for the 21st Century, we need modern, 21st Century 

equipment in the hands of our 21st Century Airmen. 

Our enemies and potential adversaries do not stand idle. They are working day and 

night to devise new ways to confront American air, space, and cyberspace power. Yet, 

we operate the oldest air and space inventories in the history of the United States Air 

Force. Therefore, it is absolutely imperative that we recapitalize and replace our aging 

the Chie

f’s Priorities
 UNITED STATES AIR FORCE

aircraft and spacecraft to ensure our dominance across the warfighting domains. We 

must acquire and modernize systems that will secure America’s freedom to maneuver, 

operate, and command and control expeditionary Joint forces in the face of emerging, highly sophisticated threats. 

Systems such as: the aerial refueling tanker—the KC-X; the combat search and 

rescue replacement vehicle—the HH-47H (formerly called CSAR-X); modern spacebased early warning and communications capabilities; the F-35 Lightning II Joint 

Strike Fighter; Long Range Strike; the MQ-1 Predator, MQ-9A Reaper, and RQ-4A/B 

Global Hawk unmanned aerial systems (UASs); the CV-22 Osprey and other modernized special operations forces (SOF) platforms; the right number of C-130J Hercules; 

and F-22A Raptors to strengthen our air dominance.

We’ll do this all while looking at options to develop Joint Cargo Aircraft to augment 

our intra-theater airlift requirements and expanding our global Intelligence, Surveillance, and Reconnaissance (ISR) capabilities in air, space, and cyberspace.

We will aggressively recapitalize and modernize our inventories of aircraft, satellites, 

and equipment, as well as our operational infrastructure, to meet the needs of our 

nation at war while providing a future Air Force that is the world’s undisputed best, 

whether the challenge be a protracted urban counterinsurgency or an intense conventional conflict with a high-tech competitor.

Fiscal responsibility is a critical element of our plan and we will progressively shed 

less capable legacy systems while reinvesting in a smaller, more capable, more 

expeditionary force with powerful global cyberspace capabilities. In essence, our 

recapitalization and modernization plan maintains our momentum in transforming 

the agility, speed, range, precision, and lethality of the entire Joint team.

Summary

As global threats continue to increase, the Air Force is poised to face the challenge. To 

accomplish our mission, we have designated our priorities: maintaining a razor-sharp 

focus on fighting the GWOT, developing our Airmen into capable leaders at all levels, 

and recapitalizing and modernizing our Total Force. 

Meeting these challenges will require bold new initiatives. Our Airmen understand 

these intuitively, and will ensure our nation’s asymmetric advantages through an 

agile, adaptable, persistent, lethal, and surge-ready air, space, and cyberspace force. 

We remain steadfast in our commitment to fly, fight, and win our nation’s wars.
THE AIR FORCE HANDBOOK 2007 

the Chie

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The mission of the U.S. Air Force is clear. As threats 

change and America’s interests evolve, the Air Force 

will continue to adapt and evolve. It will remain 

the world’s premier air and space force. Together 

with its fellow Services, it stands resolute, committed to defending the United States and defeating 

America’s enemies.

THE AIR FORCE HANDBOOK 2007 

MAINTAINING AMERICA’S EDGE

As we maintain our focus on our mission and top priorities, America’s Air Force faces 

significant challenges. Over the past 16 years, the Air Force has become a smaller, 

leaner, and more capable force—while simultaneously engaged in combat operations around the world. We continue transforming our force to guarantee that we 

will dominate air, space, and cyberspace now and into the future. Fiscal constraints, 

in addition to other challenges, translate into risks we must continue to manage and 

mitigate in order to provide the air, space, and cyberspace capabilities America needs.

Modern warfare is changing—this is nothing new to America’s Airmen, whose 

heritage spans and embraces change and whose service culture embodies courage 

and innovation for America. We will ensure a lean, lethal, and agile force, structured 

to meet future emerging threats on a dynamic world stage, and to meet our obligations as a Joint, interdependent force.

TheChanging Security Environment

America’s adversaries continue to find new and creative means with which to challenge U.S. primacy in the air, space, and cyberspace domains. While we have successfully leveraged technology in our favor to maintain our position at the leading edge 

in the development of both offensive and defensive capabilities, we can ill-afford to 

drop our guard now. 

Meeting the Global Security Challenge
 UNITED STATES AIR FORCE

Integrated air defense systems (IADs) and surface-to-air missile systems (SAMs) 

continue to evolve. IADs are incorporating more sources of data and increasing the 

speeds at which information is passed. Proliferation of these more capable systems is 

increasing. 

One of the greatest rising threats is the man-portable air defense system (MANPADS). 

The proliferation of MANPADS increases the likelihood they may end up in the hands 

of non-state actors, thereby endangering U.S. civil and military aircraft.

Access to Weapons of Mass Destruction (WMDs) by countries with advanced military 

capabilities remains a significant challenge to U.S. interests. Easier and less costly to 

make than nuclear weapons, chemical and biological weapons and technology may 

proliferate more easily and their manufacture can be hidden in civilian industry. 

As technology proliferates and access to space becomes available to more countries, 

organizations, and individuals, the threats to air, space, and cyberspace capabilities 

will become more prevalent and effective in the battlespace. 

Adapting to Non-Traditional Roles

Airmen increasingly engage in non-traditional roles requiring ingenuity and the use 

of Joint warfighting technology. Our missions and taskings range from typical ones 

like close air support and armed reconnaissance to non-traditional taskings such as 

infrastructure protection and election support.

Due to the demands of the Global War on Terror (GWOT), Airmen have increasingly 

augmented ground forces to provide security and stability in Iraq and Afghanistan. 

We are working hand-in-hand with ground and naval forces in training both Iraqi 

and Afghan security forces, rebuilding critical infrastructure, and providing medi-
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THE AIR FORCE HANDBOOK 2007 

cal services to these war-torn countries. Additionally, our Airmen provide detainee 

operations, convoy operations and protection, Explosive Ordnance Disposal, Police 

Training Teams, Military Transition Teams, civil engineering, security, interrogators, 

communications, fuels, medical, logistics, intelligence, and base operating support. 

Lessons learned during OEF and OIF jumpstarted Air Force development and optimization of a family of specialties, known as Battlefield Airmen, encompassing the 

Terminal Attack Control, Combat Control, Pararescue, and Special Operations Weather 

functional areas. Through ingenuity and technology, these Airmen designate targets, 

control aircraft, rescue and recover personnel, and gather vital combat-meteorological data. They facilitate the fullest possible extent of air and space power exploitation 

for Joint and coalition ground forces. 

We must continue to train and equip our Battlefield Airmen with the most technologically advanced systems and equipment and look for opportunities to standardize 

equipment for all Expeditionary Airmen. Ultimately, these efforts will expand the 

Joint Force Commander’s (JFC) ability to employ battlefield air and space professionals who bring unequaled accuracy, responsiveness, flexibility, and persistence to the 

Joint warfight. 

Loss of Buying Power

Although faced with tightening fiscal realities and other substantial challenges, we 

continue to balance our priorities of winning the GWOT, taking care of our Airmen and 

their families, and recapitalizing and modernizing our force.

We face demands on our resources that were unforeseeable. These demands require some very tough internal choices. Our current challenging fiscal environment 

includes the cost of a long war, reduced Air Force total obligation authority (TOA), 

absorbing inflation factors in key areas (fuel, utilities, manpower, aircraft ownership) 

that reduce overall buying power and lost savings due to Congressional restrictions 

on retirement of aging aircraft.

In 2006, the Air Force TOA for FY08–13 was reduced by approximately $12.4 billion. 

This loss of buying power reduced Air Force Program content by an additional $10 

billion per year. Base Realignment and Closure (BRAC) in 2005 produced a “must-pay” 

bill to the Air Force on the order of $1.8 billion. Over the past decade personnel costs 

increased by 51 percent, while fleet Operations and Maintenance (O&M) costs rose by 

87 percent.

Responding TO the Challenge

While we remain continuously and globally engaged, we recognize the imperative 

of investing in the future through recapitalization and modernization programs to 

maintain our momentum in transforming the agility, speed, range, precision, and 

lethality of the entire Joint team. We are committed to long-term transformation 
10 UNITED STATES AIR FORCE

of Total Force Integration, including reorganization and fielded Joint capabilities, to 

ensure a force structure with expanded capability to combat conventional threats 

while continuing to wage the GWOT.

Recapitalization and Modernization

The Air Force has over 6,000 aircraft in its inventory; however, a significant number 

operate under flight restrictions. Many transport aircraft and aerial refueling tankers 

are more than 40 years old, the average age of the bomber force exceeds 30 years, 

and the fighter force is the oldest it has ever been, at more than 18 years average 

age. The Air Force is experiencing multiple effects of use and aging across its force 

structure, including engine and structural fatigue, deterioration, and corrosion. The 

increased tempo of current operations delays routine maintenance and we find our 

systems becoming progressively less effective even as they become more costly to 

maintain and operate.

To solve this critical problem, we have adopted several targeted recapitalization, acquisition, and modernization strategies. We will transform to a smaller, more capable 

force by retiring our oldest, most costly, and least capable legacy aircraft. We will 

leverage technology to increase our capabilities while also seeking to reduce support 

costs to mitigate aging aircraft issues. We will continue to challenge the aerospace 

industry to shift its focus to recapitalization and produce more cost effective and 

supportable aerospace systems. 

Together, these strategies will sustain selected legacy systems for the Long War 

and beyond. Simultaneously, they will allow effective, efficient modernization and 

replacement of our air superiority, strike, space, mobility, special operations, and 

combat support systems, enabling the Air Force to conduct modern, networked, 21st 

Century warfare.

America’s Airmen execute a broad spectrum of missions across three warfighting 

domains. We are pursuing a large number of acquisition and modernization programs, designed to enhance Joint capabilities across the spectrum of global missions. 

These programs include the aerial refueling tanker–the KC-X; the combat search and 

rescue replacement vehicle–the HH-47H (formerly called CSAR-X); modern spacebased early warning and communications capabilities; the F-35 Lightning II Joint 

Strike Fighter; and Long Range Strike modernization. While diverse in function and 

execution, all Air Force capability efforts share common elements. All are global. All 

are expeditionary. All are transformational, and all are vital to current and future Joint 

success.

Air Force Smart Operations for the 21stCentury (AFSO21)

To meet the process challenges of the road ahead, we have embarked on an Air Forcewide journey embracing Continuous Process Improvement. Air Force Smart Operations for the 21st Century (AFSO21) embraces many concepts developed and proven 

in industry—Lean, Business Process Re-engineering, Six Sigma, and Theory 
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THE AIR FORCE HANDBOOK 2007 11

of Constraints methodologies—and strives to improve daily processes by identifying 

and eliminating activities, actions, and policies that do not contribute to the efficient 

and effective operation of the Air Force.

These process changes have occurred at every level of the Air Force resulting in 

resource savings. We have more work to do, but we believe that institutionalizing 

Continuous Process Improvement into our daily operations will allow us to meet the 

enormous challenges of the next decade and ultimately sustain and modernize the 

world’s best air, space, and cyber force. 

TotalForce Integration (TFI)

One of the Air Force’s more significant commitments to long-term transformation 

is Total Force Integration (TFI). Our Total Force partners in the Active Duty Air Force, 

Air National Guard, and Air Force Reserve are working together to maximize the Air 

Force’s overall Joint combat capability. 

Total Force initiatives integrate Air Force components into missions critical to future 

warfighting: ISR, Unmanned Aerial System (UAS) operations, and space operations. 

These missions are ideally suited for the Guard and Reserve. The reserve component 

also provides support to the Joint warfighter from U.S. locations. Using this Total 

Force approach improves our operational effectiveness, decreases our overseas 

footprint, reduces reliance on involuntary mobilization, and provides more stability 

for our Airmen, their families, and their civilian employers. 

Reorganizing for Increased Interdependence

In our ongoing effort to provide the JFC greater ability to integrate air, space, and 

cyber capabilities in support of National Security objectives we continue to transform 

our command and control structures.
12 UNITED STATES AIR FORCE

By establishing component Numbered Air Forces (NAFs), we provide an integrated 

and technologically advanced command and control capability for each Combatant 

Commander (COCOM). Over the next several years, we will continue to mature this 

command and control structure through development of centralized “reach back” 

capabilities, Total Force augmentation, and more advanced command and control 

systems.

The Air Force also organizes its combat forces into ten Air & Space Expeditionary Force 

(AEF) elements that allow us to fill COCOM requirements, provide trained and ready 

forces for emerging threats/contingencies, and manage our people by providing 

them as much stability and predictability as possible while executing the Long War 

against terror.

As we reduce garrisoned overseas bases, the Air Force will increasingly operate 

from expeditionary air bases. Having transformed over the past 16 years to an AEF 

construct and culture, we continue to innovate and evolve with new expeditionary 

concepts.

Fielded JointCapabilities

Fifth Generation Fighters—To meet the nation’s air power requirement to gain and 

maintain air dominance, as well as enable surface and sub-surface operations, the 

Air Force is fielding the Fifth Generation Fighters. These fighters combine stealth, 

maneuverability, and integrated avionics to ensure multi-role, full spectrum Joint air 

dominance, especially for Homeland Defense, the GWOT, and Major Combat Operations (MCOs). The F-22A Raptor and the F-35 Lightning II reap the benefits of decades 

of advanced research and development and field experience and deliver improved 

survivability, lethality, supportability, and sustainability. The F-22A is in full-rate 

production, participates in Homeland Defense missions and Joint training exercises, 

and is scheduled to deploy this year as part of the Air Force’s AEF.
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THE AIR FORCE HANDBOOK 2007 13

Air Operations Centers (AOCs)—The information superiority of our Air Operations 

Center (AOC) Weapon Systems enable decision-makers to focus and synchronize our 

air and space superiority, global attack, precision engagement, and rapid global 

mobility capabilities across the full range of military operations in multiple, geographically separated arenas. The Air Force is leading the way in delivering sovereign 

options to defend the homeland and our global interests by providing a global command and control (C2) capability to JFCs, enabling them to orchestrate Air, Space, and 

Cyberspace effects in pursuit of national military objectives. Our AOCs are the central 

operational nodes in this capability, and the Combined AOC at Al Udeid exemplifies 

the most advanced and robust AOC system in the Air Force today. 

Fostering Interdependence

The Air Force is committed to our nation’s Joint Force construct and works daily with 

our sister services to provide Air, Space, and Cyberspace to COCOMs around the world. 

While the other services rely on the Air Force for Global Vigilance, Global Reach, and 

Global Power, we also rely on the other services to support our combat capabilities. 

On a daily basis, Air Force mobility forces support all branches of the Department of 

Defense (DoD) as well as other government operations around the world. Increased 

demand and decreased availability map a future that demands further recapitalization and investment to ensure the viability of this national capability. Without it, our 

national defense, global presence, and global power are at increased risk.

Interdependence is needed to leverage sensor information on current and next generation aircraft and to expand and advance the airborne network. Extended machineto-machine interfaces between aircraft, C2 nodes, and ground forces will enhance the 

Air Force’s ability to provide and improve situational awareness across the Joint team.

SpaceCapabilities for Joint Operations

The U.S. depends upon the Air Force to supply critical space capabilities to meet not 

only the needs of Joint operations worldwide, but also national missions using the 

instruments of diplomatic, informational, military, and economic power. 

Operations in Iraq and Afghanistan highlight the importance of space-based C4ISR 

capabilities to U.S. and coalition forces. Commanders are operating in the most challenging electronic environment ever encountered in combat. The deployment of the 

Satellite Interference Response System (SIRS), a defensive counterspace prototype, 

has aided in the identification, geolocation and reduction of interference sources 

on critical satellite communications. Joint Blue Force Tracking has fundamentally 

changed ground warfare in the fight against terrorists by providing unprecedented 

real-time knowledge of friendly force locations. Night and urban operations are less 

dangerous and more effective when utilizing the tracking systems, which rely on GPS 
14 UNITED STATES AIR FORCE

and satellite communications. Additionally, GPS-aided munitions allow precision 

strike and reduce collateral damage. All space capabilities are key to maintaining U.S. 

asymmetric advantages in the GWOT.

The Joint Warfighting Space (JWS) concept is a critical element within the broader Air 

Force Operationally Responsive Spacelift (ORS) effort to develop the ability to rapidly deploy and employ communication, ISR, and other space capabilities. JWS will 

emphasize agility, decisiveness, and integration and will continue to explore ways of 

achieving new, more effective ways of providing space capabilities and effects to the 

Joint warfighter. 

The Space AOC, under the auspices of 14th Air Force at Vandenberg AFB California, 

serves as the core of U.S. Strategic Command’s (USSTRATCOM) Joint Space Operations 

Center (JSpOC). The Space AOC/JSpOC is the primary command and control node for 

military space operations and Joint space operations in theater contingencies. The 

Space AOC/JSpOC consists of personnel, facilities, and resources providing long-term 

strategy development, short-term crisis and contingency planning, and real-time 

execution, reallocation, and assessment of space forces in order to provide tailored 

space effects to Joint forces worldwide. One of the main focus areas of the JSpOC is 

to maintain space situational awareness (SSA) through the fusion of intelligence, 

space-based and ground-based sensor readings, and operational indications in order 

to allow U.S. and allied forces unfettered access to space capabilities.

Cyberspace

As Airmen, we are the nation’s premier multi-dimension maneuver force, with the 

agility, reach, speed, stealth, payload, precision, and persistence to deliver global effects at the speed of sound and the speed of light. Control of the Air, Space, and Cyber 

domains provides the essential bedrock for effective Joint operations—securing 

freedom from attack while ensuring freedom to attack.

In 2005 we revised the Air Force mission statement to include cyberspace. This explicit 

mention of cyberspace reflects the recognition of cross-domain interdependence and 

emphasizes our non-negotiable commitment to deliver sovereign options for the U.S. 

through dominance of Air, Space, and Cyberspace.

Cyber dominance goes beyond communications and information technology. It requires superiority across the entire electromagnetic spectrum—radio waves, microwaves, infrared, x-rays, directed energy, and applications we have yet to discover and 

exploit. A new Cyberspace Command will stand along side Air Force Space Command 

and Air Combat Command as the providers of forces that the President, COCOMs, and 

the American people can rely on for preserving the freedom of access and commerce 

in Air, Space, and now Cyberspace.
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Acquisition Reform

The Air Force continues to streamline the acquisition process to provide more efficient 

and responsive services to the warfighter. A number of completed and ongoing 

projects have contributed to the improvement of acquisition. We’ve revitalized the 

Acquisition Strategy Panel (ASP) to provide a systematic approach to develop an 

effective acquisition program roadmap and established the Air Force Review Board 

(AFRB) to fulfill the recognized need for a structured, consistent, and repeatable AF 

process that ensures milestone decisions and documentation. Additionally, we’re 

evaluating Defense Acquisition Performance Assessment (DAPA) recommendations 

for improving the acquisition system, and prototyping the Probability of Program 

Success (PoPS) model to better analyze risk in the initiation and execution of a program. Initiatives like these, combined with the overarching philosophy of AFSO21, are 

designed to improve the efficiency of an acquisition system that produces the best 

weapon systems in the world.

Summary 

September 18, 2007 will mark the 60th Anniversary of the creation of our United 

States Air Force. This year, we commemorate this anniversary of our proud service—

born of revolutionary ideas, forged in combat, and proven through decades of progress and achievement. The mission of the Air Force remains to fly and fight—in the 

Air, Space, and Cyberspace. Our legacy inspires us. Our mission propels us. Our Core 

Values guide us. We have received and will continue to build upon a proud heritage 

shaped through the ingenuity, courage, and resolve of the Airmen who preceded us. 
16 UNITED STATES AIR FORCE
THE AIR FORCE HANDBOOK 2007 17

The Air Force is deployed around the world in support of the Global War on Terrorism 

and other critical operations. In Operations Enduring Freedom (OEF) and Iraqi Freedom (OIF), the Air Force has flown more than 430,000 sorties, or approximately 80 

percent of the total coalition air effort. Aviation missions ranged from airlift and aeromedical evacuation, to close air support, interdiction, and intelligence, surveillance, 

and reconnaissance. During combat missions in 2006, Air Force fighters and bombers 

delivered approximately 1,500 munitions (bombs), approximately 90 percent of 

which were precision-guided, such as the Joint Direct Attack Munition (JDAM). The 

percentage of guided munitions used remained approximately the same as 2005. The 

Airmen of the Air Force have also provided nearly all of the in-flight refueling for the 

Joint and Coalition Forces.

Reconnaissance and Imagery. Leading the way in reconnaissance and imagery, 

the Air Force is currently flying Predator UAV missions 24 hours a day, 7 days a week. 

The capacity of Predator UAVs will increase from 10 orbits in FY06 to 21 orbits by 

FY10 to meet growing requirements. Predator aircraft are able to transmit live video 

pictures to ground-based targeting teams equipped with the Remote Operations 

Video Enhanced Receiver (ROVER) system. Linking Global Power and Global Vigilance 

capabilities to forces on the ground, ROVER has been used repeatedly to detect, 

target, and destroy improvised explosive devices (IEDs) and disrupt other insurgent 

activities across the region. Additionally, the Air Force continually adapts the employment of ISR sensors and analysis methods to optimize force protection and identify 

suspected terrorist activities. This includes using non-traditional ISR missions and 

applying change detection methodologies to detect possible IED emplacements.

2006 AIR FORCE

Crisis Response and Combat Actions
18 UNITED STATES AIR FORCE

Operation Enduring Freedom (OEF)

Overview

• OEF began on October 7, 2001. Since then, the Air Force team—Active Duty, Guard, 

Reserve—has flown more than 157,000 sorties.

• Air Force bombers, fighters, airlifters, tankers, and ISR assets remain in action daily.

U.S. Air Force Operations

• USAF B-1s, B-2s, B-52s, F-15Es, F-16s, A-10s, and AC-130s have flown more than 

75 percent of all OEF combat missions in Afghanistan, dropping more than 31,700 

munitions –10,200 tons.

• Throughout combat operations in Afghanistan, the Air Force has flown more than 

24,295 airlift missions (101,815 sorties). These missions have moved more than 

930,383 passengers and more than 615,096 tons of cargo in support of Afghan 

theater operations.

• The Air Force continues to provide full spectrum air and space support. In Afghanistan and Iraq, tankers have flown more than 11,000 refueling missions supporting 

aircraft from all services.

• Aircraft providing ISR data, such as JSTARS, UAVs, Rivet Joint, U-2, AWACS, and 

Commando SOLO, have flown more than 30,000 sorties since the beginning of the 

operation.

Operation IraqiFreedom (OIF)

Overview

• OIF remains an essential part of the Global War on Terrorism (GWOT).

• The United States continues to assist the developing Iraqi Army to battle occasional 

insurgent attacks that aim to undermine the fledgling Iraqi democracy.
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THE AIR FORCE HANDBOOK 2007 19

• The U.S., coalition partners, and the Iraqi military will continue to defeat these 

insurgents and help Iraq secure its democracy.

U.S. Air Force Operations

• Combined operations have been the hallmark of operations in both Afghanistan 

and Iraq. High levels of cooperation and coordination of air power assets have 

enabled the Air Force to provide rapid response times to commanders in the theater.

• The coalition air campaign has been the most deliberate, disciplined, and precise air 

Campaign in history. Since March 2003, the Air Force has flown over 270,000 sorties.

• Since the September 11, 2001 terrorist attack on America, Air Mobility Command 

completed nearly 74,151 missions (309,193 sorties) sorties in support of Operations Enduring Freedom and Iraqi Freedom. As of December 31, 2006, organic aircraft and contracted commercial aircraft operating in the AMC system have moved 

4,916,140 troops and 2,171,120.9 short tons of cargo. The command’s KC 10 and KC 

135 tankers flew 18,370 sorties to air refuel 41,950 receiver aircraft. By the end of 

2006, the airlift operation in support of the wars in Iraq and Afghanistan remained 

history’s second largest airlift, second only to the Berlin Airlift of 1948–1949. In 

2005, Enduring Freedom and Iraq Freedom surpassed the Persian Gulf War airlift of 

1990–1991 (Desert Shield/Storm) as the second largest airlift of all time.

• ISR assets, including JSTARS, UAVs, Rivet Joint, U-2, AWACS, and Commando SOLO, 

have flown more than 7,000 missions to provide persistent battlefield awareness.

• Throughout combat operations in Iraq, the Air Force has flown more than 37,196 

airlift missions (159,125 sorties). These missions have moved more than 2,463,585 

passengers and more than 1,137,492 tons of cargo in support of Iraqi theater operations.

• America’s unparalleled space-based capabilities have given the Joint Team the 

winning edge in position navigation and timing, missile warnings, intelligence, 

surveillance, reconnaissance, and global communication in OIF and the GWOT.
20 UNITED STATES AIR FORCE

Operation Joint Guardian

Overview

• Since June 11, 1999, the United States European Command has provided U.S. forces 

and logistical support to Operation Joint Guardian, the NATO-led peacekeeping 

operation in Kosovo.

• The NATO-led Kosovo Force (KFOR) currently includes forces from the United States, 

Great Britain, France, Germany, Italy, the Czech Republic, the Netherlands, Spain, 

Poland, Greece, Turkey, Russia, Canada, and Ukraine.

• The United States is committed to supporting peace and stability in Kosovo by 

implementing the Military Technical Agreement and participating in the NATO-led 

military force.

U.S. Forces

• The United States agreed to provide a force of approximately 7,000 U.S. personnel 

as part of the NATO KFOR, providing the headquarters and troops for one of the five 

NATO sectors.

• The United States also provides personnel, units and equipment to other components of the KFOR organization. The U.S. sector (Multinational Brigade East) is in 

southeast Kosovo. Headquarters for U.S. forces is located at Camp Bondsteel, near 

Urosevic.
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Operation JointForce

Overview

• Since December 1995, the United States European Command has provided forces in 

support of NATO-led operations in Bosnia-Herzegovina.

• The United States remains committed to supporting peace in Bosnia-Herzegovina 

by implementing the Dayton Peace Accords and participating in the NATO-led 

military force.

U.S. Forces

• From a total of almost 20,000 troops at the height of NATO’s Bosnia operations in 

1996, U.S. troop levels have steadily decreased as progress continues under the 

Dayton Peace Accords.

• The United States agreed to provide a force of approximately 6,900 U.S. personnel to 

help maintain a capable military force in Bosnia-Herzegovina.

• The United States supports the NATO Stabilization Force (SFOR) by providing the 

headquarters and most of the troops for one of the three NATO-led multinational 

divisions.

• The United States also provides personnel, units, and equipment to various parts of 

the SFOR organization.

• The majority of the U.S. forces are in northeast Bosnia, in the Multinational Division 

North (MND-N) sector, with sector headquarters at Tuzla, Bosnia.
22 UNITED STATES AIR FORCE

Lebanon Noncombatant Evacuation Operation (NEO)

Overview

On July 12, 2006, Israeli tanks and troops invaded southern Lebanon after Hezbollah 

operatives killed several Israeli soldiers and captured two others. On July 14, Israeli 

air strikes targeted Hezbollah strongholds in Beirut, Lebanon’s capital city. That same 

day, Hezbollah fired more than 100 rockets into Israel. Israel responded with rockets 

and an invasion of southern Lebanon. An unrelenting, daily exchange of rockets 

continued until a United Nations ceasefire agreement took effect on August 14, 2006. 

Due to the intense fighting in southern Lebanon between the Israel military and 

Hezbollah, American citizens were ordered to evacuate by the United States Department of State. Air Mobility Command C-17s and commercial aircraft contracted by the 

Department of State transported 12,703 U.S. citizens from Cyprus and Turkey to the 

United States in the largest noncombatant evacuation operation (NEO) since Vietnam.

U.S. Forces

• 495 American citizens evacuated from Lebanon by USAF

• 1,833 American citizens evacuated to CONUS from Lebanon via military airlift

• 6,930 American citizens evacuated to CONUS from Lebanon via commercial airlift

• ~500 non-U.S. citizens evacuated from Lebanon by DoD

• 41 USAF aircraft and 500+airmen in direct support

• 80 x MH-53 sorties

• 31 x MC-130P sorties

• 3 x KC-10/135 sorties

• 157 x C-5/17/130 sorties

• 71 x AMC contract air sorties

• USAF MH-53s directly evacuated 366 passengers from Lebanon

• USAF Expeditionary Medical Support (EMEDS) treated 1,070+ patients

• Ramstein and Incirlik Air Bases processed 3,560+ passengers and fed more than 

21,000 evacuees
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KEY AIR FORCE PERSONNEL

KEY AIR FOR

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L

THE AIR FORCE HANDBOOK 2007 25

The Honorable Michael W. Wynne

Secretary of the Air Force

Room 4E540

(703) 697-7376

General T. Michael Moseley

Chief of Staff

Room 4E562

(703) 697-9225

Major GENERAL Daniel J. Darnell

Director, Legislative Liaison

Room 4C654

(703) 697-4142

Senate Liaison Office (202) 685-2573

House Liaison Office (202) 685-4531

Congressional Action Division (703) 695-1292

Weapon Systems Division (703) 697-6711

Programs and Legislation Division (703) 697-7950

Congressional Inquiries Division (703) 695-7364

Major General Frank R. Faykes

Deputy Assistant Secretary, Budget

Room 4D131

(703) 695-1875

Budget and Appropriations Liaison (703) 614-8110
MISSION

26 UNITED STATES AIR FORCE

A-10/OA-10 Thunderbolt II

mission

Provide Close Air Support (CAS) and Forward Air Control (FAC) supporting 

the land battle, including Special Forces, and provide Combat Search 

and Rescue (CSAR) and interdiction under certain circumstances.

description

The A-10/OA-10 Thunderbolt II has excellent maneuverability at low air speeds and is 

a highly accurate weapons delivery platform. Using Night Vision Imaging Systems 

(NVIS), A-10/OA-10 pilots can conduct their missions during darkness. Thunderbolt IIs 

are designed for survivability during close air support and can survive direct hits from 

armor-piercing and high-explosive projectiles up to 23mm. Sophisticated avionics 

equipment includes communications, inertial navigation systems with embedded 

GPS capability, fire control and weapons delivery systems, target penetration aids, 

and night vision goggles. Weapons delivery systems include a 30mm GAU-8/A 

Gatling gun that fires 3,900 rounds per minute. In the Gulf War, A-10s had a mission 

capable rate of 95.7 percent, flew 8,100 sorties, and launched 90 percent of the AGM65 Maverick missiles used. These aircraft were responsible for 60 percent of Air Force 

fighter-destroyed targets in Operation Iraqi Freedom (OIF). All A-10s are being 

upgraded to A/OA-10C models by incorporation of the Precision Engagement modification, which extends through FY09. This modification integrates the A-10 avionics 

systems with a digital data link and a targeting pod. Other added capabilities include 

Joint Direct Attack Munition (JDAM) and Wind Corrected Munitions Dispenser 

(WCMD) weapons employment, a MIL-STD-1760 data bus, a digital stores management system, and Hands On Throttle And Stick (HOTAS) controls.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 27

STRATEGIC CAPABILITY

A-

10/

OA-

10 

T

h

under

b

o

lt II

contractors

Prime:System Integration, EMD, 

Production and Sustainment

- Lockheed Martin Systems 

Integration (NY)

Subcontractor(s): Integration 

and Analysis/Structures - Northrop 

Grumman (NY)

specifications

Weight 51,000 lb. (22,950 kg )

Range 800 miles (695 nautical miles)

Armament 

One 30 mm GAU-8/A seven-barrel Gatling gun with over 

1,150 rounds of ammunition. Up to 16,000 lb. (7,200 kg ) 

of mixed ordnance on eight under-wing and three underfuselage pylon stations, including 500 lb. (225 kg ) Mk-82 

and 2,000 lb. (900 kg ) Mk-84 series low/high drag bombs, 

GBU-31/32/38 Joint Direct Attack Munitions, incendiary 

cluster bombs, combined effects munitions, Wind Corrected 

Munitions Dispensers, mine dispensing munitions, AGM-65 

Maverick missiles and laser-guided/electro-optically guided 

bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-in. (6.99 cm) rockets; 

illumination flares; and AIM-9 Sidewinder missiles.

Dimensions Length: 53 ft., 4 in. (16.16 m); Height: 14 ft., 8 in. (4.42 m); 

Wingspan: 57 ft., 6 in. (17.42 m)

Power Plant Two General Electric TF34-GE-100 turbofans

Thrust 9,065 lb. each engine

Speed 450 miles per hour (Mach 0.75)

Ceiling 45,000 ft. (13,636 m) 

Crew One

Acquisition status

Program Status Modification and sustainment; projected inventory—356

Current Inventory 356 (58 percent Active, 14 percent Air Force Reserve Command (AFRC), 28 percent Air National Guard (ANG))

Future Upgrades

Precision Engagement (PE), Extended Infrared CounterMeasures (IRCM), Situational Awareness Data Link (SADL),Wing 

Replacement Program, and Mode S/5. 
MISSION

28 UNITED STATES AIR FORCE

AC-130H Spectre

mission

Provide close air support, air interdiction, and armed reconnaissance.

description

The AC-130H Spectre provides close air support, air interdiction, and armed reconnaissance. Other missions include perimeter and point defense, escort, landing, drop 

and extraction zone support, forward air control, limited command and control, and 

combat search and rescue. The AC-130H model is the second generation of the C-130 

gunships. It incorporates side-firing weapons integrated with sophisticated sensor, 

navigation, and fire control systems to provide surgical firepower or area saturation 

during extended loiter periods at night. The sensor suite consists of a television sensor 

and infrared sensor. These sensors allow the gunship to visually or electronically identify friendly ground forces and targets any place, any time. The gunship’s navigational 

devices include the inertial navigation systems and GPS. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 29

STRATEGIC CAPABILITY

AC-13

0

H Sp

e

ctre

contractors

Prime: Airframe - Lockheed Martin 

(FL); Weapon System Support

- Boeing (FL); Radar - SEI (MO); 

Communications/Navigations

- Rockwell Collins (IA)

specifications

Weight 155,000 lb. (gross weight)

Range 1,300 nautical miles (NM); unlimited with in-flight refueling

Armament 40 mm Bofors Cannon; 105 mm Howitzer

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Acquisition status

Program Status Modifications only

Unit Assignment 16th Special Operations Squadron (SOS)

Current Inventory 8

Future Upgrades Multiple Modifications
MISSION

30 UNITED STATES AIR FORCE

AC-130U Spooky

mission

Provide close air support, air interdiction, and armed reconnaissance.

description

The AC-130U Spooky gunship provides close air support, air interdiction, and armed 

reconnaissance. Other missions include perimeter and point defense, escort, landing, 

drop and extraction zone support, forward air control, limited command and control 

and combat search and rescue. The AC-130U model is the third-generation of C-130 

gunships. It incorporates side-firing weapons integrated with sophisticated sensor, 

navigation, and fire control systems to provide surgical firepower or area saturation 

during extended loiter periods, at night and in adverse weather. The sensor suite 

consists of a television sensor, infrared sensor and radar. These sensors allow the gunship to visually or electronically identify friendly ground forces and targets any place, 

any time. The AC-130U employs synthetic aperture strike radar for long-range target 

detection and identification. The gunship’s navigational devices include the inertial 

navigation systems and GPS. The AC-130U employs the latest technologies and can 

attack two targets simultaneously.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 31

STRATEGIC CAPABILITY

AC-130U Spooky

contractors

Prime: Airframe - Boeing (FL); 

Integrated Weapon System 

Support - Boeing (FL); Radar - SEI 

(MO); Communications/Navigation - Rockwell Collins (IA)

specifications

Weight 155,000 lb. (gross weight)

Range 1,300 nautical miles (NM); unlimited with in-flight refueling

Armament 25 mm Gatling gun; 40 mm Bofors cannon; 

105 mm Howitzer

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Acquisition status

Program Status One additional aircraft scheduled for delivery in CY06

Unit Assignment 4th Special Operations Squadron (SOS)

Current Inventory 16

Future Upgrades Multiple modifications
MISSION

32 UNITED STATES AIR FORCE

Advanced Extremely High Frequency (AEHF) System

mission

Provide secure, survivable communications to U.S. warfighting forces 

during all levels of conflict.

description

The Advanced Extremely High Frequency (AEHF) communications system provides 

secure, survivable, anti-jam and anti-scintillation communications for strategic and 

tactical users with interoperability across services and agencies. It offers assured mission-critical strategic networks and low probability of detection and interception. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 33

STRATEGIC CAPABILITY

Adva

n

ced 

Extre

m

e

ly High Freq

uen

cy (AEHF) 

Syste

m

contractors

Prime: Lockheed Martin (CA)

Subcontractor(s): Northrop 

Grumman (CA)

specifications

Size Three-satellite constellation

Weight 13,421 lb.

Coverage Global Coverage: 65° N–65° S

Capacity/Satellite Protected EHF: 8.2 Mbps maximum data rate; 250 Mbps 

loaded throughput; 60 Mbps RF crosslinks

Compatibility

Backwards compatible to Milstar Low Data Rate (LDR) 

and Medium Data Rate (MDR) terminals; RF crosslinked to 

Milstar satellites.

Acquisition status

Program Status

Critical Design Review - 3QFY04; Follow-on buy approval for 

AEHF 3 - 3QFY04; AEHF 3 contract award - 2QFY06; Planned 

first launch - 3QFY08.

additional Information

AEHF 1 completes the Milstar satellite constellation.
MISSION

34 UNITED STATES AIR FORCE

AGM-65 Maverick

mission

Destroy armored land combat vehicles, bunkers, structures, and ships 

with minimum collateral damage.

description

The AGM-65 Maverick is a rocket-propelled, launch-and-leave, air-to-surface missile. Guidance is Television (TV) or Infrared (IR) Seeker (Navy has Laser version). 

The Maverick is a highly versatile, point-and-shoot weapon whose primary targets 

include armor, vehicles, bunkers, and air defense. There are currently eight versions 

of the Maverick. The Air Force is currently modifying existing Mavericks (B, A/G) into 

AGM-65H/K TV versions. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 35

STRATEGIC CAPABILITY

A

GM-6

5 Maveric

k

contractors

Prime: Raytheon (AZ)

Subcontractor(s): Marvin 

Engineering (TX); Moog Inc. (UT); 

Alliant Tech Systems (UT)

specifications

Weight 500 lb.

Range 10 nautical miles (NM) (H/K version)

Dimensions Length: 97 in.; Diameter: 12 in.

Warhead 300 lb. Blast/Fragmention—AGM-65G/G2/K; 

125 lb. Shaped—AGM-65A/B/D/H

Compatability Aircraft: A-10, F-16, F-15E

Acquisition status

Program Status AGM-65H/K modification production; Lot 6 being produced, 

Lot 7 to be determined.

Current Inventory 5,596 AGM-65A/Bs; 3,030 AGM-65Ds; 4,976 AGM-65G/G2s; 

1,537 AGM-65H/Ks

Future Upgrades

1,500–2,000 AGM-65Gs (IR seeker) and AGM-65Bs (EO 

seeker) will be converted to AGM-65-H/Ks respectively. The 

goal is a 70/30 mix of IR (D/G/G2) and EO (H/K).
MISSION

36 UNITED STATES AIR FORCE

AGM-86B Air Launched Cruise Missile (ALCM)

mission

Provide a highly accurate, long-range, air-to-surface strategic nuclear 

missile that can evade air and ground-based defenses to strike targets 

anywhere in the enemy’s territory.

description

The AGM-86B Air Launched Cruise Missile (ALCM) is a highly accurate, long-range, 

air-to-surface strategic nuclear missile. It carries a single W80 nuclear warhead. The 

small, winged AGM-86B missile is powered by a turbofan jet engine that propels it at 

sustained subsonic speeds. After launch, the missile’s folded wings, tail surfaces, and 

engine inlet deploy. The AGM-86B is then able to fly complicated routes to a target 

through use of a terrain contour-matching guidance system. AGM-86B missiles can 

be air-launched in large numbers by B-52 bombers. An enemy force would have to 

counterattack each of the missiles, making defense against them costly and complicated. The missiles’ small size and low-altitude flight capability make them difficult to 

detect on radar.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 37

STRATEGIC CAPABILITY

A

GM-

86B Air Lau

n

ched Cruise Missile (ALCM)

contractors

Prime: Boeing (WA)

Subcontractor(s): E-Spectrum (TX)

specifications

Weight 3,150 lb.

Range 1,500+ miles

Armament W80-1 warhead 

Dimensions Length: 20.75 ft.; Diameter: 2 ft.; Wingspan: 12 ft.

Warhead W80-1 warhead 

Coverage Global

Compatability B-52

Acquisition status

Program Status Fielded

Unit Assignment Barksdale AFB, LA; Minot AFB, ND

Future Upgrades Undergoing life extension programs
MISSION

38 UNITED STATES AIR FORCE

AGM-86C/D Conventional Air Launched Cruise Missile (CALCM)

mission

Provide an adverse weather, day/night, air-to-surface, accurate, 

stand-off, and outside-of-theater-defenses strike capability.

description

The AGM-86C/D Conventional Air Launched Cruise Missile (CALCM) provides an 

adverse weather, day/night, air-to-surface, accurate, stand-off, and outside of theater 

defenses strike capability. It is equally effective for stand-alone, clandestine/punitive 

strikes and fully-integrated theater warfare. AGM-86C uses onboard GPS coupled 

with its Inertial Navigation System (INS) to fly. This allows the missile to guide itself 

to the target with pinpoint accuracy. The AGM-86C CALCM differs from the AGM-86B 

air-launched cruise missile in that it carries a conventional blast/fragmentation 

payload rather than a nuclear payload and employs a GPS aided INS. The AGM-86D 

incorporates avionics upgrades as well as a new penetrating warhead. The AGM-86D 

penetrator is capable against a wide range of hardened, deeply buried targets.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 39

STRATEGIC CAPABILITY

A

GM-

86C/

D Con

ventional Air Lau

n

ched Cruise Missile (CALCM)

contractors

Prime: Boeing (MO)

specifications

Weight 3,250 lb. C-model/3,280 lb. for D-model

Range >500 nautical miles (NM)

Dimensions Length: 249 in.; Diameter: 24.5 in.

Warhead

3,000 lb. class, blast fragmentation warhead for C-model; 

1,000 lb. class, Advanced Unitary Penetrator (AUP-3M) for 

D-model

Compatibility B-52H 

Acquisition status

Program Status Sustainment (no longer in production)
MISSION

40 UNITED STATES AIR FORCE

AGM-88 High Speed Anti-Radiation Missile (HARM)

mission

Target, suppress and destroy enemy radar and surface-to-air missile 

sites at standoff range utilizing high speed. 

description

The AGM-88 High Speed Anti-Radiation Missile (HARM) supports the Air Force’s and 

Navy’s Suppression of Enemy Air Defenses (SEAD) mission. Currently, HARM is the Air 

Force’s and Navy’s primary reactive anti-radiation weapon capable of destroying or 

suppressing enemy radars. The missile uses anti-radiation homing to attack Surfaceto-Air Missile (SAM) sites. HARM has a radar-sensing seeker, control section, warhead, 

and rocket motor. It is highly accurate and is an all-weather weapon. The Air Force 

platform for the missile is the F-16C/CJ; the Navy platforms are the F/A-18 and EA-6B 

with growth planned for the F-18G (Growler) which will replace the EA-6B. The Block 

IIIA/V missile upgrade adds limited geo-specificity and provides a significant step in 

countering rapidly improving threats and limiting collateral damage. Future development includes the addition of a very accurate INS/GPS to increase accuracy and an 

improved point-to-point capability to allow destruction of non-radiating targets at 

extended ranges with minimized time-to-target. Other upgrades will include seeker 

improvements to expand the target set.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 41

STRATEGIC CAPABILITY

A

GM-88 High Speed Anti-Ra

diation Missile (

H

A

RM)

contractors

Prime: Raytheon (AZ)

specifications

Range <80 nautical miles (NM)

Dimensions Length: 164 in.; Diameter: 10 in.; Wingspan: 36 in.

Warhead

145 lb. fragmentation warhead (New 45.2 lb.); 

Block III/IIIA - 25,000 steel fragments (12.6 grain);

Block IV/V - 14,000 tungsten cubes (30 grain)

Acquisition status

Program Status In sustainment

Unit Assignment

Shaw Air Force Base (AFB), SC; McEntire Air National Guard 

Station (ANGS), SC; Mountain Home AFB, ID; Misawa Air 

Base (AB), Japan; and Spangdahlem AB, Germany

Current Inventory 7,272

Future Upgrades

Under a Cooperative Research and Development (CRAD) 

agreement, Raytheon is upgrading the F-16 Aircraft 

Launcher Interface Computer and developing a HARM 

control section modification to incorporate GPS quality 

accuracy, increasing probability of kill and allowing precise 

geo-specificity. The Air Force is considering modifying some 

AGM-88Cs in the FY08 timeframe.
MISSION

42 UNITED STATES AIR FORCE

AGM-129A Advanced Cruise Missile (ACM)

mission

Provide a subsonic, low-observable, air-to-surface strategic nuclear 

missile that can evade air and ground-based defenses to strike heavily 

defended, hardened targets.

description

The AGM-129A Advanced Cruise Missile (ACM) provides a subsonic, low-observable air-to-surface strategic nuclear missile with significant range, accuracy, and 

survivability improvements over the Air Luanched Cruise Missile (ALCM). The ACM is 

designed to evade air and ground-based defenses in order to strike heavily defended, 

hardened targets at any location within an enemy’s territory. The ACM carries a single 

W80 nuclear warhead. The ACM uses laser sensor updates to give it high navigation 

accuracy and “stealth” technology to give it a low radar cross section and an increased 

chance to penetrate enemy defenses. Up to 12 ACMs can be carried by a B-52 bomber, 

allowing the bomber to attack multiple targets without penetrating enemy airspace.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 43

STRATEGIC CAPABILITY

A

GM-129A Adva

n

ced Cruise Missile (ACM)

contractors

Prime: Raytheon (AZ)

Subcontractor(s): E-Spectrum (TX)

specifications

Weight 3,700 lb.

Range 2,000+ nautical miles (NM)

Armament W80-1 warhead 

Dimensions Length: 20.8 ft.; Diameter: 2.4 ft.; Wingspan: 10 ft.

Coverage Global

Compatability B-52

Acquisition status

Program Status Fielded

Unit Assignment Barksdale AFB, LA, and Minot AFB, ND

Future Upgrades Undergoing life extension programs
MISSION

44 UNITED STATES AIR FORCE

AGM-130 Standoff Attack Weapon

mission

Attack fixed high-value targets, day or night, from outside point 

defenses. 

description

The AGM-130 Standoff Attack Weapon is a solid rocket-powered Guided Bomb Unit 

(GBU)-15. The AGM-130’s Inertial Navigation System/Global Positioning System 

(INS/GPS) Midcourse Guidance (MCG) upgrade provides the operator with the existing basic weapon capabilities along with a significantly reduced aircrew workload, 

an increased capability for target acquisition, and various options for cruise altitudes 

and impact angles. As a backup in the event of data link subsystem non-availability, 

the missile may be released in a direct attack mode (the missile may be released from 

low or high altitudes, but must be locked on to target prior to release).
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 45

STRATEGIC CAPABILITY

A

GM-130 

S

tandoff Attack 

W

eapon

contractors

Prime: Boeing (CA)

specifications

Weight 3,000 lb.

Range >30 nautical miles (NM)

Dimensions Length: 158 in.; Diameter: 18 in.

Warhead

Warhead: Blast/Fragmentation - Mk-84 vertical and 

horizontal targets; Penetrator: BLU-109; Fuze: FMU-124A/B 

(Mk-84), FMU-143 (BLU-109)

Interoperability Platform: F-15E

Guidance

 TV or IR Seeker; INS/GPS navigation/aim point update/terminal automatic tracking or manual steering via data link; 

<3 meter accuracy.

Propulsion Solid Rocket Motor

Acquisition status

Program Status Sustainment

Current Inventory 402

Future Upgrades None 
MISSION

46 UNITED STATES AIR FORCE

AIM-7M Sparrow

mission

Provide all-weather, all-altitude, medium-range capability to attack 

high-performance aircraft and missiles from any direction.

description

The Air Intercept Missile (AIM)-7M Sparrow is a radar-guided, air-to-air missile with a 

high-explosive warhead. The versatile Sparrow provides all-altitude, all-weather, and 

all-aspect capability. The missile can be carried by the F-15, F-16ADF, and F-18, and 

is radar-guided throughout time-of-flight (TOF). The AIM-7M H-build incorporates 

guidance improvements such as Home-On-Jam capability.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 47

STRATEGIC CAPABILITY

AIM-

7M Sparrow

contractors

Prime: Raytheon (AZ)

Subcontractor(s): General 

Dynamics (FL)

specifications

Weight 500 lb.

Range More than 30 nautical miles (NM)

Dimensions Length: 12 ft.; Diameter: 8 in.

Warhead Blast/Fragmentation: WAU-17; Continuous Rod: WAU-10

Interoperability Aircraft dependent

Compatability Aircraft dependent

Service Ceiling Aircraft dependent

Speed More than 2,660 mph

Acquisition status

Program Status Navy program in sustainment

Unit Assignment Numerous (system approved for demilitarization)

Current Inventory 2,500
MISSION

48 UNITED STATES AIR FORCE

AIM-9M Sidewinder

mission

Provide all-weather, all-altitude, short-range, air-to-air capability to 

attack high-performance aircraft and missiles from any direction.

Description

The Air Intercept Missile (AIM)-9M Sidewinder is a supersonic, short-range, passive 

infrared-guided, air-to-air missile with a high explosive warhead. The Sparrow has 

all-altitude, all-weather, and all-aspect capabilities. The missile can be carried by the 

A-10, F-15, F-16, F-16 ADF, and F-18. The missile’s main components are an infrared 

homing guidance section, an active optical target detector, a high-explosive warhead, and a rocket motor. The AIM-9M features improved defense against infrared 

countermeasures, enhanced background discrimination capability, and a reducedsmoke rocket motor. These modifications increase its ability to locate and lock-on a 

target and decrease the missile’s chances for detection.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 49

STRATEGIC CAPABILITY

AIM-

9M Sidewinder

contractors

Prime: Raytheon (AZ)

Subcontractor(s): General 

Dynamics (FL)

specifications

Weight 191 lb.

Range More than 8 nautical miles (NM)

Dimensions Length: 113 in.; Diameter: 5 in.

Warhead Annular Blast/Fragmentation

Interoperability Aircraft dependent

Compatability Aircraft dependent

Service Ceiling Aircraft dependent

Speed Supersonic

Acquisition status

Program Status Navy program in sustainment

Unit Assignment Numerous Active, Reserve, and National Guard squadrons

Current Inventory 2,500
MISSION

50 UNITED STATES AIR FORCE

AIM-9X Sidewinder

mission

Provide a launch-and-leave air combat munition that uses passive 

infrared (IR) energy for acquisition and tracking of enemy aircraft.

description

The Air Intercept Missile (AIM)-9X Sidewinder is the newest variant of the Sidewinder 

missile. It is a supersonic, heat-seeking, short-range, air-to-air missile carried by 

fighter aircraft. It is used in both offensive and defensive counter-air operations. 

Offensively, the weapon ensures that U.S. and combined air forces can project the 

necessary power to ensure dominant maneuver. In the defensive counter-air role, 

the missile system provides force protection. The AIM-9X complements longer-range 

radar-guided missiles such as the Advanced Medium Range Air-to-Air Missile (AMRAAM). The AIM-9X development program provides a number of improved capabilities, including: Improved IR Countermeasure Performance; Improved Probability 

of Kill (Pk); Highly Maneuverable Airframe; High Off-Boresight (HOBS) Acquisition 

and Track; Day/Night Capability. The 9X is also compatible with the Joint HelmetMounted Cueing System (JHMCS), which is designed for ease of target acquisition 

and decreased aircrew workload. Current platforms for the AIM-9X include the F-15C, 

F/A-18C/D, F/A-18E/F, and F-16. Follow-on platforms will include the F-22, F-35, and 

FMS aircraft.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 51

STRATEGIC CAPABILITY

AIM-9X Sidewinder

contractors

Prime: Raytheon (AZ)

specifications

Weight 187 lb.

Dimensions Length: 119 in.; Diameter: 5 in.

Warhead Annular Blast/Fragmentation

Interoperability Aircraft dependent

Compatability Aircraft dependent

Service Ceiling Aircraft dependent

Speed Supersonic

Acquisition status

Program Status Joint Air Force/Navy Program in production; projected 

inventory - 5097

Unit Assignment

Elmendorf AFB (AK), Lakenheath AFB (UK), Mountain Home 

AFB (ID), Kadena AB (Japan), Luke AFB (AZ), Cannon AFB 

(NM), and Missouri Air National Guard (ANG)

Current Inventory 690

Future Upgrades Preplanned Product Improvement (P3I) efforts and processor and fuze obsolescense updates.
MISSION

52 UNITED STATES AIR FORCE

AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM)

mission

Provide all-weather, all-altitude, medium-range, air-to-air capability to 

attack high-performance aircraft and missiles from any direction.

description

The Air Intercept Missile (AIM)-120 Advanced Medium-Range Air-to-Air Missile 

(AMRAAM) is a supersonic, medium-range, active radar guided air-to-air missile 

with a high-explosive warhead. The AIM-120 provides all-altitude, all-weather, 

all-aspect capability. Its platform options include the F-15, F-16, F/A-18, and F-22A. 

The Preplanned Product Improvements (P3I) program will provide the AIM-120 with 

enhanced electronic protection (EP) capabilities; improved warhead, fuzing, and 

guidance; and increased kinematics via a new five-inch stretched rocket motor.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 53

STRATEGIC CAPABILITY

AIM-120 Adva

n

ced Medium Range Air-to-Air Missile (AM

RAAM)

contractors

Prime: Raytheon (AZ)

Subcontractors: Raytheon Andover (MA); ATK Aerospace (UT)

specifications

Weight 356 lb.

Range 20+ nautical miles (NM)

Dimensions Length: 144 in.; Diameter: 7.15 in.

Warhead 45 lb. Blast/Fragmentation

Interoperability Aircraft dependent

Compatability Aircraft dependent

Service Ceiling Aircraft dependent

Speed Supersonic

Acquisition status

Program Status Joint Air Force/Navy Program in development/sustainment

Unit Assignment Numerous Active, Reserve, and Guard units

Current Inventory 4,900 AF and 1,250 Navy

Future Upgrades Preplanned Product Improvement (P3I) efforts
MISSION

54 UNITED STATES AIR FORCE

Air Force Combat Identification (AFCID)

mission

Prevent fratricide and enhance mission effectiveness.

description

Air Force Combat Identification (AFCID) is a family of radar, laser, and beacon systems 

designed to positively identify friend and foe on the battlefield. The goal of the effort 

is to accelerate the transition of advanced Combat Identification (CID) technologies 

into tactical weapons systems (fighter, bomber, Command, Control, Intelligence, 

Surveillance, and Reconnaissance (C2ISR) platforms). Technologies include cooperative systems—where the target voluntarily identifies itself as a friend—and noncooperative systems, where the target has to be identified. A cooperative system under 

development is the Mark XIIA Mode 5 secure Identification Friend or Foe (IFF) interrogator/transponder system. In the non-cooperative area, several efforts are pursuing 

air-to-ground, air-to-air, and ground-to-air identification systems that match radar 

or laser signatures of suspected enemy equipment with a signature database of 

known equipment to positively identify targets as friend or foe.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 55

STRATEGIC CAPABILITY

Air For

ce Combat Identification (AFCID)

contractors

Prime: Raytheon (NY); BAE (CA); 

Northrop Grumman (MD); Boeing 

(WA)

specifications

Range Line-of-sight to horizon

Interoperability Interoperable among Services and with NATO allies

Acquisition status

Program Status Under contract and development on-going
MISSION

56 UNITED STATES AIR FORCE

Air Force Satellite Control Network

mission

Enable deployment, checkout, and flight of operational Air Force, national, allied, and research and development satellites. 

description

The Air Force Satellite Control Network (AFSCN) is the Nation’s only high-power, 

24/7 global network operating Department of Defense (DoD), national, civil, and 

allied satellites in any orbit. Capability is provided through a global system of control 

centers, remote tracking stations, and communications links. The network enables 

satellite telemetry, tracking and commanding, and provides high-power uplink 

capability for anomaly resolution and satellite emergencies. The AFSCN is required for 

all DoD launch and early orbit operations. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 57

STRATEGIC CAPABILITY

Air For

ce Satellite Contro

l

Network

contractors

Prime: Honeywell Technical 

Services, Inc. (CO)

specifications

Size

Eight remote tracking stations, 15 antennas, three data 

link terminals, one checkout facility, and two transportable 

tracking station antennas, as well as two operations control 

centers, and centralized scheduling and control of the 

network assets

Range Global coverage, all orbits

Coverage Continuous global coverage

Capacity/Satellite One satellite per tracking station antenna; more than 150 

satellites supported; more than 160,000 contacts per year

Interoperability

Interoperable with Navy, National Oceanic and Atmospheric 

Administration (NOAA), National Air and Space Administration (NASA), and national users

Acquisition status

Program Status Operational

Future Upgrades

An ongoing program of upgrades is designed to replace 

unsustainable, aging antennas and 1960s-era electronics, as 

well as improve scheduling and orbit analysis systems and 

improve interoperability with civil networks.
MISSION

58 UNITED STATES AIR FORCE

Air Force Weather Weapon System (AFWWS)

mission

Provide our Nation’s forces with essential air and space environmental 

intelligence to ensure battlespace awareness and decision superiority.

description

The Air Force Weather Weapon System (AFWWS) provides capabilities for the five 

core processes of AF weather operations: ground-based terrestrial and ground-based 

space observing capabilities (Collect), analysis and forecasting tools for terrestrial and 

space weather phenomena (Analyze and Predict), the capability to prepare tailored 

weather and weather effects information for the warfighter (Tailor), and the capability to integrate weather into planning and execution decision-making processes to 

enhance all aspects of readiness, deployment, employment, sustainment and redeployment/reconstitution (Integrate). The AFWWS, which consists of both software 

and hardware, is a system-of-systems which principally supports the Joint Functional 

Concepts of Battlespace Awareness and Joint Command and Control.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 59

STRATEGIC CAPABILITY

Air For

ce 

W

e

ather 

W

eapon 

Syste

m (AFWWS)

contractors

Prime: Northrop Grumman (NE)

Subcontractors: Raytheon (NE); 

National Center for Atmospheric 

Research (CO)

specifications

Coverage Worldwide fielding of fixed and tactical meteorological 

equipment supporting Joint, Air Force, and Army operations.

Interoperability

Machine-to-human (M2H) interoperability via Uniform 

Resource Locator-based web services at various classification 

levels, and limited machine-to-machine (M2M) interoperability with warfighter systems via legacy interfaces and 

through use of new Joint Meteorological and Oceanographic 

Broker Language (JMBL) standards. 

Acquisition status

Program Status Various

Future Upgrades

Use of the Joint Environmental Toolkit (JET) and standard 

Joint METOC Broker Language (JMBL) will enable common 

network-centric interfaces to C4I systems for direct M2M, 

M2H and human-to-human integration and exploitation of 

weather information by warfighters and decision makers at 

all levels of operations.
MISSION

60 UNITED STATES AIR FORCE

Airborne Laser (ABL)

mission

Provide the capability to acquire, track, and kill ballistic missiles in their 

boost phase, thus protecting U.S. deployed forces, U.S. allies, and areas 

of vital interest from ballistic missile attack. 

description

The Airborne Laser (ABL) is a modified Boeing 747-400. It kills ballistic missiles in 

boost phase; autonomously detects, tracks, and engages ballistic missiles; and provides accurate missile launch location and impact points. The ABL is rapidly deployable; it will function as the pathfinder for future Directed Energy (DE) weapons and 

has the potential for other adjunct missions.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 61

STRATEGIC CAPABILITY

Air

borne L

aser (ABL)

contractors

Prime: Battle Management and 

Air Vehicle Integration & Test, 

Aircraft - Boeing Company (KS, CA); 

Beam Control/Fire Control System

- Lockheed Martin (CA); Laser

- Northrop Grumman (CA)

specifications

Weight Takeoff weight - 803,000 lb.

Range 24 hours of flight with refueling, but needs to periodically 

return to check oil consumption

Armament No armaments, but the loading and unloading of chemicals 

at the fuel farm is treated like a weapon storage area

Dimensions Length: ~ 245 ft.; Width: 231 ft.

Warhead High Energy Laser

Coverage Refuelable

Interoperability Functions as an element of the Ballistic Missile Defense 

System (BMDS); Link 16

Acquisition status

Program Status

Completed eight months of flight testing at Edwards AFB 

in July 2005 – very successful tests of the integrated Beam 

Control/Fire Control (optics) and Battle Management systems. Laser System Integration Lab (SIL) testing at Edwards 

AFB is complete. Multiple full-duration lasings at lethal 

power and duration were completed in December 2005. 

Over 70 lasing events since November 2004 have demonstrated reliable operation of the high-energy laser segment. The aircraft has completed modifications at Wichita, 

KS, to augment its floor to accommodate laser installation 

and to install solid-state lasers for missile tracking and 

atmospheric compensation. System is in the process of 

ground and flight testing of the solid state lasers, leading 

to a lethal demonstration in FY09.
MISSION

62 UNITED STATES AIR FORCE

AN/GSQ-272 AIR FORCEDISTRIBUTED COMMONGROUNDSYSTEM (AF DCGS)

mission

Collect, process, exploit, and disseminate data, information, and intelligence from Intelligence, Surveillance and Reconnaissance (ISR) sensors such as the U-2, Global Hawk, Predator, and others.

description

The AN/GSQ-272 Air Force Distributed Common Ground System (AF DCGS) is a network-centric weapon system capable of tasking ISR sensors and receiving, processing, 

exploiting, and disseminating data and information from airborne, national, and 

commercial platforms and sensors. This weapon system consists of numerous Active Duty, Air National Guard, and mission-partner sites, interconnected by a robust 

communications structure that enables collaborative reachback ISR operations. AF 

DCGS operators correlate collected imagery intelligence, signals intelligence, and 

measurement and signatures intelligence data to provide decision-quality information directly to the Joint Task Force and below, including significant support to timecritical targeting operations.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 63

STRATEGIC CAPABILITY

A

N

/GSQ-272 AIR FOR

C

E DISTRIBUTED C

OMMON GRO

UND SYSTEM (AF 

D

CGS)

contractors

Prime: Raytheon (TX, CA, VA); 

Lockheed Martin (AZ, CO); L-3 Communications (UT); Goodrich (MA); 

Northrop Grumman (MD); General 

Dynamics (VA); BEA (NY); BAE (CA); 

Kodak (NY)

specifications

Range Worldwide via datalink relay and satellite

Coverage Worldwide via reachback operations

Size

Active Duty core locations: Langley AFB, VA; Beale AFB, 

CA; Hickam AFB, HI; Ramstein AB, Germany; Pacific Air 

Forces. Air National Guard (ANG) locations: Wichita, KS; 

Birmingham, AL; Little Rock, AR; Reno, NV. Other worldwide 

locations.

Interoperability

U-2, Global Hawk, Predator, and other ISR platforms/sensors; DoD DCGS architecture; intelligence community 

systems; national intelligence databases; theater communications systems and datalinks; DCGS Integration Backbone; 

Common Imagery Processor

Acquisition status

Program Status Sustainment

Future Upgrades Upgrading to 10.2 configuration

Current Inventory One
MISSION

64 UNITED STATES AIR FORCE

AN/USQ-163 Falconer Air and Space Operations Center

Weapon System (AOC-WS) 

mission

Provide Joint/Combined Force Air Component Commander’s 

(JFACC/CFACC’s) primary tool for commanding air and space power.

description

The AN/USQ-163 Falconer Air and Space Operations Center Weapon System (AOC-WS) 

is the senior element of the Theater Air Control System. The JFACC/CFACC uses the 

system for planning, executing and assessing theater-wide air and space operations. 

The AOC-WS develops operational strategy and planning documents. It also disseminates tasking orders, executes day-to-day peacetime and combat air and space 

operations, and provides rapid reaction to immediate situations by exercising positive 

control of friendly forces.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 65

STRATEGIC CAPABILITY

A

N/USQ-1

6

3 Falconer Air 

and Space Oper

ations Center 

W

eapon 

Syste

m (A

OC-WS)

Contractors

Prime: Lockheed Martin Integrated 

Systems & Solutions (VA, MA)

Subcontractors: IBM (VA, MA);

L3 (VA, MA); SAIC (VA); DRC 

(VA, MA); ISS (VA, MA)

specifications

Size Each AOC-WS is sized to support its mission; Averages: 

1,000–2,000 people; 70,000 square ft. of space.

Interoperability

Interoperates using Internet Protocol (IP) and tactical data 

networks with Joint and Coalition Command and Control 

(C2) units at various command levels. Receives ISR data from 

various sources at various classification levels. Air Tasking 

Orders and Airspace Control Orders are disseminated to air 

bases throughout the theater. AOC receives and processes 

situation awareness data from tactical units to enable the 

prosecution of time-sensitive targets.

Acquisition status

Program Status Fielding Increment 10.1; Pre-Milestone B for Increment 10.2

Future Upgrades

Increment 10.2: Net Ready Compliance, Improved Collaboration, Joint Air Operations Plan and Joint Air Execution 

Plan linked to assessment; Reduction of decision support 

process cycle times; Decision quality information; Automate 

capability to support integrated air and space effects-based 

dynamic strategy development and assessment ; Effectively 

deconflict airspace in Air Tasking Order planning and execution ; C2 Constellation Net capabilities to manage, protect, 

and exchange information with joint, allied, and coalition 

military and civil nodes; Standard common data model 

and IM strategy to enable data association and information 

persistence and sharing within and beyond the AOC WS; 

Integrated system and management of network resources; 

Integrated automated support for IPB for air and space 

operations planning; Improved coalition interoperability; 

Information and functionality sharing 
MISSION

66 UNITED STATES AIR FORCE

B-1B Lancer

mission

Rapidly deliver massive quantities of precision and non-precision 

weapons, anywhere in the world, at any time.

description

The multi-mission B-1B Lancer is a highly versatile, supersonic aircraft that carries 

the largest payload of both guided and unguided weapons in the Air Force inventory. 

It has three internal weapons bays and the ability to mix weapons loads between 

bays and within a bay for J-Series weapons. The B-1B’s offensive avionics system 

includes high-resolution synthetic aperture radar, capable of tracking, targeting, and 

engaging moving vehicles as well as self-targeting and terrain-following modes. In 

addition, the B-1B’s equipment enables aircrews to navigate globally without the aid 

of ground-based navigation aids, as well as engage targets with a high level of precision. The B-1B features an integrated, robust onboard defense and countermeasures 

system. The aircraft can carry up to 30 cluster munitions (CBU-87, -89, -97, -103, 

-104, -105) or up to 24 Joint Direct Attack Munitions (JDAM) guided weapons. The 

B-1B is flexible enough to be employed from inside or outside the theater of operations and is capable of conducting all-weather, deep strike, and night air-to-surface 

attacks. The B-1B’s speed, superior handling characteristics, substantial payload, 

excellent radar targeting system, long loiter time and survivability enable the B-1B 

to create a multitude of far-reaching effects across the battlefield as a key element of 

any joint/composite strike force.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 67

STRATEGIC CAPABILITY

B-

1B L

a

n

cer

contractors

Prime: Airframe - Boeing (CA); 

Propulsion - General Electric (OH); 

Radar - Northrop Grumman (MD)

specifications

Weight 477,000 lb. (max weight)

Range Intercontinental (unrefueled)

Armament 

Three weapons bays, capable of mixing weapons loads 

between bays and within a bay; 84 Mk-82 (500-lb.) or 24 

Mk84 (2,000-lb.) general- purpose bombs; Mk-62 and 

Mk 65 mines; 30 CBU-87/89/97 cluster munitions and 

CBU-103/104/105 wind corrected equivalents; 24 GBU31 (2,000-lb.) JDAMs. Initial capability for 12 AGM-154 

Joint Standoff Weapons (JSOW) and/or 24 AGM-158 Joint 

Air-to-Surface Standoff Missiles (JASSM) in October 2004. 

Initial capability for 15 GBU-38 (500-lb.) JDAM in March 

2005. Largest ordnance load-out of any U.S. aircraft.

Dimensions Wingspan, wings forward: 137 ft.; Wingspan, wings aft: 79 

ft.; Length: 146 ft.; Height: 34 ft.

Service Ceiling Over 30,000 ft.

Speed 900-plus mph (Mach 1.2 at sea level)

Crew Four (two pilots, two weapon systems officers)

Acquisition status

Program Status Modernization, Modification and Sustainment

Unit Assignment Dyess AFB, TX; Ellsworth AFB, SD

Current Inventory 67

Future Upgrades

JASSM-Extended Range (ER), Defensive Upgrade, Radar, 

Situational Awareness, Datalink, on-board diagnostics, 

inertial navigation upgrade, Target Pod
MISSION

68 UNITED STATES AIR FORCE

B-2 Spirit

mission

Deliver massive firepower in a short time, anywhere in the world, 

through high-threat defenses using both conventional and nuclear 

munitions. 

description

Along with the B-52 and B-1B, the B-2 provides the strategic effectiveness inherent 

in manned multi-role bombers. With its low-observable, or ”stealth,” characteristics, 

it can penetrate an enemy’s most sophisticated defenses and threaten its most valued 

and heavily defended targets. Its capability to penetrate air defenses and threaten 

effective retaliation with relative impunity provides a strong, effective deterrent and 

combat force well into the 21st century. The revolutionary blending of low-observable technologies with high aerodynamic efficiency and large payload gives the B-2 

important advantages over other platforms. Its low-observability provides greater 

freedom of maneuver while high altitude flight increases its range and provides a 

better field of view for the aircraft’s sensors. The B-2’s low observability is derived 

from a combination of reduced infrared, acoustic, electromagnetic, visual, and radar 

signatures. The dramatically reduced sum of these signatures makes it difficult for 

today’s sophisticated defensive systems to detect, track, and engage the B-2. The B-2 

has a crew of two: a pilot in the left seat and mission commander in the right, compared to the B-1B’s crew of four and the B-52’s crew of five.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 69

STRATEGIC CAPABILITY

B-

2 Spi

rit

contractors

Prime: Northrop Grumman (CA)

specifications

Size Length: 69 ft. (20.9 m); Height: 17 ft. (5.1 m); 

Wingspan: 172 ft. (52.12 m)

Weight (Typical): 336,500 lb. (152,634 kg)

Range Intercontinental (unrefueled)

Armament 

Two weapons bays, capable of employing conventional and 

nuclear weapons. Unguided weapons include 80 Mk-82 

(500-lb.), 36 M117 (750-lb.), or 16 Mk-84 (2,000-lb.) 

general-purpose bombs; 80 Mk-62 series sea mines or 34 

CBU-87/89/97 cluster munitions. Precision weapons include 

16 GBU-31 (2,000-lb.) JDAMs or 80 GBU-38 (500-lb.) JDAMs 

or 8 GBU-28 (5,000-lb) or 8 GBU-37/B (5,000-lb) or 16 AGM154 Joint Standoff Weapons (JSOW) or 16 AGM-158 Joint 

Air-to-Surface Standoff Missiles (JASSM). Nuclear weapons 

include 16 B-61 or 16 B-83 nuclear gravity bombs.

Speed High subsonic 

Payload More than 40,000 lb. (18,144 kg) 

Ceiling 50,000 ft. (15,240 m)

Acquisition status

Program Status Modernization, Modification and Sustainment

Unit Assignment Whiteman AFB, MO

Current Inventory 21

Future Upgrades

Link-16, Alternate High Frequency Material, 

Radar Modernization Program; Extremely High Frequency 

(EHF) Satellite Communications (SATCOM); and Computers
MISSION

70 UNITED STATES AIR FORCE

B-52H Stratofortress

mission

Deliver massive quantities of precision and non-precision conventional 

and nuclear weapons anywhere in the world at any time.

description

The B-52H Stratofortress is a long-range, heavy bomber that can perform a variety 

of missions. For more than 40 years, B-52 Stratofortresses have been the workhorse 

of the manned strategic bomber force for the United States. The B-52 is capable 

of dropping or launching the widest array of weapons in the U.S. inventory. This 

includes gravity bombs, cluster bombs, precision guided missiles, and Joint Direct 

Attack Munition (JDAM). Updated with modern technology, the B-52 will be capable 

of delivering the full complement of joint developed weapons and continues into the 

21st century as an important element of our nation’s defenses. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 71

STRATEGIC CAPABILITY

B-52H

Str

ato

fortress

contractors

Prime: Airframe - Boeing Aircraft 

(KS); Engines - Pratt & Whitney (KS)

Subcontractor(s):Electronic 

Counter Measures Improvement 

(ECMI) - ITT Industries (NJ); Avionics Midlife Improvement (AMI) - 

Honeywell (FL)

specifications

Weight Approximately 185,000 lb. empty

Range Intercontintental (unrefueled)

Armament 

One weapons bay and two external pylons, capable of 

employing conventional and nuclear weapons from the bay 

and pylons (J-series from pylons only). Unguided weapons 

include 45 Mk-82 (500-lb.) or 12 Mk-84 (2,000-lb.) general-purpose bombs; Mk-62, Mk-63, and Mk 65 mines; 24 

CBU-87/89 cluster munitions or 16 CBU-103/104/105 wind 

corrected equivalents. Precision weapons include 12 GBU-31 

(2,000-lb.) JDAMs or 12 AGM-154 Joint Standoff Weapons 

(JSOW) or 20 AGM-86 C/D Conventional Air Launched Cruise 

Missiles (ALCM) or 12 AGM-158 Joint Air-to-Surface Standoff 

Missiles (JASSM) or 10 GBU-10 (2000-lb.) laser guided 

bombs (LGB) or 13 GBU-12 (500-lb.) LGBs. Initial capability 

for 12 GBU-38 (500-lb) JDAM in March 2005. Nuclear weapons include 20 AGM-86B ALCM or 12 AGM-129 Advanced 

Cruise Missiles or 8 B-61/B-83 nuclear gravity bombs.

Dimensions Length: 159 ft., 4 in.; Height: 40 ft., 8 in.; Wingspan: 185 ft.

Service Ceiling 50,000 ft.

Speed 650 mph (Mach 0.86)

Crew Capacity Five (aircraft commander, pilot, radar navigator, navigator, 

and electronic warfare officer)

Acquisition status

Program Status Modernization, Modification and Sustainment

Unit Assignment Minot AFB, ND; Barksdale AFB, LA

Current Inventory 76

Future Upgrades

Conventional Modifications; Combat Network Communications Technology (CoNECT)—Satellite and secure wideband 

high data rate communication datalink; Advanced Targeting 

Pods—Litening AT pod capability; Avionics Midlife Improvement—inertial navigation, aircraft computer and data transfer unit upgrades; Miniature Air Launched Decoy (MALD)
MISSION

72 UNITED STATES AIR FORCE

C-5 Galaxy

mission

Provide strategic inter-theater airlift in support of U.S. national defense.

description

The C-5 Galaxy provides the Air Mobility Command (AMC) with inter-theater airlift 

in support of U.S. national defense. The C-5 Galaxy and the C-17 Globemaster are 

partners in AMC’s strategic airlift concept. The C-5 Galaxy is one of the largest aircraft 

in the world. It can carry outsize and oversize cargo over intercontinental ranges and 

can take off or land within relatively short distances.
GLOBAL REACH

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STRATEGIC CAPABILITY

C-

5 Galaxy

contractors

Prime: Lockheed Martin (GA)

Subcontractor(s): Avionics 

Modernization Program (AMP)

- Honeywell (NM); ARINC (MD); 

Reliability Enhancement and 

Re-Engining Program (RERP)

- General Electric (NC); Goodrich (AL)

specifications

Weight 769,000 lb. peacetime; 840,000 lb. wartime 

Range Unlimited with in-flight refueling

Dimensions Wingspan: 222.9 ft.; Height: 65.1 ft.; Length: 247.1 ft.

Service Ceiling 45,000 ft.

Payload Up to 36 pallets (270,000 lb.)

Speed 518 mph (450 knots)

Passenger Capacity 73

Acquisition status

Program Status Sustainment/upgrade

Unit Assignment

Active: 8 C-5A, 36 C-5B, 2 C-5C and 3 C-5M; Travis AFB CA; 

Altus AFB, OK; Dover AFB, DE;

Air Force Reserve (AFRES): 32 C-5A, 11 C-5B; Lackland AFB, 

TX; Westover ARB, MA; Wright-Patterson AFB, OH

Air National Guard (ANG): 19 C-5A; Memphis, TN; Stewart 

ANG Base, NY; Martinsburg, WV scheduled for C-5 activation 

in FY08

Current Inventory 111

Future Upgrades Large Aircraft Infrared Countermeasures (LAIRCM)
MISSION

74 UNITED STATES AIR FORCE

C-9C

mission

Provide operational support airlift for high priority passengers 

and cargo.

description

The C-9C is the military variant of the DC-9-32, equipped with robust passenger 

communications and data transfer capabilities. The plane features an executive suite 

and first-class style seating for up to 42 passengers.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 75

STRATEGIC CAPABILITY

C-

9

contractors

C

Prime: Airframe Depot - Lockheed 

Martin (SC); Engine Depot - AeroThrust (FL)

specifications

Weight 110,000 lb.

Range 2,100 nautical miles (NM)

Dimensions Wingspan: 93 ft.; Length: 119 ft.; Height: 27 ft.

Service Ceiling 37,000 ft.

Speed 520 mph (Mach 0.80)

Passenger Capacity 42 passengers

Acquisition status

Program Status Sustainment

Unit Assignment Scott AFB, IL

Current Inventory 3
MISSION

76 UNITED STATES AIR FORCE

C-12C/D/F/J

mission

Provide cargo and passenger airlift for operational support airlift and 

embassy support missions; support test operations at Edwards and 

Holloman Air Force Bases.

description

The C-12C/D/F/J is a military variant of the Beech Super King Air 200 (C/D/F) and 

1900 (J) with specialized mission equipment. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 77

STRATEGIC CAPABILITY

C-12C/

D/F/J

contractors

Prime: Airframe - L-3 Communications/Vertex Aerospace (MS)

Subcontractor(s):Engines 

Propulsion - Pratt & Whitney (WV)

specifications

Weight 12,500 lb. (J-model = 16,600 lb.)

Range 1,700 nautical miles (NM) (J-model = 1,500 NM)

Dimensions Wingspan: 55 ft.; Length: 44 ft. (J-model = 58 ft.); 

Height: 15 ft.

Service Ceiling 31,000 ft. (J-model = 25,000 ft.)

Speed 300 to 340 mph depending on model

Passenger Capacity Eight passengers (J-model = 19 passengers)

Acquisition status

Program Status Sustainment; delivery completed in December 1987

Unit Assignment

Osan AB, Korea; Elmendorf AFB, AK; Edwards AFB, CA; 

Holloman AFB, NM; Andrews AFB, MD; Embassy sites 

worldwide

Current Inventory 28

Future Upgrades

Electronic Flight Information System (Communications, 

Navigation, Surveillance/Air Traffic Management (CNS/ATM) 

and Navigation Safety)
MISSION

78 UNITED STATES AIR FORCE

C-17 Globemaster III

mission

Provide rapid strategic delivery of troops and all types of cargo to main 

operating bases or directly to forward bases in the deployment area.

description

The C-17 Globemaster III is the newest, most flexible cargo aircraft to enter the airlift 

force. It is capable of performing tactical airlift and airdrop missions when required. 

The inherent flexibility and performance of the C-17 force improve the ability of the 

total airlift system to fulfill the worldwide air mobility requirements of the United 

States. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 79

STRATEGIC CAPABILITY

C-17 Gl

o

b

emaster III

contractors

Prime: Airframe - Boeing (CA, MO); 

Engines - Pratt & Whitney (CT)

Subcontractor(s): Major Airframe 

Components - Vought Aircraft 

Industries (TX) 

specifications

Weight 585,000 lb. 

Range Unlimited with in-flight refueling

Dimensions Wingspan: 169 ft. 10 in.; Height: 55 ft. 1 in.; Length: 174 ft.

Service Ceiling 45,000 ft.; 450 knots at 28,000 ft. (Mach .74)

Speed Mach 0.74

Payload 164,900 lb. (18 pallets)

Passenger Capacity 102 troops/paratroops or 48 litters and 54 ambulatory 

attendants

Acquisition status

Program Status Production; 15 per year; projected inventory - 190

Unit Assignment

Air Force Reserve (AFRES): March AFB , CA; 

Air National Guard (ANG): Jackson, MS; 

Active: McChord AFB,WA; Travis AFB, CA; Edwards AFB, CA; 

Elmendorf AFB,AK; Hickam AFB, HI; Altus AFB, OK; Charleston AFB, SC; Dover AFB, DE; McGuire AFB, NJ

Current Inventory 159

Future Upgrades Modifications
MISSION

80 UNITED STATES AIR FORCE

C-20B/H

mission

Provide worldwide air transportation for the vice president, cabinet, 

and congressional members, and other high-ranking U.S. and foreign 

officials; provide air transportation supporting U.S. European Command 

(USEUCOM) operational requirements. 

description

The C-20B/H is the military variant of the Gulfstream III (C-20B) and Gulfstream IV 

(C-20H) equipped with passenger communications and data transfer systems. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 81

STRATEGIC CAPABILITY

C-

20B/

H

contractors

Prime: Airframe - M7 Aerospace (TX)

Subcontractor(s):Engines - Rolls 

Royce (TX); Dallas Airmotive (TX)

specifications

Weight C-20B: 69,700 lb.; C-20H: 74,600 lb.

Range C-20B: 2,700 nautical miles (NM); C-20H: 3,375 NM

Dimensions Wingspan (B,H): 78 ft./78 ft.; Length (B,H): 83 ft./88 ft.; 

Height (B,H): 25 ft./25 ft.

Service Ceiling 45,000 ft.

Speed 530 mph (Mach 0.80)

Passenger Capacity 12 passengers

Acquisition status

Program Status Sustainment; delivery completed in 1987 (C-20B) and 1996 

(C-20H)

Unit Assignment Andrews AFB, MD; Ramstein AB, Germany

Current Inventory Five (5) C-20B; two (2) C-20H

Future Upgrades Mission Communication/Data Systems
MISSION

82 UNITED STATES AIR FORCE

C-21A

mission

Provide high-priority cargo and passenger airlift in support of 

Combatant Commander operational requirements; enable medical 

evacuations. 

description

The C-21 is the military version of the Lear Jet 35A business jet. It provides cargo and 

passenger airlift and can be configured to transport litters for medical evacuations.
GLOBAL REACH

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STRATEGIC CAPABILITY

C-21

A

contractors

Prime: Airframe - Computer 

Sciences Corp./APD (TX); 

Engines - Dallas Airmotive (TX)

specifications

Weight 18,300 lb.

Range 2,300 nautical miles (NM)

Dimensions Wingspan: 39 ft.; Length: 48 ft.; Height: 12 ft.

Service Ceiling 45,000 ft.

Speed 530 mph (Mach 0.81)

Passenger Capacity 8 passengers and 42 cubic feet of cargo

Acquisition status

Program Status Sustainment

Unit Assignment

Andrews AFB, MD; Wright-Patterson AFB, OH; Scott AFB, IL; 

Peterson AFB, CO; Keesler AFB, MS; Ramstein AB, Germany; 

Yokota AB, Japan

Current Inventory 76

Future Upgrades None
MISSION

84 UNITED STATES AIR FORCE

C-32A

mission

Provides worldwide air transportation for the president, vice president, 

cabinet members, congressional delegations, and other senior U.S. and 

foreign officials. 

description 

C-32A is the military variant of the commercial Boeing 757-200 with interior 

furnishings and electronic equipment to accommodate senior government officials. 

The cabin is equipped with robust passenger communications and data transfer 

systems and an executive suite.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 85

STRATEGIC CAPABILITY

C-32

A

contractors

Prime: Airframe - Boeing (WA)

Subcontractor(s):Engines - Pratt 

& Whitney (CT)

specifications

Weight 255,000 lb.

Range 3,800 nautical miles (NM)

Dimensions Wingspan: 125 ft.; Length: 155 ft.; Height: 44.5 ft.

Service Ceiling 41,000 ft.

Speed 530 mph (Mach 0.8)

Passenger Capacity 46 passengers

Acquisition status

Program Status Sustainment

Unit Assignment 89th Air Wing, Andrews AFB (MD)

Current Inventory 4

Future Upgrades Mission Communication/Data System; Communications, 

Navigation, Surveillance/Air Traffic Management (CNS/ATM)
MISSION

86 UNITED STATES AIR FORCE

C-37A

mission

Provide worldwide air transportation for the vice president, White 

House staff, cabinet members, members of Congress, Combatant

Commanders (COCOM) and other senior U.S. and foreign officials. 

description

The C-37A is a military variant of the commercial Gulfstream V jet, equipped with 

robust passenger communications and data systems. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 87

STRATEGIC CAPABILITY

C-37

A

contractors

Prime: Airframe - Gulfstream (GA)

Subcontractor(s): Engines - 

Rolls Royce (GA) 

specifications

Weight 90,500 lb.

Range 5,300 nautical miles (NM)

Dimensions Wingspan: 93.5 ft.; Length: 96.5 ft.; Height: 26 ft.

Service Ceiling 51,000 ft.

Speed 530 mph (Mach 0.8)

Passenger Capacity 14

Acquisition status

Program Status Sustainment; delivery completed 1QFY03

Unit Assignment

Andrews AFB, MD (VIP Special Airlift Mission); MacDill AFB, 

FL (COCOM); Hickam AFB, HI (COCOM); Chievres Air Base, 

Belgium (COCOM)

Current Inventory Nine

Future Upgrades Communication Systems
MISSION

88 UNITED STATES AIR FORCE

C-40B/C

mission

Provide worldwide air transportation for U.S. leaders and Combatant 

Commanders (COCOM). 

Description

The C-40B/C is a military variant of the commercial Boeing 737 business jet, equipped 

with robust communications and data transfer systems (C-40B only). It provides 

air transportation for U.S. leaders, including COCOMs. Customers include the vice 

president, the first lady, cabinet members, and members of Congress. The C-40C is 

also capable of variable configurations for accommodating from 34 to 68 passengers, 

depending on mission requirements.
GLOBAL REACH

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STRATEGIC CAPABILITY

C-

4

contractors

0B/C

Prime: Airframe - Boeing (WA)

Subcontractor(s) - Engines - CFM 

International (WA)

specifications

Weight 171,000 lb.

Range C-40B: 4750 nautical miles (NM); C-40C: 4,628 NM

Dimensions Wingspan: 112 ft.; Length: 117 ft.; Height: 41 ft.

Service Ceiling 41,000 ft.

Speed 530 mph (Mach 0.8)

Passenger Capacity C-40B: 26 passengers and 11 crew; C-40C: up to 68 

passengers and 11 crew

Acquisition status

Program Status

Procurement; three additional C-40Cs have been purchased 

for delivery to Scott AFB, IL during FY07/08; AF expects to 

complete delivery in FY08

Unit Assignment

89th Air Wing, Andrews AFB, MD; 15th Air Base Wing, 

Hickam AFB, HI; 86th Air Wing, Ramstein AB, Germany; 

201st Airlift Squadron, DC Air National Guard, Andrews AFB, 

MD; 932nd Air Wing, Scott AFB, IL

Current Inventory 7 (10 projected)

Future Upgrades Self Defense Systems for COCOM aircraft
MISSION

90 UNITED STATES AIR FORCE

C-130 Hercules

mission

Provide airlift and transport for air-dropping troops and equipment into 

hostile areas. 

description

The C-130 Hercules operates throughout the U.S. Air Force, serving with Air Mobility Command (stateside based), Air Force Special Operations Command, theater 

commands, the Air National Guard, and the Air Force Reserve Command, fulfilling a 

wide range of operational missions in both peace and wartime situations. Basic and 

specialized versions of the aircraft perform a diverse number of roles, including airlift 

support, Antarctic resupply, aeromedical missions, weather reconnaissance, aerial 

spray missions, fire-fighting duties for the U.S. Forest Service, and natural disaster 

relief missions.
GLOBAL REACH

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STRATEGIC CAPABILITY

C-130 

Hercules

contractors

Prime: Lockheed Martin 

Aeronautics Company (MD)

specifications

Weight C-130E/H: 155,000 lb. (69,750 kg) 

Range 

Range at Maximum Normal Payload - C-130H: 1,208 mi. 

(1,050 nautical miles (NM)); C-130E: 1,150 mi. (1,000 NM)

Range with 35,000 lb. of payload - C-130H: 1,496 mi. 

(1,300 NM); C-130E: 1,438 mi. (1,250 NM)

Dimensions Length: 97 ft., 9 in. (29.3 m); Height: 38 ft., 10 in. 

(11.9 m); Wingspan: 132 ft., 7 in. (39.7 m)

Service Ceiling

C-130H: 23,000 ft. (7,077 m) with 42,000 lb. (19,090 kg) 

payload; C-130E: 19,000 ft. (5,846 m) with 42,000 lb. 

(19,090 kg) payload

Payload C-130E, 42,000 lb. (19,090 kg); C-130H, 42,000 lb. (19,090 kg)

Speed

C-130E: 345 mph/300 ktas (Mach 0.49) at 20,000 ft. (6,060 

m); C-130H: 366 mph/318 ktas (Mach 0.52) at 20,000 ft. 

(6,060 m)

Passenger Capacity 92 combat troops or 64 paratroopers

Acquisition status

Program Status Sustainment

Unit Assignment

Air Force Reserve (AFRES): Peterson AFB, CO; Minn-St Paul, 

MN; Youngstown, OH; Niagara, NY; Pope AFB, NC; Dobbins 

AFB, GA; Maxwell AFB, AL

Air National Guard (ANG): Cheyenne, WY; Rosencrans, MO; 

Peoria, IL; Minn-St Paul, MN; Selfridge, MI; Schenectady, NY; 

New Castle, DE; Yaeger, WV; Charlotte, NC; Luis Munoz Marin 

IAP, PR; Savannah, GA; Louisville, KY; Nashville, TN; Little 

Rock AFB, AR; Carswell, TX; Will Rogers, OK; Elmendorf AFB, 

AK; Reno, NV; Boise, ID

Active: Pope AFB, NC; Little Rock AFB, AR; Dyess AFB, TX; 

Elmendorf AFB, AK

Current Inventory Active force, 186; Air National Guard, 222; Air Force 

Reserve, 106

Future Upgrades

Avionics Modernization Program (AMP), Large Aircraft 

Infrared Countermeasures (LAIRCM), Center Wing Box (CWB) 

Replacement, Enhanced Terrain Collision Avoidance System 

(ETCAS), APN-241 Weather Radar
MISSION

92 UNITED STATES AIR FORCE

C-130 Senior Scout

mission

Deliver near-real-time Intelligence, Surveillance, and Reconnaissance 

(ISR) information to locate and track enemy forces. 

description

The SENIOR SCOUT is a radio signal monitoring sensor package carried by a C-130H. 

The SENIOR SCOUT offers a low-cost, small-footprint, quick-reaction collection capability to theater commanders and can also satisfy national-level information requirements. It is contained in a shelter mounted on pallets and configured for installation 

on any C-130H/H1/H2 aircraft. The crew complement includes several Signals Intelligence (SIGINT) operators to locate and track targets. The SENIOR SCOUT was recently 

cited for ISR excellence for operations in direct support of the 22nd Marine Expeditionary Unit (USMC) in Operation Enduring Freedom in June 2004. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 93

STRATEGIC CAPABILITY

C-130 SENIOR

S

C

O

U

T

contractors

Prime: Lockheed Martin Integrated 

Systems and Solutions (CO)

Subcontractor(s): Sierra Nevada 

Corporation (Plano Microwave, Inc.) 

(NV, TX, UT); L-3 Communications 

(TX)

specifications

Size Pallet Size: Three pallet sizes or approximately equal to an 

18-ft. semi bed

Weight Gross max takeoff weight 155,000 lb. Each SENIOR SCOUT 

shelter weighs approximately 24,500 lb.

Range 

Collection range between 250–400 miles, dependent upon 

target, terrain, and altitude. 

Mission length: 7 (un-refueled)–13 (refueled) hours

Dimensions Wingspan: 132 ft.; Length: 100 ft.; Height: 38 ft.

Interoperability NABRE, LINK 16, JTIDS, TADIL-A, TIBS, SENSOR PACER

Compatibility Any C-130 H/H1/H2 (all services) 

Acquisition status

Program Status Modification and sustainment

Unit Assignment 169th Intelligence Squadron (ACC); Utah Air National Guard, 

Salt Lake City

Current Inventory Three systems (capsules)
MISSION

94 UNITED STATES AIR FORCE

Mission

Provide unobtrusive, long-range, long-loiter collection capability in a 

permissive environment. 

Description

Scathe View is composed of a high-endurance, adverse weather-operable, specially 

modified C-130H aircraft; a roll-on/roll-off sensor control and communications pallet 

operated by two on-board airborne imagery analysts; and the Wescam MX-15 “pentasensor,” a day or night capable imagery sensor with a laser range finder and a laser 

illuminator. The Scathe View disseminates intelligence data and information directly 

to ground forces in real time via on-board voice and data communications suites. 

Employed with the Remote Operations Video Enhanced Receiver (ROVER) system, it 

can provide still-frame and full-motion video imagery downlink to receiver equipped 

ground units, complemented by real-time voice communications to the ground. 

Programmed Tactical Common Data Link and beyond line of sight data communication upgrades will allow for high-quality imagery transmission to ground exploitation units in theater and for worldwide dissemination, respectively. Scathe View and 

its National Guard crews have been an essential component of search and rescue, 

aerial mapping and Humanitarian Relief Operations (HUMRO) during post-Hurricane 

Katrina operations.

C-130H Scathe View
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 95

STRATEGIC CAPABILITY

C-13

0

H Scathe View

Contractors

Prime: ATK Mission Research 

Integrated Systems (TX)

specifications

Weight 920 lb. 

Range

Range is same as C-130H: Maximum Normal Payload - 1,208 

mi. (1,050 nautical miles (NM)) With 35,000 lb. of payload 

- C-130H: 1,496 mi. (1,300 NM)

Coverage Full Motion Video

Acquisition status

Program Status Modification and sustainment

Current Inventory

8 modified ANG C-130H aircraft, 152nd Airlift Wing (AMC); 

Scathe View system, 152nd intelligence Squadron (ACC), 

Reno ANG Base (NV)

Unit Assignment

C-130H aircraft, 152nd Airlift Wing (AMC); Scathe View 

system, 152nd intelligence Squadron (ACC),

Reno ANG Base (NV)

Future Upgrades

Upgrading sensors to latest generation full motion video 

sensor (MX-15); Beyond Line of Sight Capability, allowing 

passing of data to intermediate higher headquarters and 

world-wide users.
MISSION

96 UNITED STATES AIR FORCE

C-130J

mission

Provide immediate movement of combat troops and supplies within 

theaters of operation, as well as weather reconnaissance and psychological operations capabilities.

description

The C-130 operates throughout the U.S. Air Force, serving with Air Education and 

Training Command, Air Force Special Operations Command, Air National Guard, and 

the Air Force Reserve Command, fulfilling a wide range of operational missions in 

both peace and war situations. Basic and specialized versions of the aircraft airframe 

perform a diverse number of roles, including airlift support, aeromedical missions, 

weather reconnaissance, and natural disaster relief missions. The WC-130J version 

provides weather reconnaissance and the EC-130J version provides psychological 

operations capabilities.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 97

STRATEGIC CAPABILITY

C-13

0

J

contractors

Prime: Lockheed Martin (GA)

Subcontractor(s):Engine - Rolls 

Royce (IN); Engine Subsystem

- GKN Aerospace (UK); Propellers 

and Avionics - Smith Aerospace 

(U.S. and UK)

specifications

Weight 164,000 lb.

Range 3,600 nautical miles (NM), Global with in-flight refueling 

(EC-130J)

Dimensions

C-130J (Short): Wingspan - 132.6 ft.; Length - 97.8 ft.; 

Height - 38.8 ft. C-130J: Wingspan -132.6 ft.; Length - 112.8 

ft.; Height - 38.8 ft.

Service Ceiling 33,000 ft.

Speed 342 knots

Payload/Passenger 

Capacity

Load Comparisons C-130E/H/J (Short) C-130J

Payload 42,000 lb. 47,000 lb.

Cargo Floor Length 40 ft. 55 ft.

463L Pallets 6 8

Medical Litters 74 97

CDS Bundles 16 24

Combat Troops 92 128

Paratroopers 64 92

Acquisition status

Program Status

Full Rate Production through 2008; Projected inventory 

- 82; FY03 multi-year contract will deliver 42 C-130Js, 

FY05–FY09. FY06 GWOT Supplemental added 3 C-130Js 

AMC will receive its first C-130J in FY07 while USAFE receives 

its first C-130J in FY09

Unit Assignment Keesler AFB, MS; Baltimore, MD; Harrisburg, PA; Quonset, RI; 

Channel Islands, CA; Little Rock, AR 

Current Inventory 53 fielded (26 C-130J, 10 C-130J (Short), 10 WC-130J, and 

7 EC-130J)

Future Upgrades

Communication, Navigation & Safety/Air Traffic Management (CNS/ATM) requirements will be achieved through 

Block Upgrade Program
MISSION

98 UNITED STATES AIR FORCE

CBU-87/103 Combined Effects Munition (CEM)

mission

Provide penetration, fragmentation, and incendiary effects for dispersed light armor and personnel targets.

description

The Cluster Bomb Unit (CBU)-87 Combined Effects Munition (CEM) is a multi-purpose 

cluster weapon (penetration, fragmentation, incendiary effects) for dispersed light 

armor and personnel targets. After release from the aircraft, and at pre-determined 

flight parameters, the CBU-87 dispenses 202 BLU-97 bomblets (3-lb. multi-purpose 

submunitions) over the target area in a circular pattern (pattern characteristics are 

determined by dispense conditions and winds). The CBU-87 improves combat efficiency. Using the CBU-87 (and area attack weapons in general) decreases the time 

required to destroy necessary targets in a campaign, decreases the number of sorties 

required, keeps aircrews out of harm’s way, and decreases the number of weapons 

required to accomplish the mission. The CBU-103 combines the CBU-87 and the Wind 

Corrected Munitions Dispenser (WCMD) tail kit which inertially steers the munition 

from a known release point to precise target coordinates while compensating for 

launch transients, winds aloft, surface winds, and adverse weather.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 99

STRATEGIC CAPABILITY

CBU-87

/

1

0

3 Combined Eff

e

cts M

u

nition (C

EM)

contractors

Prime: Aero General/Honeywell 

(MN); Alliant Tech (MN)

specifications

Weight ~950 lb.

Range 

Two CEM configurations: CBU-87 (static tail): ballistic trajectory; CBU-103 (Wind Corrected Munition Dispenser (WCMD) 

tail): 10 nautical miles (NM)

Armament Contains 202 BLU-97 (3-lb.) combined effects bomblets 

(shaped charge/fragmentation/incendiary)

Dimensions Length: 92 in.; Diameter: 15.6 in.

Coverage

Coverage area (submunition pattern size) depends on many 

factors, but the pattern is typically circular with a diameter 

of about 200 ft.

Compatability

The following aircraft can employ the CEM:

CBU-87; F-16, F-15E, F-117A, A-10, B-52, B-1B, B-2; 

CBU-103; F-16, F-15E, B-52, B-1B

Acquisition status

Program Status No longer in production

Current Inventory CBU-87 approximately 87,000; CBU-103 approx 19,800

Future Upgrades None
MISSION

100 UNITED STATES AIR FORCE

CBU-89/104 Gator

mission

Provide a cluster bomb weapon containing anti-personnel and anti-armor bomblets for area denial missions.

description

The Cluster Bomb Unit (CBU)-89 GATOR is a cluster weapon that contains anti-personnel and anti-armor bomblets. It is designed for area denial missions. The CBU-89 

GATOR dispenses 72 BLU-91 anti-tank bomblets and 22 BLU-92 anti-personnel 

bomblets over the target area in a circular pattern (pattern characteristics are determined by dispense conditions and winds). The CBU-89 improves combat efficiency. 

Using CBU-89 (and area attack weapons in general) decreases the time required to 

destroy necessary targets in a campaign, reduces the number of sorties required, 

keeps aircrews out of harm’s way, and decreases the number of weapons required to 

accomplish the mission. The CBU-89 contains a self destruct mechanism which can be 

set for three different time delays. The CBU-104 combines the CBU-89 and the Wind 

Corrected Munitions Dispenser (WCMD) tail kit which inertially steers the munition 

from a known release point to precise target coordinates while compensating for 

launch transients, winds aloft, surface winds, and adverse weather.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 101

STRATEGIC CAPABILITY

CBU-89

/

1

0

4 Gator

contractors

Prime: Honeywell (MN); Aerojet 

(CA); General Dynamics (FL); Alliant 

Tech (MN)

specifications

Weight Approximately 705 lb.

Range 

Gator configurations: CBU-89 (static tail): ballistic trajectory; 

CBU-104 (Wind Corrected Munition Dispenser (WCMD) tail): 

10 nautical miles (NM)

Armament Contains 72 BLU-91 anti-armor bomblets (4.31 lb. each) and 

22 BLU-92 anti-personnel bomblets (3.75 lb. each)

Dimensions Length: 92 in.; Diameter: 15.6 in.

Coverage

Coverage area (submunition pattern size) depends on many 

factors, but the pattern is typically circular with a diameter 

of about 200 feet.

Compatability

The following aircraft can employ the Gator: 

CBU-89: F-16, F-15E, F-117A, A-10, B-52, B-1B, B-2;

CBU-104: F-16, F-15E, B-52, B-1B

Acquisition status

Program Status No longer in production

Current Inventory CBU-89 Approx 9,900; CBU-104 Approx 100

Future Upgrades None
MISSION

102 UNITED STATES AIR FORCE

CBU-97/105 Sensor Fused Weapon (SFW)

Mission

Conduct persistent surface attacks and destroy moving and fixed land 

combat vehicles, including main battle tanks, providing multiple kills 

per weapon. 

Description

The Cluster Bomb Unit (CBU)-97 Sensor Fused Weapon (SFW) contains 10 BLU-108 

submunitions, each with four projectiles, for a total of 40 independently targeted 

warheads. The warheads have an active laser and passive infrared (IR) sensors. The 

40 warheads search a target area up to 30 acres and fire an Explosively Formed 

Projectile (EFP) into the target designated by correlating the active and passive sensor 

signatures. The kill mechanism is an EFP copper liner formed with 2.2 lb. of PBXN-11 

explosive. The explosive force forms the copper into an armor penetrating projectile 

accelerated to hypervelocity. The CBU-105 combines the CBU-97 and the Wind 

Corrected Munitions Dispenser (WCMD) tail kit which inertially steers the munition 

from a known release point to precise target coordinates while compensating for 

launch transients, winds aloft, surface winds and adverse weather.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 103

STRATEGIC CAPABILITY

CBU-97

/

1

0

5

Sensor F

used 

W

eapon (

S

F

W)

Contractors

Prime: Textron (MA) 

Subcontractor(s): Day & 

Zimmerman Inc (KS); Alliant 

Techsystems (WV, WI); General 

Dynamics (WA); Hi Shear (CA); 

Kurt Manufacturing (MN); Pacific 

Scientific (AZ); Pioneer Aerospace 

(CT); Reynard Corp (CA); Tundra 

Semiconductor (ME) 

specifications

Weight 920 lb. 

Range Two SFW configurations: CBU-97 (static tail): ballistic 

trajectory; CBU-105 (WCMD tail): 10 nautical miles (NM)

Armament 10 BLU-108 submunitions

Dimensions Length: 91 in.; Diameter: 15.6 in.

Coverage The 40 warheads scan a target area up to 30 acres 

(1,600 ft. x 700 ft.).

Compatability

The following aircraft can employ the SFW: 

CBU-97: F-16, F-15E, A-10, B-52, B-1B, B-2;

CBU-105: F-16, F-15E, B-52, B-1B

Acquisition status

Program Status Production ends FY07

Current Inventory CBU-97: approximately 90; CBU-105: 3,100

Future Upgrades None
MISSION

104 UNITED STATES AIR FORCE

Combatant Commanders Integrated Command and Control

System (CCIC2S)

mission

Provide fixed command and control (C2) capabilities to support 

NORAD’S commander in executing aerospace warning and control 

missions; support the USSTRATCOM commander in executing space 

operations, and coordinate global missile defense missions, including 

support to other combatant commanders. 

description

The Combatant Commanders Integrated Command and Control System (CCIC2S) is the 

operational-level C2 system for Air Force space systems. For NORAD, CCIC2S provides 

the capabilities to command and control NORAD regions and sectors; for USSTRATCOM, CCIC2S provides the capabilities to command and control service components. 

These components include: Air Force component to USSTRATCOM [JSpOC]; Naval 

Networks and Space Operations Command [NNSOC]; U.S. Army Space and Missile 

Defense Command/Army Strategic Command [SMDC/ARSTRAT]; and space wings and 

units in support of the space operations mission. In addition, CCIC2S capabilities support the Integrated Tactical Warning and Attack Assessment (ITW/AA) air defense and 

space operations situational requirements of the government of Canada, combatant 

commanders, governmental agencies, and international and commercial partners.

The system will incorporate a standards-based approach, including Network Centric 

Enterprise Services. The system can be leveraged for space use. The Single Integrated 

Space Picture (SISP) is a project under CCIC2S and will provide command and control 

of space forces.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 105

STRATEGIC CAPABILITY

Combatant Commanders Integr

ated Command 

and Contro

l

Syste

m (CCIC2S)

contractors

Prime: Lockheed Martin (CO)

Subcontractor(s): Digital Net 

(BAE-IT) (CO); Northrop Grumman 

(Aerojet ATESC) (CA); Northrop 

Grumman-Electronic Systems (CA); 

Boeing (VA); Computer Science 

Corp. (VA)

specifications

Interoperability

The system will incorporate a standards-based approach, 

including Network Centric Enterprise Services, consistent 

with the DoD Information Technology Standards Registry.

Standards Compliance

The system adheres to the Chairman Joint Chiefs of Staff 

(CJCS) ITW/AA standards. The space command and control 

section of CCIC2S is not ITW/AA required.

Acquisition status

Program Status

Air & Missile capabilities are in sustainment and space 

capabilities development is being migrated to a different 

program.

Future Upgrades

Air & Missile capabilities are in sustainment and all space 

capabilities development is being migrated to a different 

program.
MISSION

106 UNITED STATES AIR FORCE

Combat Survivor Evader Locator (CSEL)

mission

Provide enhanced, 24-hour, assured, two-way, secure combat search 

and rescue satellite communication and location capabilities. 

Description

The Combat Survivor Evader Locator (CSEL) is an Air Force-led joint program that uses 

precise GPS positioning and advanced anti-spoofing technologies to provide a reliable 

and accurate survivor location, an optimized waveform to reduce detectability, and 

increased probability of collection by national assets. CSEL replaces the antiquated 

PRC-90/-112 survivor radios with a new over-the-horizon (OTH), end-to-end system 

that provides assured 24-hour, two-way, secure satellite communications along with 

military GPS that includes anti-jamming and anti-spoofing. CSEL utilizes the international search and rescue satellite system (SARSAT) for polar-area over-the-horizon 

(OTH) data communications. With these new capabilities, CSEL will increase rescue 

force success rates in ongoing contingency operations, providing rapid and accurate 

location and authentication of survivor/evaders in minutes, compared to what can 

take days today. CSEL includes three segments: hand-held radio, OTH satellite communications, and search and rescue center computer application.
THE AIR FORCE HANDBOOK 2007 107

STRATEGIC CAPABILITY AGILE COMBAT SUPPORT

Combat Su

rvivor Evader Locator (CSEL)

contractors

Prime: Boeing (CA);

Subcontractor(s): Thales 

Communications (MD) ; 

Interstate Electronics Corp. (CA); 

Senior Systems Technology (CA)

specifications

Size Width: 3 1/4 in.; Length: 8 in.; Depth: 1 3/4 in.

Weight 30.7 oz. with non-rechargable batteries; 33.4 oz. with 

rechargable batteries

Range Global coverage

Coverage Global

Capacity/Satellite

CSEL operates with Ultra High Frequency (UHF) satellites, 

UHF Follow-On (UFO) and Search and Rescue Satellite 

(SARSAT), and national assets.

Interoperability Interoperable with joint radios and satellites per military 

and commercial standards

Compatibility Compatible with radios, satellites, and user input/output 

devices per military and commercial standards 

Acquisition status

Program Status 1QFY07: Full rate production approved; CSEL fielded with 

Army, Navy, and Air Force

Current Inventory CSEL has delivered 11,000 radios as of December 2006

Future Upgrades Terminal Area Communication – Early CY08; Terminal Area 

Guidance – Early CY09
MISSION

108 UNITED STATES AIR FORCE

Control and Reporting Center (CRC)

mission

Provide the Joint Forces Air Component Commander (JFACC) with the 

capability to conduct theater air operations including joint, U.S., and 

combined operations.

description

The Control and Reporting Center (CRC) is the Air Force’s only 24/7 persistent deployable ground battle management command and control (BMC2) platform employed 

at the tactical level of war. The CRC is the most forward-based link in the Joint Battle 

Management Command and Control (JBMC2) family of systems. It is interoperable 

with other JBMC2 systems and provides real-time shared situational awareness at the 

tactical level and common shared situational awareness at the operational level. The 

CRC conducts detailed air space management, air surveillance, aircraft identification, 

data link management, and theater air defense. The CRC provides the decision superiority that enables more agile, more lethal, and survivable joint operations. It may be 

employed by itself or in combination with other ground-based and airborne tactical 

C2 assets and supports a broad range of military operations. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 109

STRATEGIC CAPABILITY

Contro

l

and 

R

e

porting Center (C

RC)

contractors

Prime: Thales Raytheon (CA)

Subcontracors: Sensis Group (NY); 

Technology Services Corp (MD)

specifications

Size Numerous configurations of trucks, tents, and computer 

equipment

Acquisition status

Program Status CRC is fielded. Replacement system, the Battle Control 

System – Mobile, is Post Milestone (MS) B for Spiral 3

Unit Assignment

Active: Eglin AFB, FL; Hill AFB, UT; Mountain Home AFB, ID; 

Spangdahlem AB, GE; Aviano AB, IT

Air National Guard: Orange, CT; Savannah, GA; Gulfport, MS

Current Inventory 96 Operations Modules (OM), 41 RADARs
MISSION

110 UNITED STATES AIR FORCE

Counterspace Systems

mission

Protect friendly space-related capabilities from enemy attack or interference and prevent adversaries from using their space capabilities 

against us. 

description

The Counterspace Systems program is designed to meet current and future military 

space control needs. It supports acquisition of both the Offensive Counterspace and 

Defensive Counterspace systems. A current project within this program is the Counter 

Communications System (CCS). This is an offensive electronic warfare system designed to disrupt adversary satellite-based communications using reversible, nondestructive means. Other projects include the Rapid Attack Identification Detection and 

Reporting System (RAIDRS) and Command and Control elements that are required to 

execute counterspace missions. RAIDRS is a defensive counterspace system designed 

to detect, report, identify, locate, and classify attacks against U.S. military space 

assets. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 111

STRATEGIC CAPABILITY

Co

unterspace 

Syste

m

s

contractors

Prime:CCS - Harris Corp. (FL); 

Rapid Attack Identification Detection and Reporting System, first 

phase (Block 10) - Integral Systems, 

Inc. (MD) 

specifications

Coverage

CCS and Deployable RAIDRS elements are transportable 

via C-130. RAIDRS will have worldwide coverage. CCS will 

provide coverage within the Joint Operating Area where it 

is deployed.

Interoperability Interoperable with all space control assets

Acquisition status

Program Status

Three additional Block 10 CCS systems being procured in 

FY06/07. Block 20 system in pre-acquisition risk reduction. 

RAIDRS: Block 10 system in development. Critical Design 

Review (CDR) completed for 1QFY07.

Unit Assignment

CCS is assigned to the 76th Space Control Squadron, Peterson AFB, CO and the 4th Space Control Squadron, Holloman 

AFB, NM. RAIDRS will be assigned to the 21st Space Wing, 

Peterson, AFB, CO.

Current Inventory CCS: Three Block 10 systems delivered, currently undergoing 

capability upgrades
MISSION

112 UNITED STATES AIR FORCE

CV-22B

mission

Conduct long-range, adverse weather, clandestine penetration of 

medium-to-high threat environments in politically or militarily denied 

areas to infiltrate, exfiltrate, and resupply Special Operations Forces 

(SOFs).

description

The CV-22B is designed to insert and extract SOF units deep into denied areas during 

one period of darkness. The state-of-the-art, tilt-rotor platform combines the vertical takeoff and landing capability of a helicopter with the long-range, high-speed 

performance of a fixed-wing aircraft. The CV-22B variant of the V-22 will feature a 

multimode terrain-following/terrain-avoidance radar, radar and infrared warning 

and countermeasure systems, additional fuel tanks, and upgraded communications 

and navigation systems. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 113

STRATEGIC CAPABILITY

CV-22

B

contractors

Prime: Bell/Boeing (joint venture 

between Bell/Textron, TX, and 

Boeing ADS, PA)

Subcontractor(s): Propulsion

- Rolls Royce (IN); TF/TA Radar

- Raytheon (TX); Electronic Warfare 

Suite - ITT Avionics (NJ)

specifications

Weight Empty: 35,800 lb.; Max Vertical Takeoff: 52,600 lb.; Short 

Takeoff: 57,000 lb.; Self-Deploy Weight: 60,500 lb. 

Range 500 nautical miles (NM) combat radius (unlimited with 

aerial refueling)

Dimensions Wingspan: 45.8 ft.; Length: 57.3 ft.; Height: 22.1 ft.; 

Rotors tip-to-tip: 84.6 ft.

Service Ceiling 25,000 ft.

Speed 230 knots cruise

Payload 20,000 lb. internal or 10,000 lb. external with minimum fuel

Passenger Capacity 18 Special Operations Forces troops

Acquisition status

Program Status

In September 2005, the V-22 program was approved to start 

full-rate production. CV-22B is undergoing Block 10 developmental testing at Edwards AFB. An Operational Utility 

Evaluation was completed July 2006 certifying readiness 

for training operations at Kirtland AFB. Block 10 Initial 

Operational Testing & Evaluation (IOT&E) is planned for 

October 2007 to certify operational readiness. The projected 

inventory will be 50. The Initial Operational Capability phase 

is planned for 2009.

Unit Assignment 71st Special Operations Squadron, Kirtland AFB, NM 

Current Inventory 4

Future Upgrades

Block 20 planned for FY08 start. Upgrades will include: 

Emergency/Reserve Power, tactical air data link, communications upgrades, high-altitude conversion operations, 

Terrain Following/Terrain Avoidance (TF/TA) radar enhancement
MISSION

114 UNITED STATES AIR FORCE

Defense Meteorological Satellite Program (DMSP)

mission

Provide global visible and infrared cloud cover imagery and other atmospheric, oceanographic, land surface, and space environment data to 

support multi-service requirements and battlespace characterization 

everywhere that U.S. forces operate.

description

The Defense Meteorological Satellite Program (DMSP) designs, builds, launches, and 

maintains satellites monitoring the meteorological, oceanographic,terrestrial and 

solar environments. Using the DMSP data, military weather forecasters can detect 

developing patterns of weather and track existing weather systems over remote 

areas, including the presence of severe thunderstorms, dust storms, hurricanes, and 

typhoons. This data is vital to the effective employment of forces and weapon systems worldwide. The program includes five satellites flying in two sun-synchronous 

orbits. The primary weather sensor on DMSP is the Operational Linescan System, 

which provides continuous visual and infrared imagery of cloud cover over an area 

1,600 nautical miles wide. Additional satellite sensors measure atmospheric vertical 

profiles of moisture and temperature, sea surface winds, and the presence of soil 

moisture. The DMSP satellites also measure space environment charged particles 

and electromagnetic fields to assess the impact of the ionosphere on ballistic-missile 

early warning radar systems, electrical grids, satellite operations, and long-range 

communications. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 115

STRATEGIC CAPABILITY

D

e

fense Meteoro

logical Satellite Program (

D

M

SP)

contractors

Prime:Spacecraft - Lockheed 

Martin (CA); Sensors - Northrop 

Grumman (MD)

Subcontractors:Sensor - Northrop 

Grumman (CA); Flight Software 

Independent Verification and 

Validation (IV&V) - Integral Systems, Inc. (MD)

specifications

Weight 2720.1 lb.

Range Polar-orbiting at 450 nautical miles (NM)

Dimensions 14.1 ft. long (4.29 m) without solar panels deployed

Coverage Full global coverage every 12 hours

Capacity/Satellite Launched on a medium Evolved Expendable Launch Vehicle

Interoperability Air Force Weather Agency ensures DMSP data is interoperable with a broad range of user platforms.

Compatability Air Force Weather Agency ensures DMSP data is compatible 

with a broad range of user platforms.

Acquisition status

Program Status All DMSP satellites have been delivered , but not all DMSP 

satellites have launched

Unit Assignment Operated by National Oceanic and 

Atmospheric Administration

Current Inventory 5 satellites

Future Upgrades All DMSP satellites have been delivered
MISSION

116 UNITED STATES AIR FORCE

Defense Satellite Communications System (DSCS) III

mission

Provide super-high freqency satellite communications to troops in the 

field as well as commanders at multiple locations worldwide. 

description

The Defense Satellite Communications Systems (DSCS) is the workhorse of military 

satellite communications. The system provides uninterrupted secure voice and high 

rate data communications to DoD users for monitoring events and deploying and 

sustaining forces anywhere in the world. It is used for high-priority command and 

control communication such as the exchange of wartime information between 

defense officials and battlefield commanders. The military also uses DSCS to transmit 

space operations and early warning data to various systems and users. The system 

consists of nine Phase III DSCS satellites that orbit the earth at an altitude of more 

than 22,000 miles. Each satellite uses six super high frequency transponder channels 

capable of providing secure voice and high data rate communications. The system 

also features a single-channel transponder for disseminating emergency action and 

force direction messages to nuclear-capable forces. The single steerable dish antenna 

provides an increased power spot beam which can be tailored to suit the needs of 

different size user terminals. DSCS satellites can resist jamming and consistently 

exceed their 10-year design life. DSCS users operate on the ground, at sea, or in the 

air. Members of the 50th Space Wing’s 3rd Space Operations Squadron at Schriever Air 

Force Base, CO, provide satellite command and control support for all DSCS satellites.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 117

STRATEGIC CAPABILITY

D

e

fense Satellite Commu

nications 

Syste

m (DS

C

S) III

contractors

Prime: Lockheed Martin Missiles 

and Space (global)

specifications

Weight 2,716 lb. (1,232 kg)

Range Capability to orbit the earth at an altitude of more than 

22,000 miles

Dimensions Length: 6 ft. (1.8 m); Height: 6 ft. (1.8 m); Width: 7 ft. 

(2.1 m); 38-ft. span (11.5 m) with solar arrays deployed

Coverage 65° N to 65° S 

Capacity/Satellite Five satellite (primary) constellation in geosynchronous 

orbit, with four residual satellites 

Acquisition status

Program Status Complete

Unit Assignment 3 Space Operations Squadrons (SOPS)

Current Inventory 5 Primary Satellites, 4 Residual Satellites

Future Upgrades None
MISSION

118 UNITED STATES AIR FORCE

Defense Support Program (DSP) 

mission

Provide early detection and warning of missile launches and nuclear 

explosions to National Command Authorities and operational commands. The satellite constellation has been the cornerstone of North 

America’s early warning system for more than 30 years. 

description

DSP satellites orbit the earth about 35,780 kilometers over the equator in geosynchronous orbits. They use infrared sensors to detect heat from missile and booster 

plumes against the earth’s background.

Typically, DSP satellites were launched into geosynchronous earth orbit on a Titan 

IV booster and inertial upper stage combination. However, one DSP satellite was 

launched using the space shuttle on mission STS-44 (Nov. 24, 1991). The next and 

final DSP satellite is scheduled for launch on the new Evolved Expendable Launch 

Vehicle Delta IV, Heavy in FY07.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 119

STRATEGIC CAPABILITY

D

e

fense Support Program (DSP) 

contractors

Prime: Northrop Grumman (CA) 

specifications

Weight 5,250 lb. (2,386 kg)

Dimensions Height: 32.8 ft. (10 m) on orbit; Diameter: 22 ft. (6.7 m) on 

orbit

Coverage Continuous global coverage

Interoperability Interoperable with Cheyenne Mountain Operations Center 

and other strategic users 

Acquisition status

Program Status The Defense Support Program (DSP) has completed production. One satellite, DSP-23, is awaiting launch. 

Unit Assignment

The 460th Space Wing, with headquarters at Buckley Air 

Force Base, CO, has units that operate DSP satellites and report warning information, via communications links, to the 

North American Aerospace Defense Command/U.S. Northern 

Command and U.S. Strategic Command early warning 

centers within Cheyenne Mountain, located near Colorado 

Springs, CO. These centers immediately forward data to various agencies and areas of operations around the world.
MISSION

120 UNITED STATES AIR FORCE

Deliberate Crisis and Action Planning

and Execution Segments (DCAPES) 

mission

Present, plan, source, mobilize, deploy, account for, sustain, redeploy, 

and reconstitute forces for contingency and crisis operations. Annually 

deploys over 69,000 Airmen to 64 countries. Real-time collaborative tool/

environment providing accurate deliberate and crisis action planning. 

description

Deliberate Crisis and Action Planning and Execution Segments (DCAPES) is being 

developed as the next-generation Air Force interface to the Joint Operational Planning and Execution System (JOPES). It is intended to tightly synchronize data across 

a range of Air Force and Joint planning support systems to provide a more effective 

crisis action planning capability for a wider range of operational scenarios and will 

fully support the force provider function of the Air Forces (AFFOR) Commander. 

DCAPES provides a real time, two-way interchange of personnel, manpower, logistics, 

and operational data between the Air Force and the warfighting Combatant

Commanders. It matches people, cargo, and airframes/weapon systems to the Combatant Commander’s warfighting requirements.
GLOBAL REACH GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 121

STRATEGIC CAPABILITY

D

eliber

ate Crisis 

and A

c

tion Planning 

and 

Execu

tion 

Seg

ments (

DCAPES)

contractors

Prime: Computer Sciences Corp 

Federal Sector Defense Group (VA)

Subcontracor:Tier II Helpdesk 

Support – SAIC (VA)

Acquisition status

Program Status

Evolutionary acquisition strategy; incremental spiral development with multiple software releases to accommodate 

refinement and prioritization of user requirements, and 

improve adaptability with commercial technology.

Increment 2a - ACAT III – Post Milestone C; v4.0.2.0 fielded: 

October 2006

Unit Assignment

Increment 2 a: v4.0.3.0 – Air Force Manpower/Personnel 

System (base level) Deployed—legacy system retired; War 

and Mobilization Planning System, Unit Type Code Management Increment 2b – ACAT IAC – Milestone B/Contract 

Award – 1QFY09
122 UNITED STATES AIR FORCE

MISSION

Distributed Mission Operations (DMO)

mission

Provide a networked combat training and mission rehearsal capability that will develop the warfighter’s individual and team skills to accomplish the complex operations and functions necessary for today’s 

ground, air, and space operations.

description

An Air Force readiness capability, interconnecting high-fidelity aircrew training 

devices, C2, and ISR simulators in a realistic, immersive training environment via 

telecommunications networks. It provides high-fidelity on-demand training at warfighter locations worldwide. DMO focuses on warfighter individual and team skills. It 

is based on scalable packages from operational to strategic level of war. DMO allows 

warfighters to train as teams while remaining at home stations, reducing Ops Tempo 

and travel costs. DMO will provide a fully integrated Air and Space component of the 

Joint National Training Capability (JNTC). It will enable joint, inter-service/agency, 

and Air Force exercises, experiments, wargames, RDT&E and mission rehearsal as the 

supporting networks and systems evolve.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 123

Distributed Mission Oper

ations (

D

M

O)

contractors

Prime: DMO Operations & Integration - Northrop Grumman (FL)

specifications

Interoperability Capable of integration with Joint and Coalition Training/Mission Rehearsal systems

Acquisition status

Program Status Operational

Unit Assignment

F-15C: 33rd Fighter Wing, Eglin AFB, FL; 1st Fighter Wing 

Langley AFB, VA; 3rd Wing, Elmendorf AFB, AK; 18th Wing, 

Kadena AB, Japan; 48th Fighter Wing, Lakenheath AB, England; 20th Fighter Wing, Shaw AFB, SC; 366th Fighter Wing, 

Mt Home AFB, ID; 35th Fighter Wing, Misawa AB, Japan; 

52nd Fighter Wing Spangdahlem AB, Germany 

AWACS: 552nd Air Control Wing Tinker AFB, OK; 3rd Wing, 

Elmendorf AFB, AK; 18th Wing, Kadena AB, Japan

JSTARS: 116th Air Control wing Robbins AFB, GA

Rivet Joint: 55th Wing, Offutt AFB, NE

Distributed Mission Operations Center (DMOC): 

505th Distributed Warfare Group, Kirtland AFM, NM

Distributed Training Operations Center (DTOC) ANG:

132nd Fighter Wing, Des Moines International Airport

Current Inventory

F-15C: 5 Mission Training Centers (MTCs)/18 cockpits 

F-16 Blk 50: 4 MTCs/14 Cockpits

AWACS: 5 sites/ 70 positions 

JSTARS: 1 MTC /18 positions 

Rivet Joint: 1 MTC/17 positions 

Distributed Mission Operations Center

Distributed Training Operations Center

Future Upgrades F-15E, A-10, B-1, B-2, B-52, F-16 Blk 40, F-22, F-35, Air Operations Centers (AOC), Control and Reporting Centers (CRC)
MISSION

124 UNITED STATES AIR FORCE

E-3 Sentry Airborne Warning and Control System (AWACS)

mission

Provide all-weather surveillance, command, control, and communications needed by commanders of U.S., NATO, and other allied air defense 

forces.

description

The E-3 Sentry Airborne Warning and Control System (AWACS) aircraft provides responsive and flexible real-time command and control/battle management in support 

of worldwide operational employment of U.S. and coalition forces. AWACS provides 

persistent and survivable surveillance, battle management, weapons control, threat 

warning, and combat ID information in support of commander taskings. It gives commanders a self-contained and worldwide, around-the-clock capability to prosecute 

air and ground campaigns. The E-3 Sentry is a modified Boeing 707/320 commercial 

airframe with a rotating radar dome. The radar combined with an identification 

friend or foe subsystem can look down to detect, identify, and track enemy and 

friendly low-flying aircraft by eliminating ground clutter returns that confuse other 

radar systems. Other major subsystems in the E-3 include navigation, communications, computers (data processing), and displays.
GLOBAL POWER

GLOBAL REACH GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 125

STRATEGIC CAPABILITY

E-3

Sentry Air

borne Warning 

and Contro

l

Syste

m (AWAC

S)

contractors

Prime: Boeing Aerospace Co. (WA)

Subcontractor(s): Northrop 

Grumman (MD)

specifications

Size Length: 145 ft., 8 in. (44 m); Wingspan: 130 ft., 10 in. 

(39.7 m); Height: 41 ft., 4 in. (12.5 m) 

Weight 347,000 lb. (156,150 kg) 

Range More than eight hours (unrefueled) 

Coverage

The radar has a range of more than 250 miles (375.5 km) for 

low-flying targets and farther for aerospace vehicles flying 

at medium to high altitudes

Acquisition status

Program Status

The AWACS Block 40/45 Upgrade is in the middle of System 

Development and Demonstration (SDD). It includes several 

projects aimed at reducing operator workload, providing a 

fused air picture to the warfighter, and transmitting that 

air picture off-board in a more timely manner Integrated 

Demand Assigned Multiple Access (DAMA) Global Air Traffic 

Management (GATM) (IDG) expands user availability of 

severely limited DoD UHF SATCOM channels through the use 

of DAMA and meets mandate for International Civil Aviation compliance on near-term air traffic control navigation 

requirements. The AWACS fleet is currently being modified 

with IDG 

Unit Assignment 552 Air Control Wing, Tinker AFB, OK

Current Inventory 32 operational aircraft and 1 test aircraft
126 UNITED STATES AIR FORCE

MISSION

E-4B National Airborne Operations Center (NAOC)

mission

Provide a highly survivable command, control, and communications 

center to direct U.S. forces, execute emergency war orders, and coordinate actions by civil authorities in case of national emergency or 

distruction of ground command and control centers. 

description

The E-4B National Airborne Operation Center (NAOC) serves as the National Airborne 

Operation Center for the President and the Secretary of Defense. The E-4B, a militarized version of the Boeing 747-200, is a four-engine, swept-wing, long-range, 

high-altitude airplane capable of being refueled in flight. The main deck is divided 

into six functional areas; a command work area, conference room, briefing room, an 

operations team work area, a communications area, and rest area. An E-4B crew may 

include up to 114 people, including a joint-service operations team, an ACC flight 

crew, a maintenance and security component, a comminications team, and selected 

augmentees.The E-4B has electromagnetic pulse protection, nuclear and thermal 

shielding, and an advanced, secure, radio and satelite communications system with 

connectivity to strategic and tactical command and control systems. 
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 127

E-4B National Air

borne Oper

ations Center (

N

A

OC)

contractors

Prime: Boeing Wichita Development and Modernization Center (KS)

Subcontractors: Raytheon (FL);

Rockwell Automation (TX); L-3 Communications (TX); Boeing Aerospace 

Operations (OK)

specifications

Weight Maximum Gross Taxi Weight: 803,000 lb.; Maximum Takeoff 

Weight: 800,000 lb.; Dry Weight: 526,500 lb.

Range 72 hours with mid-air refueling

Armament None

Dimensions Height: 63 ft., 5 in.; Length: 231 ft., 4 in.; Width: 195 ft., 8 in.

Coverage Global

Capacity/Satellite

Satellite Connectivity: Defense Satellite Communications 

System; Milstar; MILSATCOMs; Connexions by Boeing 

broadband internet access; INMARSAT satellite network; 

AT&T SATSTAR Other Unique Connectivity: Northstar Ground 

Entry Point UHF Comms

Interoperability Enables worldwide communication among strategic and 

tactical satellite systems and the Airborne Operations Center

Compatability Yes

Acquisition status

Program Status Fielded

Unit Assignment 1st AACS, 55th Wing, Offutt AFB

Current Inventory 4 aircraft

Future Upgrades None
MISSION

128 UNITED STATES AIR FORCE

E-8C Joint STARS

mission

Provide surveillance of fixed and moving ground targets to assess the 

enemy situation and to support location, tracking, targeting, and attack operations. These functions support the primary mission of Joint 

STARS—to provide dedicated support to ground and air theater commanders. 

description

The E-8C Joint Surveillance Target Attack Radar System (Joint STARS) is an airborne 

battle management and command and control (C2) platform that provides long-endurance, all weather surveillance and targeting information on moving and stationary targets via Ground Moving Target Indicator (GMTI) and Synthetic Aperture Radar 

(SAR) technologies. It sends GMTI and SAR data to shooters and Common Ground 

Stations to enhance combatant commanders’ battle management and situational 

awareness.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 129

STRATEGIC CAPABILITY

E-8C 

J

oint STARS

contractors

Prime: Northrop Grumman (FL, LA)

specifications

Weight 336,000 lb. (gross weight)

Range 8 hours, 20 hours with in-flight refueling

Dimensions Wingspan: 130 ft., 10 in.; Height: 42 ft., 6 in.; Length: 152 

ft., 11 in.

Coverage For Official Use Only-(not releasable)

Capacity/Satellite Three Demand Assigned Multiple Access (DAMA) SATCOM 

radios

Interoperability Enables communications and datalink information sharing 

with various U.S., UK, and coalition assets

Acquisition status

Program Status Post Milestone C; Modification and sustainment

Unit Assignment 116th Air Control Wing, Robins AFB, GA

Current Inventory 17 operations aircraft, 1 test aircraft, 1 pilot trainer aircraft

Future Upgrades Re-engining, Affordable Moving Surface Target Engagement 

(AMSTE), and Joint Tactical Radio System (JTRS) Phase I.
130 UNITED STATES AIR FORCE

MISSION

EC-130H Compass Call

mission

Conduct electronic attack and offensive information warfare from a 

stand-off jamming platform.

description

The EC-130H COMPASS CALL is the DoD’s premier Electronic Attack and Information 

Warfare weapon system COMPASS CALL’s mission is to counter advanced command, 

control, and communication (C3) systems and conduct medium range stand-off jamming of air defense radars. Its primary role is to increase the survivability of combat 

aircraft and aircrews by denying effective command and control of the enemy Integrated Air Defense System (IADS), and disrupting air defense surface-to-air missile 

(SAM) and anti-aircraft artillery (AAA) threats. COMPASS CALL also supports ground 

and special operations forces by denying hostile forces and terrorists the communications and situational awareness needed to coordinate operations against U.S. and 

allied troops. COMPASS CALL is a core component of the Joint Airborne Electronic Attack system of systems. With the ability to be quickly modified to counter new threats 

and targets, this versatile platform is able to bring essential capabilities to virtually 

any combat operation.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 131

EC-13

0

H Compass Call

contractors

Prime: L-3 Communications (TX); 

BAE Systems (NH)

Subcontractor(s): Raytheon 

Systems Corporation (IN); General 

Dynamics (CA)

specifications

Size Length: 100 ft.; Wingspan: 132 ft. 7 in.; Height: 38 ft. 3 in.

Weight Maximum takeoff weight: 155,000 lb.

Range Unlimited (air refuelable)

Coverage Line-of-sight

Acquisition status

Program Status Modification and sustainment

Unit Assignment 55th Electronic Combat Group (ACC), Davis Monthan AFB, AZ

Current Inventory 15 Total Aircraft Inventory (PAI) = 14 Primary Mission 

Aircraft (PMAI) and 1 flight deck trainer (PTAI)
MISSION

132 UNITED STATES AIR FORCE

Evolved Expendable Launch Vehicle (EELV) 

mission

Provide military, civilian, and commercial users a significantly more 

flexible, less costly, medium- to heavy-lift launch capability for placing 

large payloads into orbit. 

description

The Evolved Expendable Launch Vehicle (EELV) is composed of two families of launch 

vehicles—the Atlas V and the Delta IV—with the capability to accommodate light, 

medium, and heavy payloads for all users. The EELV system includes all equipment, 

facilities, and launch base infrastructure necessary to launch a payload, place it in 

the required delivery orbit, provide specified environments, provide EELV system 

maintenance, and perform any necessary recovery/refurbishment operations. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 133

STRATEGIC CAPABILITY

Ev

olved 

E

x

pendable Lau

n

ch Vehicle (EELV) 

contractors

Prime: United Launch Alliance (CO, 

CA, AL, TX, FL)

Subcontractor(s): Pratt & Whitney 

(FL); Alliant Techsystems; Mitsubishi Heavy Industries (Japan); 

B.F.Goodrich (NM); Aerospace (CA); 

Allied Signal Aerospace (AZ); KAMAG 

(Germany); Aerojet (CA); Keystone 

Engineering (LA); GDE Systems (CA); 

Arrowhead Products (CA); 

La Barge (AR); Honeywell (FL); Contraves (Switzerland); NPO Enerogomash (Russia); 

Moog Inc. (NY); Cincinnati Electronics (OH); United Engineering Co (MO); Lincoln 

Composites (NE)

specifications

Size Medium, intermediate, and heavy lift vehicles

Range All required satellite orbits

Coverage All required space orbits

Capacity/Satellite Pounds-to-orbit range: 2,500 lb.–48,260 lb. Range will vary 

depending on orbit, vehicle, and vehicle configuration.

Interoperability Capability to launch from both coasts

Compatibility Standard interface allows all DoD, NASA, and commercial 

payloads to launch on EELV.

Acquisition status

Program Status Program currently in full-rate production
134 UNITED STATES AIR FORCE

MISSION

Expeditionary Combat Support System (ECSS)

mission

Provide better, more efficient and less expensive logistics support to 

warfighters.

description

The Expeditionary Combat Support System (ECSS) will provide superior combat 

support information to Air Force and Joint users by 2012. The program will reduce the 

need for over 400 legacy systems while improving logistics processes within the Air 

Force Enterprise. The transformation will involve the use of a preferred commercialoff-the-shelf (COTS) Enterprise Resources Planning (ERP) suite and selected “bolt-on” 

systems, plus a Systems Integrator; overseeing the blueprinting, configuration, 

implementation, and roll-out of acquisition phases; and ensuring that world class 

technical/integration, change management, training, and program management 

processes and concepts are incorporated into the acquisition. ECSS will enable the Air 

Force to standardize processes across logistics (Transportation, Supply, and Maintenance & Repair) and other key business functions directly related to logistics (Engineering, Personnel, Acquisition and Finance), while reducing legacy systems within 

the Air Force Enterprise, with the goal of creating efficiencies. The Air Force logistics 

community is the major implementer of the ECSS ERP.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 135

E

x

pedition

ary Combat Support 

Syste

m (

E

CSS)

contractors

To be determined

Acquisition status

Program Status Milestone A

Future Upgrades To be determined
MISSION

136 UNITED STATES AIR FORCE

F-15A–D Eagle

mission

Provide all-weather, extremely maneuverable, air-to-air fighter capability designed to gain and maintain air supremacy over the battlefield 

and defend the homeland. 

description

The F-15A-D Eagle is designed to perform air-to-air missions with uncompromising 

performance. The Eagle’s air superiority is achieved through a mixture of unprecedented maneuverability, acceleration, range, weapons, and avionics. It can outperform and outfight enemy defense, outperform and outfight any current enemy 

aircraft at all altitudes, day or night, and in all types of weather. The Eagle has electronic systems and weaponry to detect, acquire, track and attack enemy aircraft while 

operating in friendly or enemy-controlled airspace. The weapons and flight control 

systems are designed so one person can safely and effectively perform air-to-air 

combat. The F-15A-D augments the F-22A as a proven air superiority aircraft employing all of the Air Force’s air-to-air missiles. F-15Cs were deployed to the Persian 

Gulf in 1991 in support of Operation Desert Storm where they proved their superior 

combat capability with a confirmed 36:0 kill ratio. F-15C fighters accounted for 36 of 

the 39 Air Force air-to-air victories. They have since been deployed to support Operations Southern/Northern Watch (the patrolling of the UN-sanctioned no-fly zones in 

Iraq), Operation Provide Comfort in Turkey (in support of NATO operations in Bosnia), 

Operation Enduring Freedom in Afghanistan, and Operation Iraqi Freedom. The USAF 

plans to keep 178 F-15C/Ds in the inventory through 2025. Modernization efforts 

include AESA radars, helmet mounted cueing systems, and GPS.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 137

STRATEGIC CAPABILITY

contractors

Prime: Boeing Aircraft (MO)

Subcontractor(s):Engine - Pratt 

& Whitney (CT); Radar - Raytheon 

(MS, CA); Avionics - Honeywell 

(NM), Northrop Grumman (IL)

Specifications

Weight 68,000 lb. (C/D maximum takeoff weight)

Range 3,450 mile ferry range with conformal fuel tanks and three 

external fuel tanks

Armament

One 20mm multi-barrel gun mounted internally with 940 

rounds of ammunition; Normal missile load is two AIM-9Xs 

and six AIM-120s.

Dimensions Wingspan: 42.8 ft.; Length: 63.8 ft.; Height: 18.5 ft.

Speed Mach 2.5 plus

Service Ceiling 50,000 ft.

Power Plant Two Pratt & Whitney F100-PW-100 or 220 turbofan engines 

with afterburners

Thrust 23,450-25,000 lb. each engine

Crew F-15A/C: one; F-15B/D: two

Acquisition Status

Program Status Modernization and sustainment

Current Inventory Active force, 359; Air National Guard, 140

Future Upgrades

Upgrades to the F-15A-D will maintain the aircraft’s operational effectiveness through 2025+, and will include 

active electronically scanned array radar, a digital electronic 

warfare suite, and a helmet mounted cueing system.

F-15A–

D Ea

g

l

e
MISSION

138 UNITED STATES AIR FORCE

F-15E Strike Eagle 

mission

Provide unique night/all-weather/all-altitude deep-penetration precision strike capability and air superiority. The F-15E also performs Close 

Air Support (CAS), Time Sensitive Targeting (TST), Dynamic Targeting, 

Destruction of Enemy Air Defenses (DEAD), Offensive and Defensive 

Counter Air, Homeland Defense, Global Persistent Attack, Non-Traditional Intelligence Surveillance and Reconnaissance, Strike, and Air 

Interdiction. 

Description

The F-15E Strike Eagle is a dual-role fighter designed to perform nearly all air-to-air 

and air-to-ground missions. It is a twin-engine, two-tail, two-seat, supersonic fighter 

capable of employing nearly all USAF air-to-ground and air-to-air munitions. The 

F-15E has an array of modern avionics and electronics systems that enable the pilot 

and weapons system officer to fight at all altitudes, day or night, and in all types 

of weather. Combining the highest fuel and weapons capacity of any fighter with 

systems such as Fighter Data Link, Night Vision Goggles, Low Altitude Navigation and 

Targeting Infrared for Night (LANTIRN) and infrared targeting pods, the F-15E has the 

capability to fight its way deep into enemy territory, destroy enemy ground positions 

with precision weapons, and then fight its way out. 

The F-15E has participated in nearly every combat operation since the First Gulf War 

(1991). It has flown combat operations over the former Yugoslavia (Deny Flight and 

Allied Force), Iraq (Northern Watch, Southern Watch, Provide Comfort and Iraqi Freedom), and Afghanistan (Enduring Freedom). In Operation Iraqi Freedom, the F-15Es 

penetrated deep into the Iraqi defenses to destroy key targets and are credited with 

destroying 65 MiGs on the ground as well 60% of the Iraqi Medina Republican Guard. 

The F-15E is going to be the basis of the legacy fighter force through 2030 and beyond. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 139

STRATEGIC CAPABILITY

F-15E STRIKE Ea

g

le 

contractors

Prime: Boeing Aircraft (MO) 

Subcontractor(s):Engine - Pratt 

& Whitney (CT); Radar - Raytheon 

(MS, CA); Avionics - Honeywell 

(NM); Avionics - Northrop 

Grumman (IL)

Specifications

Weight 81,000 lb. (maximum takeoff weight)

Range 2,400 mi. ferry range with conformal fuel tanks and three 

external fuel tanks

Armament

One 20mm multi-barrel gun mounted internally with 500 

rounds of ammunition; four AIM-120 Advanced Medium 

Range Air-to-Air (AMRAAM) missiles and four AIM-9 

Sidewinder missiles, or eight AIM-120 AMRAAM missiles; 

virtually all of the air-to-surface weapons in the Air Force 

inventory (nuclear and conventional), including GBU-28 

Bunker Buster, GBU-15, AGM-130, AGM-65 Maverick, GPS 

guided Joint Direct Attack Munition (JDAM), Laser Guide 

Bombs (LGB), and Small Diameter Bombs (SDB) 

Dimensions Wingspan: 42.8 ft.; Length: 63.8 ft.; Height: 18.5 ft.

Speed Mach 2.5 plus 

Service Ceiling 50,000 ft.

Power Plant Two Pratt & Whitney F100-PW-220 or 229 turbofan engines 

with afterburners

Thrust 25,000–29,000 lb. each engine

Crew Pilot and weapon systems officer

Acquisition Status

Program Status Modernization and sustainment

Current Inventory Active force, 224; Air National Guard, 0; Reserve, 0

Future Upgrades

Upgrades to the F-15E will maintain the aircraft’s operational effectiveness through 2030 and are planned to include an 

active electronically scanned array radar, a digital electronic 

warfare suite, and a helmet mounted cueing system.
MISSION

140 UNITED STATES AIR FORCE

F-16 Fighting Falcon 

mission

Provide low-cost, high-performance, air-to-air combat and air-to-surface 

attack capability.

description

The F-16 Fighting Falcon is a compact, maneuverable, multi-role fighter aircraft that 

is proven in air-to-air combat and air-to-surface attack. The F-16’s maneuverability 

and combat radius (distance it can fly to enter air combat, stay, fight and return) 

exceed that of potential threat fighter aircraft. It can locate targets in all weather 

conditions and detect low flying aircraft in radar ground clutter. In an air-to-surface 

role, the F-16 can fly more than 500 miles (860 km), deliver its weapons with superior 

accuracy, defend itself against enemy aircraft, and return to its starting point. In 

designing the F-16, advanced aerospace science and proven reliable systems from 

other aircraft such as the F-15 and F-111 were selected and combined to simplify the 

airplane and reduce its size, purchase price, maintenance costs and weight. Fully fueled, the F-16 can withstand up to nine G’s—nine times the force of gravity. Avionics 

systems include a highly accurate inertial navigation system coupled with a GPS by 

which a computer provides steering information to the pilot. The plane has UHF and 

VHF radios, instrument landing system, a warning system, and modular countermeasure pods to be used against airborne or surface electronic threats. During Operation 

Iraqi Freedom (OIF) the F-16 continued its superior performance in precision strike 

missions using a variety of GPS and laser guided weapons. Currently, the F-16 comprises 53 percent of the Air Force fighter force structure and provides 67 percent of 

the precision guided munitions capability in our Air Expeditionary Forces.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 141

STRATEGIC CAPABILITY

F-

16 Fighting Falcon 

contractors

Prime: Airframe - Lockheed Martin 

(TX); Engines - Pratt & Whitney 

(CT); General Electric (OH)

Subcontractors: Northrop Grumman (MD); Raytheon (TX); Israel 

Aircraft Industries (Israel); Honeywell International (CA, NJ, NM, MN)

Specifications

Weight 37,500 lb. (16,875 kg)

Range More than 2,000 mi. ferry range (1,740 nautical miles)

Armament

One M-61A1 20mm multibarrel cannon with 500 rounds; 

external stations can carry up to six air-to-air missiles, 

conventional air-to-air and air-to-surface munitions and 

electronic countermeasure pods.

Dimensions Length: 49 ft., 5 in. (14.8 m); Height: 16 ft. (4.8 m); 

Wingspan: 32 ft., 8 in. (9.8 m)

Service Ceiling Above 50,000 ft. (15 km)

Power Plant F-16C/D: one Pratt & Whitney F100-PW-200/220/229 or 

General Electric F110-GE-100/129

Thrust F-16C/D, 28,500 lb.

Crew F-16C, one; F-16D, one or two 

Acquisition Status

Program Status Sustainment, no new aircraft procurement planned 

at this time

Unit Assignment Active Air Force, Reserves, and Air National Guard

Current Inventory Active Force, F-16C/D, 714; Reserve, F-16 C/D, 69; and Air 

National Guard, F-16 C/D, 472

Future Upgrades

Major structural integrity modifications to the airframe 

and engines to extend the service life, and avionics modifications for performance improvements and weapons 

compatibility
MISSION

142 UNITED STATES AIR FORCE

F-16 HARM Targeting System (HTS) R6 and R7

mission

Provides F-16 aircraft with the capability of real-time targeting of 

enemy air defense system threats. 

description

The F-16 High-Speed Anti-Radiation Missile (HARM) targeting system detects and 

provides targeting information on enemy air defense radar outside the lethal range 

of their associated surface-to-air missiles (SAM). The system supports the F-16’s 

Suppression/Destruction of Enemy Air Defenses (SEAD/DEAD) mission. The HARM 

Targeting System (HTS) enables employment of the AGM-88 HARM in the “range 

known” mode—the missile’s most lethal mode. HTS targeting information increases 

HARM lethal range by 25 percent and increases the probability of hitting the target 

radar. The HTS Release 7 version will provide a precision targeting capability needed 

for accurate employment of GPS-aided munitions as well as HARM, with increased 

situational awareness and detection range.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 143

STRATEGIC CAPABILITY

contractors

Prime: Raytheon Missile 

Systems (AZ)

Specifications

Weight R6 - 90 lb.; R7 - 114 lb. maximum

Dimensions Length: 56 in.; Diameter: 8 in.

Acquisition Status

Program Status

F-16 HTS is operational at six locations (nine active duty and 

one guard squadron); all are currently equipped with HTS 

Release 6 (R6) hardware and software.

HTS R7 began fielding in September 2006 to provide current 

R6 capability until the next F-16 software update in May 

2007, which will allow full precision targeting capability.

Unit Assignment

Shaw AFB, SC; Mountain Home AFB, ID; Cannon AFB, 

NM; Misawa AB, Japan; Spangdahlem AB, Germany; and 

McEntire Air National Guard Base (ANGB), SC

Current Inventory 205 pods (includes 11 non-operational test units)

Future Upgrades

HTS Release 7 (R7) modification adds Precision Geolocation 

Targeting and dual carriage of HTS with Advanced Targeting 

Pods (SNIPER) in FY07. The initial delivery of modified HTS 

pods (to R7 configuration) were delivered in September 

2006, two months ahead of contract requirements Future 

pod and modification requirements include the following: 

Retrofit kit (modification) contracts awarded in FY05 and 

FY06 to purchase kits to modify 200 HTS R6 pods to HTS R7 

configuration. In FY06 and FY07, contracts are awarded/

planned for install of the 200 kits purchased in FY05 and 

FY06 and to buy 22 production pods, increasing the inventory of HTS R7 pods to ease Combat Air Forces availability. In 

FY07, another lot of 9 production pods is planned.

F-

16 

H

A

RM Targeting 

Syste

m (HTS) 

R6 

and R7
MISSION

144 UNITED STATES AIR FORCE

F16-TARS (Theater Airborne Reconnaissance System)

mission

Provide warfighting theaters with organic, survivable, and responsive 

penetrating tactical reconnaissance that gathers timely, high-quality 

imagery intelligence data for use by commanders in the air-land battle.

description

The F16-TARS (Theater Airborne Reconnaissance System) consists of a removable pod 

uploaded to F-16C Block 25/30/32 aircraft. TARS is the Air Force’s only high-speed, 

penetrating, under-the-weather, theater-controlled, reconnaissance capability. In 

the span of a single engagement, it provides unique rapid strike and reconnaissance 

in a high-threat environment. Per the 2004 operational requirements document and 

as requested by CENTAF, TARS must provide near-real-time imagery transmission to 

forces on the ground, allowing immediate response to threats and battle damage assessment (BDA). Continuously deployed in Iraq since May 2005, TARS has significantly 

increased imagery available in Operation Iraqi Freedom (OIF) by producing over 

6,000 images for CENTCOM in support of infantry and special operations personnel 

engaged in counter-insurgent pre-raid planning, time-sensitive targeting, BDA, and 

counter-IED support. Data link capability will begin limited fielding in FY07 
GLOBAL VIGILANCE

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STRATEGIC CAPABILITY

F

16-

TARS (

The

ater Air

borne 

R

e

connaiss

a

n

ce 

Syste

m)

contractors

Prime: BAE (NY); L-3 Communications (UT)

Specifications

Size 162 in. x 29 in. x 28.5 in.

Weight 1,200 lb.

Coverage Digital Electro-Optical Sensor

Capacity/Satellite 20 Pods - 10 Forward Framing Sensor (FFS); 10 with 

Medium Altitude Electro-Optical and FFS; 

Acquisition Status

Program Status Sustainment

Future Upgrades Datalink for near-real-time data transmission
MISSION

146 UNITED STATES AIR FORCE

F-22A Raptor

mission

Perform both air-to-air and air-to-ground missions enabling full realization of operational concepts vital to the 21st century Air Force. 

description

The F-22A Raptor is the Air Force’s newest fighter aircraft. Its combination of stealth, 

supercruise, maneuverability, and integrated avionics, coupled with improved supportability, represents an exponential leap in warfighting capabilities. The F-22A 

is a critical component of the Global Strike Task Force. It is designed to project air 

dominance rapidly at great distances and to defeat threats attempting to deny access 

to our nation’s Joint Forces. 
GLOBAL POWER

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STRATEGIC CAPABILITY

F-22A Raptor

contractors

Prime:Center Fuselage, Final 

Assembly, and overall System 

Integration - Lockheed Martin-Aero 

(GA); Mid Fuselage - Lockheed 

Martin-Aero (TX); Aft Fuselage and 

Wings - Boeing (WA); Propulsion

- Pratt & Whitney (CT)

Subcontractor(s): Radar - 

Northrop Grumman (MD)

specifications

Weight 63,634 lb.

Range 

Primary Air Superiority Mission: 260 Nautical Miles (NM) 

subsonic + 100 NM supersonic radius; Secondary Subsonic 

Long Range Air Superiority Mission: 570 NM radius

Armament 

One M61A2 20-millimeter cannon; Payload: 480 20mm 

rounds for the gun; side weapon bays can carry two AIM-9 

infrared (heat seeking) air-to-air missiles; main weapon 

bays can carry (air-to-air loadout) six AIM-120 radar-guided 

air-to-air missiles or (air-to-ground loadout) two 1,000-lb 

GBU-32 JDAMs and two AIM-120 radar-guided air-to-air 

missiles.

Dimensions Length: 62 ft., 1 in. (18.9 m); Height: 16 ft., 8 in. (5.1 m); 

Wingspan: 44 ft., 6 in. (13.6 m)

Service Ceiling Above 60,000 ft. (approximately 18 km)

Speed Mach 2 class 

Acquisition status

Program Status

Full Rate Production, 24 in production to be delivered to 

Langley through 2006; last delivery in 2011; projected 

inventory - 183

Unit Assignment

Edwards AFB, CA; Nellis AFB, NV; Tyndall AFB, FL; Langley 

AFB, VA; Holloman AFB; Hickam AFB; Future Unit Assignment: Elmendorf AFB, AK

Current Inventory 75 Aircraft (as of 17 October 2006); approximately 2 aircraft 

per month delivery rate

Future Upgrades

Integration of Small Diameter Bomb (SDB), Enhanced Airto-Ground Radar, Non-traditional Intelligence, Surveillance, 

and Reconnaissance (NTISR) capabilities
MISSION

148 UNITED STATES AIR FORCE

F-35 Lightning II Joint Strike Fighter 

mission

Provide all-weather, precision, stealthy, air-to-ground strike capability, 

including direct attack on the most lethal surface-to-air missiles 

(SAMs) and air defenses; meet the requirements of the three U.S. Services, the UK, and other allies. 

description

The F-35 Lightning II, Joint Strike Fighter (JSF) program will develop and deploy an 

affordable, fifth-generation, stealthy, multi-role strike fighter aircraft. The Conventional Takeoff and Landing (CTOL) F-35 will be used to support the Air Force core 

competencies of Air and Space Superiority, Global Attack, Precision Engagement, 

and Agile Combat Support. The F-35 will complement a force structure that includes 

fighter, bomber, and support assets operating in an environment with F-22A and 

within the projected Command, Control, Communications, Computers, Intelligence, 

Surveillance, and Reconnaissance (C4ISR) architecture. The F-35 capitalizes on system 

commonality and modularity among variants, maximizing affordability and logistical 

support for 21st century AEF employment. The service versions of the F-35 include 

the following: 

• USAF: F-35A CTOL, stealthy, multi-role aircraft (primary air-to-ground) to replace 

the F-16 and A-10 and complement the F-22A

• USMC: F-35B (Short Takeoff and Vertical Landing (STOVL)), stealthy, multi-role strike 

fighter to replace the AV-8B and F/A-18

• USN: F-35C (Carrier Version (CV)), stealthy, multi-role strike fighter to complement 

the F/A-18E/F

• UK: F-35B STOVL aircraft to replace the Sea Harrier and GR-7 
GLOBAL POWER

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STRATEGIC CAPABILITY

F-35 Lightning II

J

oint 

Strike Fighter 

contractors

Prime: Airframe - Lockheed Martin 

(TX); F135 Engine - Pratt & Whitney 

(CT); F136 Engine - General 

Electric/Rolls-Royce Fighter Engine 

Team (OH, IN) 

Subcontractors:Center Fuselage

- Northrop Grumman (CA); Aft 

Fuselage and Tails - BAE (UK); 

Lift System Components - RollsRoyce (UK, IN)

Specifications

Weight 28,900 lb.

Combat Radius Threshold: 590 NM (CTOL); 450 NM (STOVL); 600 NM (CV)

Armament 

Payload - Internal: Two AIM-120C Advanced Medium Range 

Air-to-Air Missiles (AMRAAM); Two 2,000 lb class Joint 

Direct Attack Munition (JDAM), Wind Corrected Munition 

Dispenser (WCMD), Guided Bomb Unit (GBU), Cluster Bomb 

Unit (CBU), Joint Stand-off Weapon (JSOW); Small Diameter 

Bomb; GAU-12 25mm gun; External: AIM-9X; Mk-82, 83, 

84 family of JDAM and Laser Guided Bombs; AGM-158 Joint 

Air-to-Surface Standoff Missile (JASSM)

Dimensions Wingspan: 35 ft.; Length: 51.1 ft.; Wing Area: 460 square ft.

“G” +9.0/-3.0 (CTOL); +7.0/-2.0 (STOVL); +7.5/-3.0 (CV)

Speed Level Flight - 1.5 Mach > 30,000 ft.; Design Max - 700 

KCAS/1.6 Mach

Acquisition Status

Program Status

System Development and Demonstration (SDD); Production 

begins in 2007 with deliveries in 2009 - 2028; Projected 

inventories - 1763 CTOL variants for USAF; 680 STOVL/CV 

variants for the Navy and Marine Corps

Unit Assignment Planned testing at Edwards AFB, CA; Nellis AFB, NV; Planned 

training at Eglin AFB, FL

Current Inventory 0
MISSION

150 UNITED STATES AIR FORCE

F-117 Nighthawk 

mission

Penetrate high-threat air space, using low-observable stealth 

technology, and conduct precision strikes against critical, robustly 

defended targets.

description

The F-117 Nighthawk is the world’s first operational aircraft designed to exploit 

low-observable stealth technology and use laser-guided and GPS-guided weapons 

against critical targets. The unique design of the single-seat F-117 provides exceptional combat capabilities. About the size of an F-15 Eagle, the twin-engine F-117 

aircraft is powered by two General Electric F404 turbofan engines and has quadruple 

redundant fly-by-wire flight controls. Air-refuelable, the F-117 supports worldwide 

commitments and adds to the deterrent strength of U.S. military forces. 
GLOBAL POWER

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STRATEGIC CAPABILITY

F-117 Nighth

awk 

contractors

Prime: Airframe/Contractor 

Logistics Support - Lockheed 

Martin (CA) 

Subcontractor(s):Engines - 

General Electric (MA); IRADS - 

Raytheon-Texas Instruments (TX); 

Weapon System Trainer - 

L-3 Communications (TX)

specifications

Weight 52,500 lb. (23,625 kg)

Range Unlimited with air refueling

Armament Internal weapons carriage: GBU-27; EGBU-27; Laser GBU10/12; Various cluster bomb munitions (CBUs)

Dimensions Length: 63 ft., 9 in. (19.4 m); Height: 12 ft., 9.5 in. (3.9 m); 

Wingspan: 43 ft., 4 in. (13.2 m)

Interoperability Participates as key member of integrated strike packages

Service Ceiling 35,000 ft.

Power Plant Two GE-404, non-augmented engines, each with 9,040 lb. 

of thrust

Speed Sub-sonic (0.9 Mach)

Acquisition status

Program Status Sustainment

Unit Assignment 49th Flight Wing, Holloman AFB, NM

Current Inventory 42 F-117; two YF-117
MISSION

152 UNITED STATES AIR FORCE

GBU-31/32/38 Joint Direct Attack Munition (JDAM)

mission

Provide the warfighter with accurate weapons delivery in adverse 

weather from medium to high altitudes. 

description

The GBU-31, GBU-32, and GBU-38 Joint Direct Attack Munition (JDAM) series of 

precison guided munitions consists of existing inventory general purpose bombs 

integrated with “JDAM tailkits.” The JDAM tailkit includes a new tail section and aero 

surfaces combined with a Global Positioning System aided Inertial Navigational 

System (GPS/INS) for precision all-weather delivery. JDAM can be launched from all 

altitudes in dive, toss, and loft manuvers as well as straight and level flight with an 

on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against 

single or multiple targets on a single pass. The warfighters have declared JDAM the 

“weapon of choice” after thousands of engagements in the Kosovo, Afghanistan, and 

Iraq air-to-ground campaigns. 
GLOBAL POWER

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STRATEGIC CAPABILITY

GBU-31

/32

/38

J

oint Dire

ct Attack M

u

nition (JDAM)

contractors

Prime: Boeing (MO)

Subcontractors:Tail Actuator 

System - Textron (MA); Inertial 

Measurement Unit - Honeywell 

(MN); GPS Receiver - RockwellCollins (IA); Mission Computer

- Lockheed Martin (NJ)

specifications

Weight

GBU-31 – Mk-84, BLU-109 2,000 lb. bomb series; GBU-32 

– Mk-83/BLU-110 1000 lb. bomb series ; GBU-38 – Mk-82/

BLU-111 500 lb. bomb series

Range <15 nautical miles (NM)

Dimensions GBU-31 (MK-84) 152.7 inches, (BLU-109) 148.6 inches; GBU32 (MK-83) 119.6 inches; GBU-38 (MK-82) 96.2 inches

Warhead Blast/Fragmentation: MK-82/BLU-111, MK-83/BLU-110, 

MK-84; Penetrator: BLU-109

Compatibility Operational on: B-1B, B-2A, B-52H, F-15E, F-16 Block 30, 40 

& 50, F/A-18A+/C/D/E/F, F-22A, F-117, AV-8B

Guidance Global Positioning System aided Inertial Navigation System 

(GPS/INS)

Acquisition status

Program Status Full rate production of JDAM GBU-31, GBU-32 and GBU-38 

tailkits.

Current Inventory Over 126,000 tail kits in Air Force, Navy and Marine inventory

Future Upgrades

An Integrated GPS Anti-jam System (IGAS) will be incorporated into all JDAM tailkits beginning with Lot 11 which will 

start delivery in 2 QTR FY 08
MISSION

154 UNITED STATES AIR FORCE

GBU-39/B Small Diameter Bomb (SDB) 

mission

Provide fighter and bomber aircraft with a tactically significant stand-off 

attack capability from outside of point defenses against fixed targets, 

while increasing loadout and minimizing collateral damage. 

description

The GBU-39/B Small Diameter Bomb (SDB) weapon system consists of the weapon 

(GBU-39/B), a four-place miniature munitions carriage system (BRU-61/A), mission 

planning system, accuracy support infrastructure, and logistics. The SDB is a 250 lb.- 

class weapon designed as a small autonomous, conventional, air-to-surface, nearprecision weapon that is interoperable with established/projected Command, Control, Computers, Communications, Intelligence, Surveillance, and Reconnaissance 

(C4ISR) architectures and is compatible with current and future Air Force platforms.
GLOBAL POWER

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STRATEGIC CAPABILITY

GBU-39/B Small Diameter Bomb (SDB) 

contractors

Prime: Boeing (MO)

specifications

Weight 285 lb.

Range 

>= 40 nautical miles (NM) down-range from 0.8 mach at 

40K Mean Sea Level (MSL); >= 35 NM cross-range from 0.8 

mach at 40K Mean Sea Level (MSL)

Dimensions Length: 71 in.; Width: 7.5 in.; Height: 7.8 in. 

Warhead Penetration/Blast/Fragmentation Warhead

Compatibility Aircraft: Threshold - F-15E; Objective - F-22, F-16, F-35, 

F-117, B-52, B-1, B-2, A-10, and MQ-9

Guidance Inertial Navigation System/Global Positioning System 

(INS/GPS) Guidance

Acquisition status

Program Status

Low Rate Initial Production; Full Rate Production 1QFY07; 

projected inventory - 24,000; Required Assets Available 

(RAA)on F-15E met 28 August 2006; Initial Operational 

Capability (IOC) on F-15E declared 2 October 2006.

Current Inventory 162 GBU-39/Bs, 20 BRU-61/As

Future Upgrades

Increment II to provide initial capability against moving 

targets in adverse weather. Focused Lethality Munition Joint 

Capability Technology Demonstration (JCTD) will integrate 

new warhead, potentially providing the ability to prosecute 

targets requiring minimized collateral damage (previously 

off-limits targets).
MISSION

156 UNITED STATES AIR FORCE

Global Broadcast Service (GBS)

Mission

Provide global broadcast of high-volume, high-speed information 

to deployed forces.

Description

The Global Broadcast Service (GBS) is a communications broadcast service that simultaneously broadcasts imagery, video, and data information to multiple dispersed 

users using small receive terminals. The GBS uses payloads on two DoD satellites 

plus commercial leases over the continental United States (mandatory) and Europe 

(augmentation). Three fixed primary injection points and two mobile injection points 

uplink broadcasts to satellites.
GLOBAL VIGILANCE

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STRATEGIC CAPABILITY

Gl

obal Bro

a

dcast 

Service (

G

B

S)

Contractors

Prime: Raytheon Intelligence & 

Information Systems (VA)

Subcontractors: Raytheon Technology Services (VA); Chelton Microwave (MA); GTSI (VA); Viasat (MD) 

Specifications

Size

Number existing: two military payloads augmented by 

commercial leases

Future: operations over five Wideband Global SATCOM 

(WGS) system satellites

Coverage Global Coverage: 65° N–65° S

Capacity/Satelite Maximum data rate: 24 Mbps

Acquisition Status

Program Status

Milestone II - 1QFY98; Initial Operational Capability 1 

- 1QFY04; Beyond Low-Rate Initial Production (BLRIP) 

- 2QFY07. GBS is transferring to Wideband Global SATCOM 

(WGS) satellites once available for use; transition begins 

in FY07. 
MISSION

158 UNITED STATES AIR FORCE

Global Positioning System (GPS)

mission

Provide highly accurate positioning, navigation, and timing data (globally, 24 hours a day, and in any type of weather) to an unlimited number of civil users and authorized military users. 

description

The Global Positioning System (GPS) is comprised of three segments: space segment, 

control segment, and user segment. The space segment consists of 24 or more satellites in six orbital planes, traveling in semi-synchronous (12-hour) orbits around the 

earth. The control segment, sometimes referred to as the ground segment, consists 

of a Master Control Station (MCS), a Back-Up MCS (BMCS), six dedicated monitor 

stations, five ground antennas (four dedicated and one shared), and eight National 

Geospatial-Intelligence Agency (NGA) monitor stations. The user segment includes 

the myriad of civil and military GPS receivers used for air, land, sea, and space applications. The GPS is commanded and controlled by Air Force Space Command, 2nd 

Space Operations Squadron at Schriever AFB, CO. 
GLOBAL VIGILANCE

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STRATEGIC CAPABILITY

Gl

obal Positioning 

Syste

m (

G

P

S)

contractors

Prime: Block II/IIA - Boeing (CA);

Block IIR/IIRM - Lockheed Martin 

(PA); Block IIF - Boeing (CA); 

Block III - TBD

Subcontractors: Lockheed Martin 

(PA); Harris (FL)

specifications

Size

Block II/IIA - 28 launched/17 on orbit; Block IIR - 13 

launched/12 on orbit; IIR-M - Three launched, three on orbit; 

IIF - TBD; GPS III - TBD

Weight II - 3,670 lb.; IIA - 4,150 lb.; IIR - 4,485 lb.; IIR-M - 4,525 lb.; 

IIF - 3,566 lb.; GPS III - TBD

Coverage Continuous global coverage

Acquisition status

Program Status Operational - IIRM-1 launched September 25, 2005; first IIF 

launch, FY08; first GPS III launch, FY13
MISSION

160 UNITED STATES AIR FORCE

Halvorsen (formerly Next Generation Small Loader [NGSL])

Mission

Provide “high reach” cargo off-load and up-load.

Description 

The Halvorsen loader is Air Mobility Command’s newest Material Handling Equipment 

(MHE) acquisition. It is a self-propelled, diesel-powered, air- and surface-transportable, 25,000-pound capacity, loading/off-loading vehicle. It will augment and 

ultimately replace existing 25,000-pound loaders and the remaining Wide Body 

Elevator Loaders (WBELs) through attrition, and will be part of the 463L pallet material handling system. The Halvorsen loader is C-130 deployable and able to function 

in austere operating locations. It will transport cargo (463L pallets, airdrop platforms, 

rolling stock, and containers) and interface with the full spectrum of military and 

civilian cargo aircraft. It is a Non-Developmental Item (NDI) procurement – modified 

version of the Australian Truck Aircraft Side Loading Unit (TASLU).
GLOBAL POWER

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STRATEGIC CAPABILITY

Halvorsen (

for

mer

ly 

Next 

Gener

ation Small Lo

ader [NGSL])

Contractors

Prime: FMC Technologies Inc. (FL)

Subcontractors: Deck Welding

- Johnstown Welding & Fabrication 

(PA); Engine - Detroit Diesel (MI);

Transmission - Allison Transmissions (IN); Front Axle - Dana Corporation (IN); Hydraulic Cylinders 

- Clover Hydraulics (WI)

specifications

Weight Approx 32,000 lb. (C-130 deployment limitation)

Range 3,500 nautical miles (NM)

Dimensions Transport: Length: 355 in.; Width: 109 in.; Height: 94 in. 

Operation: Length: 355 in.; Width: 170 in.; Height: 94 in.

Speed 17 mph on level surface (fully loaded)

Payload 25,000 lb. (3 pallets)

Other Specifications Deck Height: 39 in. to 18.5 ft.

Acquisition status

Program Status

Currently, production runs through Aug 07; 24 per year; 

projected inventory – 394. FY07 & FY08 GWOT Submission 

for 39 additional loaders

Unit Assignment 146 locations worldwide

Current Inventory 388

Future Upgrades

Cab cooling and auto lube on 93 loaders. These modifications already accomplished on the remainder of the fleet, to 

include loaders on the assembly line.
MISSION

162 UNITED STATES AIR FORCE

HC-130P/N King 

Mission

Provide Combat Search and Rescue (CSAR) and Personnel Recovery 

(PR); airborne command and control for search and rescue operations; 

extended visual/electronic searches; delivery of survival equipment 

over land or water; and unimproved airfield operations for survivor 

medical evacuation. 

Description 

The HC-130P/N King aircraft provides a range of Combat Search and Rescue (CSAR) 

and Personnel Recovery (PR) capabilities by increasing the range of helicopters 

through in-flight refueling, insertion of para-rescue specialists (trained in emergency 

trauma medicine, harsh environment survival, and assisted evasion) via tactical 

delivery, and airdrop of supplies and equipment to isolated personnel in permissive 

or hostile environments. The HC-130 can fly in the day against a reduced threat; 

however, crews normally fly night, low-level, air refueling and airdrop operations 

using night vision goggles. The HC-130 can fly low-level NVG tactical flight profiles to 

avoid detection. To enhance the probability of mission success and survivability near 

populated areas, crews employ tactics that include incorporating no external lighting 

or communications and avoiding radar and weapons detection.
GLOBAL POWER

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STRATEGIC CAPABILITY

HC-130P/

N King 

Contractors

Prime: Lockheed Martin (SC)

specifications

Weight 155,000 lb.

Range 3,500 nautical miles (NM)

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Service Ceiling 30,000 ft.

Self-Protection Radar and missile warning receivers, chaff and flare 

dispensers, cockpit armor

Speed 289 mph (464 km per hour) at sea level

Other Specifications

Communications: UHF/VHF/SATCOM/Secure/Anit-jam 

Navigation: Integrated INS/GPS/Dopler, digital low-power 

color radar

Acquisition status

Program Status Sustainment

Unit Assignment

Moody AFB, GA; Kirtland AFB, NM; Davis-Monthan AFB, AZ; 

Patrick AFB, FL (AFRC); Moffett FAF, CA (ANG); F.S. Gabreski 

Airport, NY (ANG); Kulis ANGB, AK (ANG)

Current Inventory 36

Future Upgrades

Integrated SATCOM, NVG compatible lighting (ARC), Forward 

Looking Infrared (FLIR) (ANG), Enhanced Traffic Alert and 

Collision Avoidance System (E-TCAS) (partial), personnel 

locator system (partial), cockpit mods under C-130 Avionics 

Modernization Program (AMP), in-flight refueling (receiver) 

capability, tactical data receivers, HC-130 Simulator
MISSION

164 UNITED STATES AIR FORCE

HH-60G Pave Hawk 

mission

Conduct day/night/marginal weather alert response missions to recover downed aircrew or other isolated personnel in hostile or permissive 

environments; perform disaster relief, noncombatant evacuation operations, counter-drug operations, civil search and rescue, and Space 

Shuttle support. 

description

The HH-60G Pave Hawk provides Combat Search and Rescue (CSAR) and Personnel 

Recovery (PR). It is the most rapidly deployable, long range, combat rescue helicopter 

in the Air Force inventory. The Pave Hawk is a highly modified version of the Army 

Black Hawk helicopter. It features an upgraded communications and navigation suite 

that includes integrated inertial navigation/global positioning/Doppler navigation 

systems, satellite communications, secure voice, and Have Quick communications. All 

HH-60Gs have an automatic flight control system, night vision goggles lighting, and 

forward looking infrared system that greatly enhances night low-level operations. 

The Pave Hawk has color weather radar and an engine/rotor blade anti-ice system 

that gives the HH-60G adverse weather capability. Pave Hawk mission equipment 

includes a retractable in-flight refueling probe, internal auxiliary fuel tanks, and 

two crew-served 7.62mm/.50cal machine guns. Pave Hawk combat enhancements 

include a radar warning receiver, infrared jammer, and a flare/chaff countermeasure 

dispensing system. HH-60G rescue equipment includes a hoist capable of lifting a 

600-lb. load (270 kilograms) from a hover height of 200 feet (60.7 meters), and a personnel locating system that is compatible with the PRC-112 survival radio. It provides 

range and bearing information to a survivor’s location. A limited number of Pave 

Hawks are equipped with an over-the-horizon tactical data receiver that is capable of 

receiving near real-time mission update information. 
GLOBAL POWER

GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 165

STRATEGIC CAPABILITY

HH-60

G Pave Hawk 

contractors

Prime: Sikorsky (CT)

specifications

Weight 22,000 lb.

Range 500 nautical miles (NM)

Armament M-240 7.62 machine gun, GAU-2C-7.62mm mini-gun, 

GAU-18 .50 caliber machine gun 

Dimensions Main Rotor: 53 ft.; Length: 64 ft.; Height: 16 ft.

Service Ceiling 14,200 ft.

Self-Protection Integrated Chaff/Flare/RWR, Infra-red (IR) Jammer, Kevlar 

armor, Self-sealing fuel tanks

Speed 125 knots

Other Specifications

Communications: UHF Line-of-Sight (LOS), VHF LOS, Secure 

UHF Satellite Communications (SATCOM)/DAMA, Personal 

Locator System (PLS), HQ-II; Navigations: Integrated INS/

GPS/Doppler Forward Looking Infrared (FLIR), over-thehorizon (OTH) Tactical Receiver, Digital Moving Map/Threat 

Display, WX Radar, and Hoist

Acquisition status

Program Status Sustainment

Unit Assignment

Moody AFB, GA; Nellis AFB, NV; Kirtland AFB, NM; Kadena 

Air Base, Japan; Naval Air Station (NAS) Keflavik, Iceland; 

Patrick AFB, FL (AFRC); Davis-Monthan AFB, AZ (AFRC, AD); 

Moffett FAF, CA (ANG); F.S. Gabreski Apt, NY (ANG); Kulis 

ANGB, AK (ANG), Hill AFB, UT (AFMC)

Current Inventory 101

Future Upgrades

Upgraded Comm/Nav/Electronic Warfare Suite, External Gun 

mount, Flare/Chaff CMDS – Self Protection System; 701C 

Engine – Improved Durability Gearbox Upgrade, Structural 

Integrity Program, Dual Engine Contingency Power, Light 

Airborne Recovery System ARS-6 Ver-12, Forward Looking 

Infrared System, Improved Night Vision Imaging System 

compatible External/Internal lighting. The next generation 

combat search and rescue replacement aircraft, CSAR-X, solves 

critical deficiencies in both numbers and capability of HH-60G.
MISSION

166 UNITED STATES AIR FORCE

Hypersonic Technology Vehicle (HTV)

MISSION

Develop advanced space vehicles to deliver and deploy a variety of 

conventional payloads worldwide. 

DESCRIPTION

Hypersonic Technology Vehicle (HTV) technology demonstrations will contribute to 

global reach capabilities by demonstrating an unpowered, maneuverable, hypersonic glide vehicle capable of carrying a 1,000-lb. payload. The HTV effort provides 

dual growth paths to the Air Force’s Prompt Global Strike (PGS) system and Defense 

Advanced Research Projects Agency’s (DARPA) hypersonic cruise vehicle. It represents an affordable, low-risk building block approach to validating key hypersonic 

technologies. HTV will demonstrate a common set of hypersonic technologies by 

flying three vehicles of progressively greater capabilities. These include step increases 

in thermal protection, precision, cross range, and communications/command and 

control capabilities.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 167

STRATEGIC CAPABILITY

H

y

personic

T

e

chno

logy Vehicle (HTV)

CONTRACTORS

Prime: Lockheed Martin (CA)

Subcontractor(s): Lockheed 

Martin (PA); Carbon Advanced 

Technologies, Inc. (TX)

specifications

Size Length: 12 ft.; Diameter: 4 ft.

Weight 2,200 lb.

Range 4,000–9,000 nautical miles (NM), depending on 

configuration

Coverage Intercontinental to global

Capacity/Satelite 1,000 lb.

Compatability

Must be compatible with GPS and the Global Information 

Grid, as well as standardized Air Force Command and Control 

and Data Dissemination Systems

Acquisition status

Program Status Demonstration Program; first demonstration launch is currently scheduled for 4QFY07
MISSION

168 UNITED STATES AIR FORCE

Joint Air-to-Surface Standoff Missile (JASSM) 

mission

Provide stand-off capability to attack critical hardened and non-hardened, fixed and re-locatable targets defended by next-generation 

defense systems. 

description

The Joint Air-to-Surface Standoff Missile (JASSM) is a conventional, air-to-surface, 

precise, autonomous, low-observable, stand-off cruise missile capable of penetrating 

enemy defenses and striking high-value, fixed, or relocatable targets. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 169

STRATEGIC CAPABILITY

J

oint Air-to-Su

rface 

S

tandoff Missile (

J

ASSM) 

contractors

Prime: Lockheed Martin (FL, AL); 

Subcontractors: Teledyne Continental Engine (OH, AL); Williams 

International (MI, UT); Fiber Innovations (MA); Klune (UT); Wyman-Gordon Forgings (TX); L-3 Communications Telemetry (PA)

specifications

Weight 2,250 lb.

Range JASSM: Greater than 200 nautical miles (NM); 

JASSM-Extended Range (ER): Greater than 500 NM

Warhead 1,000 lb. Blast-Fragmentation and Penetration Warhead

Compatability Aircraft Compatiblity: Threshold - B-52 and F-16; Objective - 

B-1, B-2, F-15, F-117, and F-35; JASSM-ER Threshold: B-1

Guidance INS/GPS and an Imagine Infrared (IIR) Terminal Seeker

Acquisition status

Program Status

Milestone (MS) I began Program Definition and Risk Reduction (PDRR) June 1996; MS II began engineering and 

manufacturing development (EMD) 1QFY99; Low rate initial 

production (LRIP) 1QFY02; MS III 4QFY04; Full rate production 1QFY05; Required Assets Available (RAA) declared on 

B-52, B-1, B-2, and F-16; Initial Operational Capability (IOC) 

on B-52 (Barksdale) and B-1 (Dyess) August 2005; on F-16 

(Hill) May 2006; on B-2 (Whiteman) September 2006

Current Inventory 455

Future Upgrades JASSM Extended Range (JASSM-ER) - FY08 deliveries; JASSM 

2-Way Weapon Data Link - FY10 deliveries
MISSION

170 UNITED STATES AIR FORCE

Joint Helmet Mounted Cueing System (JHMCS)

Mission

Provide helmet-mounted visual cueing of sensors and weapons; provide display of targeting and aircraft data; enable first-look/first-shot 

air-to-air visual range advantage, quicker ground target designation, 

and improved situational awareness. 

Description

The Joint Helmet Mounted Cueing System (JHMCS) improves both air-to-air and 

air-to-ground combat effectiveness and situational awareness by providing a visorprojected Head-Up Display (HUD) to cue weapons and sensors, and display targeting and aircraft data. In close air-to-air combat, JHMCS allows the pilot to visually 

target enemy aircraft utilizing close range weapons, especially at high off-boresight 

angles with the AIM-9X. For air-to-ground combat, JHMCS greatly reduces the time 

to designate and acquire ground targets. JHMCS improves situational awareness by 

displaying visual targeting and aircraft performance information on the helmet’s 

visor, enabling the pilot to monitor this information while looking outside the cockpit. The system uses a magnetic transmitter unit on the left side canopy rail and a 

magnetic receiver unit in the helmet to determine the pilot’s line-of-sight. The JHMCS 

Electronic Unit interfaces with the aircraft system bus to provide helmet line-of-sight 

to the mission computer and receive data for the helmet display.
GLOBAL VIGILANCE

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STRATEGIC CAPABILITY

J

oint 

H

elmet Mo

unted C

u

eing 

Syste

m (JHMC

S)

Contractors

Prime: Boeing (MO)

Subcontractor(s): Vision Systems 

International (CA); Rockwell Collins 

Display Systems (CA); Elbit Fort 

Worth (TX); Elbit Systems (Israel)

specifications

Weight Total head supported weight less than or equal to 4.3 lb.

Compatability Operational on USAF F-15C/D, F-16C/D, Navy F/A-18C/D/E/F, 

and foreign F-15, F-16, F/A-18. 

Field of View / Regard 20° / 360°

Qualified Ejection Speed 450 knots

Acquisition status

Program Status Joint Air Force/Navy Program in full rate production

Unit Assignment

Elmendorf AFB (AK), Lakenheath (UK), Mountain Home AFB 

(ID), Shaw AFB (SC), Hill AFB (UT), Spangdahlem AB (GE), 

Misawa AB (JP), McEntire ANG (SC), Missouri ANG (MO), NAS 

Lemoore (CA), NAS Oceana (VA), NAF Atsugi (JP)

Future Upgrades Preplanned Product Improvement (P3I) includes Night Vision 

capability, and an option for a flat panel display.
MISSION

172 UNITED STATES AIR FORCE

KC-10 Extender 

mission

Provide worldwide air refueling for Air Force, Navy, NATO, and allied 

aircraft, as well as strategic airlift capability; enable global mobility and 

local and global strike missions.

description

The KC-10 Extender is an aerial refueling asset built on the commercial DC-10 airframe. The aircraft creates an air bridge to enable global mobility and global strike 

missions (such as B-2 missions) and local strike missions by enabling longer sorties. 

It has 88-percent systems commonality with the DC-10, with additional systems and 

equipment necessary for its Air Force mission. These additions include military avionics; aerial refueling boom and aerial refueling hose and drogue systems; a seated 

aerial refueling operator station; and aerial refueling receptacle and satellite communications. The maximum fuel transfer rate to receiver aircraft is 1,100 gallons per 

minute for the boom system and 470 gallons per minute for the drogue system. There 

are 59 KC-10 aircraft in the USAF tanker fleet (20 aircraft with multi-point fueling 

capability). There are two active duty units at McGuire AFB, NJ, and Travis AFB, CA.
GLOBAL REACH

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STRATEGIC CAPABILITY

KC-

10 

Extender 

contractors

Prime: Airframe - Boeing (TX); 

Engines - Kelly Aviation Center 

(KAC) (TX)

Subcontractor(s): ARINC (OK)

specifications

Weight Maximum gross takeoff weight: 590,000 lb.

Dimensions Wingspan: 165.3 ft.; Height: 58 ft.; Length: 181.5 ft.

Compatibility Capable of air refueling Air Force, Navy, Marine, NATO, and 

allied Aircraft

Service Ceiling 42,000 ft.

Speed 619 mph (Mach 0.825)

Payload Max total payload 356,000 lb.

Max Cargo 170,000 lb.

Max Fuel Load 186,000–356,000 lb. (depending on cargo load)

Passenger Capacity 75

Acquisition status

Program Status Sustainment

Unit Assignment McGuire AFB, NJ, and Travis AFB, CA

Current Inventory 59

Future Upgrades Aircraft Modernization Program (AMP)
MISSION

174 UNITED STATES AIR FORCE

KC-135 Stratotanker 

mission

Provide worldwide air refueling and strategic airlift for Air Force, Navy, 

NATO, and allied aircraft; enable global mobility and local and global 

strike. 

description

The KC-135 Stratotanker creates an air bridge to enable global mobility and global 

strike missions (such as B-2 missions) and local strike missions by enabling longer 

sorties. It is built on a similar airframe to the 707 passenger aircraft. The KC-135 

completed an engine upgrade in June 2005 to put F-108 engines (CFM-56 commercial engines) on the 417 KC-135R model aircraft. It is equipped with military avionics, 

an aerial refueling boom, a prone aerial refueling operator station, and satellite 

communications. There are currently 530 KC-135 E/D/R/T models in the inventory at 

35 bases, 29 states, and two overseas bases: Kadena Air Base (AB), Japan, and RAF 

Mildenhall, UK. Twenty-nine KC-135 E model aircraft will be retired in FY07 as approved in the FY07 National Defense Authorization Act (NDAA). Twenty aircraft are 

capable of multi-point refueling using hose and drogue refueling. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 175

STRATEGIC CAPABILITY

KC-135

Str

atotanker 

contractors

Prime:Engineering - Boeing (KS); 

Depot Maintenance - Boeing (TX);

GATM - Rockwell Collins (TX)

Subcontractor(s): Depot Maintenance - PEMCO (AL); CFM-56/F108 

R model engines - General Electric 

(OK); TF-33 E-model engines

- Pratt & Whitney (OK)

specifications

Range With fuel offload of 150,000 lb. throughout flight: 1,500 

nautical miles (NM)

Dimensions Wingspan: 130.9 ft.; Height: 41.7 ft.; Length: 128.9 ft.

Compatibility Capable of air refueling Air Force, Navy, Marine, NATO, and 

allied aircraft

Service Ceiling 50,000 ft.

Speed 530 mph at 30,000 ft.

Payload Max total payload: 200,000 lb.

Max Cargo Load 83,000 lb.

Max Fuel Load 117,000–200,000 lb.

Passenger Capacity 54

Acquisition status

Program Status Sustainment

Unit Assignment

Air Force Reserve (AFRES): Andrews AFB, MD; Beale AFB, CA; 

March AFB, CA; Grissom, IN; Selfridge, MI; Seymour Johnson 

AFB, NC; Tinker AFB, OK.

Air National Guard (ANG): Bangor, ME; Birmingham, AL; 

Eielson AFB, AK; Fairchild AFB, WA; Forbes Field, KS; Hickam 

AFB, HI; Lincoln, NE; March AFB, CA; McConnell AFB, KS; 

McGhee Tyson, TN; McGuire AFB, NJ; Meridian Key Field, MS; 

Gen Mitchell, WI; Niagara, NY; Pease, NH; Pittsburgh, PA; 

Rickenbacker, OH; Salt Lake City, UT; Scott AFB, IL; Sioux City, 

IA; Sky Harbor Phoenix, AZ.

Active: Fairchild AFB, WA; Grand Forks AFB, ND; MacDill 

AFB, FL; McConnell AFB, KS; Robins AFB, GA; Altus AFB, OK; 

Edwards AFB, CA 

Current Inventory 530

Future Upgrades Control Column Actuated Brake, Global Air Traffic Management (GATM)
MISSION

176 UNITED STATES AIR FORCE

Launch & Test Range System (LTRS) 

Mission

Perform command, control, and communications functions while ensuring public safety in support of national (DoD, civil, and commercial) 

space launches, ballistic missile and missile defense tests, and aeronautical flight tests; and provide sensors to support the space surveillance mission.

Description 

The Launch & Test Range System (LTRS) is a key enabler for all Air Force, DoD, and 

National Aeronautics and Space Administration (NASA) capabilities that employ or 

depend on space-based or ballistic missile systems. It provides responsive, reliable, 

and cost-effective launch scheduling, communications, metric tracking, telemetry, 

flight safety, and emergency termination to an average of 30 DoD, civil, and commercial space launches and ballistic missile tests per year. Both launch and test ranges 

are national assets, which as two of the 26 members of the Major Range and Test 

Facility Base are sized, operated, and maintained primarily for DoD Test and Evaluation missions but also may be available to all users that have a valid requirement for 

their capabilities. It also supports guided weapons and aeronautical tests and space 

surveillance missions. The LTRS consists of the Eastern Range at Patrick AFB/Cape 

Canaveral AFS, the Western Range at Vandenberg AFB, and downrange sites and 

assets associated with both. The ranges include 16 command transmitters, 17 tracking radars, and 14 telemetry antennas, as well as a multitude of associated suites of 

equipment. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 177

STRATEGIC CAPABILITY

Contractors

Prime:Lockheed Martin (CA); ITT 

Industries (FL); InDyne, Inc (CA); 

Computer Sciences/Raytheon (FL)

Subcontractors: L-3 Communications 

(CA); KSS (Kelly’s Logistics Support 

Services) Scitor (CA); SRI International 

(CA); Hughes Space (CO); Boeing (FL); 

Contraves (PA); TRAK Microwave (FL); 

RT Logic (CO); ADC (MN); ENSCO (FL);

Net Acquire (WA); Freescale Semiconductor Inc (CO); Dolphin (NY); ASR (CA); Excel (CA); 

Superior (NY); CDI Corp (CA); Volt (CA); Lockheed Martin Tactical Aircraft Systems (CA); 

Lockheed Martin Technical Operations (CA); Alcatel (TX); DCS Corp (CA); Robinson & 

Robinson (FL); Smith Electric (CA); ITT Industries (FL)

specifications

Coverage

Provides trajectory coverage for current and forecasted 

launches: 

ER: Launch trajectories from 34° to 112° 

WR: Launch trajectories from 153.6° to 281°

Supports launches with 24 hours between close of first 

launch window and opening of second launch window

Interoperability Interoperable with NASA and commercial launch systems

Acquisition status

Program Status Undergoing modernization and recapitalization while 

operational

Unit Assignment 30th Space Wing – Western Range; 45th Space Wing 

– Eastern Range

Current Inventory Two operational ranges

Future Upgrades Modernization of radar, telemetry, and command destruct 

instrumentation

Lau

n

ch & 

Test Range 

Syste

m (LTRS) 
MISSION

178 UNITED STATES AIR FORCE

LGM-30G Minuteman III

mission

Provide strategic deterrence for the nation through an intercontinental 

ballistic missile system with prompt global strike capabilities.

description

The LGM-30G Minuteman III is a highly survivable, silo-based, inertially guided 

nuclear missile of intercontinental range on alert since 1970. Using a rapid targeting 

and execution system and penetration aids, each Minuteman III can effectively 

deliver up to three independently targetable reentry vehicles into denied areas 

against fixed and fleeting targets.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 179

STRATEGIC CAPABILITY

L

GM-

3

0

G Min

uteman III

contractors

Prime: Northrop Grumman Mission 

Systems (UT)

Subcontractor(s): Lockheed 

Martin (PA); Boeing (OH); Alliant 

Techsystems (UT); Raytheon (MA); 

Honeywell (FL); Aerojet (UT)

specifications

Weight 79,432 lb.

Range 6,000 miles plus

Armament One to three MK12/12A reentry vehicles (RVs)

Dimensions Length: 59.9 ft.; Diameter: 5.5 ft.

Warhead W62/W78

Coverage Global

Speed Approximately 15,000 mph at burnout

Acquisition status

Program Status Fielded, undergoing life extension programs

Unit Assigment 500 MMIII missiles deployed at Malmstrom AFB (MT); Minot 

AFB (ND), and FE Warren AFB (WY)
MISSION

180 UNITED STATES AIR FORCE

MC-130E Combat Talon 

Mission

Provide global, day/night, and adverse weather airdrop, air/land, 

infiltration, and exfiltration of personnel and equipment. 

Description

The MC-130E Combat Talon supports U.S. and allied special operations forces with 

infiltration and exfiltration missions. It also plays a deep-penetrating, helicopter 

refueling role during special operations missions.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 181

STRATEGIC CAPABILITY

MC-13

0

E Combat Talon 

Contractors

Prime: Airframe - Lockheed 

Martin (SC); Integrated Weapon 

System Support - Boeing (FL); 

Radar - Raytheon (TX); General 

Avionics - L-3 Communications (GA, 

TX); Communications/Navigation 

- Rockwell Collins (IA) 

Specifications

Weight 155,000 lb. (gross weight)

Range 2,700 nautical miles (NM); unlimited with in-flight refueling

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Acquisition Status

Program Status Modifications only

Unit Assignment Duke Field, NC

Current Inventory 10
MISSION

182 UNITED STATES AIR FORCE

MC-130H Combat Talon II

Mission

Provide global, day/night, and adverse weather airdrop, air/land, infiltration, and exfiltration of personnel and equipment in support of U.S. 

and allied special operations forces. 

Decsription

The MC-130H Combat Talon II conducts covert penetration of politically sensitive/

hostile airspace to insert, resupply, and extract special operations forces and equipment and to aerially refuel helicopters for extended operations. These missions are 

conducted in adverse weather and at night at low level and long range.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 183

STRATEGIC CAPABILITY

MC-13

0

H Combat Talon II

Contractors

Prime: Airframe - Lockheed Martin 

(SC); Integrated Weapon System 

Support - Boeing (FL); Radar - SEI 

(MO); General Avionics - L-3 

Communication (GA, TX); 

Communication/Navigation

- Rockwell Collins (IA)

Specifications

Weight 155,000 lb. (gross weight)

Range 2,700 nautical miles (NM); unlimited with in-flight refueling

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Acquisition Status

Program Status Twelve interim MC-130W configured aircraft being procured

Unit Assignment Hurlburt Field, FL; Kirtland AFB, NM; Midenhall AFB, UK; 

Kadena AFB, Japan

Current Inventory 20

Future Upgrades Multiple modifications 
MISSION

184 UNITED STATES AIR FORCE

MC-130P Combat Shadow 

mission

Fly clandestine or low-visibility, low-level missions into politically 

sensitive or hostile territory to provide air refueling for special operations helicopters. 

description

The MC-130P primarily flies its single- or multi-ship missions at night to reduce 

detection and intercept by airborne threats. Secondary capabilities include airdrop of 

small special operations teams, small bundles, and Zodiac and combat rubber raiding 

craft as well as night-vision goggle take-offs and landings.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 185

STRATEGIC CAPABILITY

MC-130P Combat 

S

h

adow 

contractors

Prime: Airframe - Lockheed Martin 

(SC); Integrated Weapon System 

Support - Boeing (FL); Communications/Navigation - Rockwell 

Collins (IA)

Specifications

Weight 155,000 lb. (gross weight)

Range

2,700 nautical miles (NM) without internal Benson Tanks; 

4,000+ NM with internal Benson Tanks; unlimited with InFlight Refueling (Benson Tanks are fuel tanks placed in the 

cargo area to hold additional fuel normally used for Helicopter Air Refueling—fuel can be used by the MC-130P)

Dimensions Wingspan: 132 ft.; Length: 99 ft.; Height: 38 ft.

Acquisition Status

Program Status Modifications only

Unit Assignment Hurlburt Field, FL; Kirtland AFB, NM; Midenhall AFB, UK; 

Kadena AFB, Japan

Current Inventory 23

Future Upgrades Multiple modifications 
MISSION

186 UNITED STATES AIR FORCE

Medium Launch Vehicle (MLV) 

mission

Provide continuing, highly reliable launch of medium-weight national 

security satellites into low-earth, polar, geosynchronous transfer, and 

stational orbits.

description

The Delta II Medium Launch Vehicle (MLV) launches GPS Block IIR Replenishment 

satellites. The MLV utilizes multiple configurations and is capable of launching a 

6,098 kg payload, or satellite, into a 185 km Low Earth Orbit (LEO), or a 2,171 kg 

payload into Geosynchronous Transfer Orbit (GTO). GTO orbits are required to loft 

satellites from lower LEO orbits to higher Geosynchronous Earth Orbits (GEO), which 

allow satellites to rotate with the earth and remain positioned over one region of 

the earth’s surface. Reliability of the Delta II Medium Launch Vehicle (MLV) is over 98 

percent, with 122 (out of 124) successful launches since 1989.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 187

STRATEGIC CAPABILITY

Medium Lau

n

ch Vehicle (MLV) 

contractors

Prime: United Launch Alliance (CO, 

AL, FL, CA, TX)

Subcontractor(s): Alliant (UT);

Rocketdyne (CA); Aerojet (CA)

Pratt & Whitney (FL); 

Honeywell (FL); Thiokol (UT)

specifications

Size Length: 125 ft. (38.1 m); Diameter: 10 ft. (3.05 m)

Weight Mass at liftoff: 512,267 lb. (231,900 kg)

Range 6,098 kg payload to LEO - 185 km orbit at 28.5 degrees;

2,171 kg payload to GTO - apogee of 35,786 km

Capacity/Satellite Pounds to orbit range: 2,050–12,450; Will vary depending 

on orbit and vehicle configuration

Interoperability

Launches from both Cape Canaveral Air Force Station 

(CCAFS) and Vandenberg AFB, cooperating with NASA and 

commercial launch services

Compatibility Satisfies all payload integration requirements

acquisition status

Program Status MLVIII (Delta II) Active
MISSION

188 UNITED STATES AIR FORCE

MH-53J/M Pave Low III/IV 

mission

Provide low-level, long-range, undetected penetration into denied 

areas—day or night, in adverse weather—for infiltration, exfiltration, 

and resupply of special operations forces. 

description

MH-53J/M Pave Low III/IV missions are almost always conducted under cover of 

darkness and frequently under adverse weather conditions requiring extended flight 

operations as low as 50 feet using night vision goggles or Instrument Meteorological 

Conditions as low as 100 feet above ground level. Missions involve deep penetrations 

of hostile areas at extreme ranges without escort. The MH-53J/M employs a sophisticated avionics system to enhance crew situational awareness and avoid threats.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 189

STRATEGIC CAPABILITY

M

H-53J/M Pave Low III

/IV 

contractors

Prime: Airframe- Sikorsky (CT); 

Engine/Gear Box - Lockheed Martin 

(GA); Radar/Forward Looking 

Infrared (FLIR) - Raytheon (TX); 

General Mods - EJM (FL); MTC (GA)

specifications

Weight 46,000 lb. (gross weight)

Range 600 nautical miles (NM); unlimited with helicopter air 

refueling

Armament Two 7.62 mm Mini-Guns; one .50 Caliber Machine Gun

Dimensions Length: 88 ft.; Height: 25 ft.; Roto Diameter: 72 ft. 

acquisition status

Program Status Modifications only

Additional Information

Drawdown begins in 2009
MISSION

190 UNITED STATES AIR FORCE

Military Satellite Communication (MILSATCOM) Terminals 

Mission

Develop, procure, deploy, and sustain multi-band satellelite communications (SATCOM) terminals used by Air and Space Expeditionary 

Forces (AEF), the Single Integrated Operations Plan (SIOP), combatant 

commanders, and other users to communicate over current and emerging transformational military and commercial satellite systems.

Description

Military Satellite Communications (MILSATCOM) Terminals provide the president, 

combatant commanders, and warfighters in the field with secure, worldwide communications capability. Terminals provide the user segment of the MILSATCOM space 

system. MILSATCOM Terminals addressed by this warfighting system are the Ground 

Multi-band Terminal (GMT), Family of Advanced Beyond Line of Sight Terminals (FABT), High Data Rate Radio Frequency (HDR-RF), Airborne Integrated Terminal (AIT), 

Secure Mobile Anti-Jam Reliable Tactical Terminal (SMART-T), Multi-Band Multi-Mode 

Radio (MBMMR), Global Broadcast System (GBS) Receive Terminals, and Defense 

Satellite Communication System (DSCS) Terminals.
GLOBAL VIGILANCE

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STRATEGIC CAPABILITY

Mili

tary Satellite Commu

nication (MIL

S

AT

C

OM) 

Termi

nals 

Contractors

Prime: Boeing (CA); Raytheon (MA, 

FL, IN, VA); Rockwell (IA); BAE (NH); 

Lockheed Martin (CA); Northrop 

Grumman (CA)

Subcontractor(s): Harris (FL); L-3 

Communications (UT); ViaSat (CA)

specifications

Coverage Global

Capacity/Satellite

Terminals operate with current systems such as MILSTAR, 

UHF Follow-On (UFO) satellites, and the Defense Satellite 

Communications System (DSCS), as well as commercial 

systems, and will operate with future systems such as Advanced Extremely High Frequency (AEHF), Wideband Global 

SATCOM (WGS), Transformational Satellites (TSAT), and the 

Mobile User Objective System (MUOS)

Interoperability Interoperable with joint and allied SATCOM terminals per 

military and commercial standards

Compatibility Compatible with satellites and user input/output devices per 

military and commercial standards 

acquisition status

Program Status Terminals are in various stages of development, production, 

fielding, and sustainment
192 UNITED STATES AIR FORCE

MISSION MISSION

Military Strategic and Tactical Relay (Milstar) 

Mission

Provide secure, jam-resistant, worldwide satellite communications to 

meet essential wartime requirements for high-priority military users. 

Description

Milstar is a joint-service, multi-satellite constellation that links command authorities 

with a wide variety of resources, including ships, submarines, aircraft, and ground 

stations. Each Milstar satellite serves as a smart switchboard in space by directing 

traffic from terminal to terminal anywhere on the earth. Since the satellite actually processes the communications signal and can link with other Milstar satellites 

through crosslinks, the requirement for ground-controlled switching is significantly 

reduced. The satellite establishes, maintains, reconfigures, and disassembles required 

communications circuits as directed by the users. Milstar terminals provide encrypted 

voice, data, teletype, or facsimile communications. A key goal of Milstar is to provide 

interoperable communications among the users of Army, Navy, and Air Force Milstar 

terminals.

The Milstar system is composed of three segments: space (the satellites), terminal 

(the users), and mission control. Air Force Space Command’s Space and Missile 

Systems Center at Los Angeles Air Force Base, CA, is responsible for development 

and acquisition of the Milstar space and mission control segments. The Electronics 

Systems Center at Hanscom AFB, MA, is responsible for the Air Force portion of the 

terminal segment development and acquisition. The 4th Space Operations Squadron at Schriever AFB, CO, is the front-line organization providing real-time satellite 

platform control and communications payload management.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 193

Mili

tary 

Str

ategic

and Tac

tical

R

elay (Milstar) 

Contractors

Prime: Lockheed Martin Missiles 

and Space (Global)

Specifications

Weight Approx. 10,262 lb.

Range Orbit altitude: 22,250 nautical miles (NM) (geosynchronous 

orbit)

Coverage 65° N to 65° S 

Capacity/Satelite Five satellite (primary) constellation in geosynchronous 

orbit

Launch Vehicle Titan IVB/Centaur upper stage

Acquisition Status

Program Status Complete

Unit Assignment 4 SOPS

Current Inventory 5 satellites

Future Upgrades None
MISSION

194 UNITED STATES AIR FORCE

Mission Planning Systems (MPS)

Mission

Enable warfighters to plan missions from training to combat, including 

weapon delivery and airdrops. The plan is developed alone or in collaboration with planners for other elements of the mission, depending 

on the specifics of the mission. It ultimately provides the printed or 

electronic materials needed for the executing platform to accomplish 

the assigned mission. 

Description

Mission Planning Systems (MPS) use data such as maps, imagery, weather, and 

platform performance, and works within the mission planning system to develop 

a specific action plan. MPS provide automated mission-planning tools and support 

for fixed and rotary wing aircraft and guided munitions. The program consists of 

common hardware and software components required by every platform, as well as 

individual platform-specific hardware and software components. It creates a flight 

plan based on threats, targets, terrain, weather, aircraft performance capability, 

and configuration. MPS must allow the warfighter to plan deliveries, calculate fuel 

requirements, and assess routes based on known enemy threat location and type. 

It also optimizes and de-conflicts flight routes with other aircraft, and writes this 

information to a Data Transfer Device (DTD) for uploading into the required aircraft. 
GLOBAL POWER

GLOBAL REACH GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 195

STRATEGIC CAPABILITY

Mission Planning 

Syste

ms (MP

S)

Contractors

Prime: Lockheed Martin Missiles 

and Space (Global)

Specifications

Interoperability

Complies with Army, Air Force, Navy and Special Operations Forces Information Exchange Requirements (IERs). In 

accordance with CJCSI 6212.01D, MPS meets the network 

ready key performance parameter

Acquisition Status

Program Status

Program consists of five increments: Increment I - Concept 

Exploration; Increment II - Production & Development 

with a Full Deployment Decision Review scheduled for 

2nd Quarter 2007; Increment III - System Development & 

Demonstration with a Milestone C planned for 1st quarter 

2008; Increments IV and V are Pre-Milestone B development activities with Milestone Bs scheduled for 2nd quarter 

2007 and 4th quarter 2008 respectively

Unit Assignment 951 Electronic Systems Group, Hanscom AFB, MA

Future Upgrades To be determined
MISSION

196 UNITED STATES AIR FORCE

MQ-1 Predator

Mission

Provide dedicated support to ground troops by directly down-linking 

real-time full motion video to units equipped with Remotely Operated 

Video Enhanced Receiver (ROVER) terminals. Predator’s primary mission is long-dwell reconnaissance and target acquisition in support of 

the Joint Forces commander. 

Description

The MQ-1 Predator is an Unmanned Aircraft System (UAS) that delivers persistent 

Intelligence, Surveillance, and Reconnaissance (ISR) with day/night full-motion 

video (EO/IR), laser target designation/illumination, and direct-strike capabilities 

using Hellfire laser-guided missiles. The MQ-1 Predator is a medium-altitude, longendurance remotely piloted aircraft, and has the capability to directly attack critical, 

perishable targets.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 197

STRATEGIC CAPABILITY

M

Q-1 Pred

ator

Contractors

Prime: General Atomics - Aeronautical Systems Incorporated (CA)

Subcontractor(s): L-3 

Communications (UT); Raytheon (TX)

Specifications

Size Wingspan: 55 ft.; Length: 28 ft.

Weight Maximum takeoff weight: 2,500 lb.

Range 400 nautical miles (NM) (with 16 hours on station)

Armament Two AGM-114 Hellfire laser-guided missiles

Warhead Blast/Fragmentation or anti-armor

Coverage

Varies by sensor. Full motion video coverage—electrooptical, infrared, and low-light video cameras; All are Line 

of Sight (LOS)

Capacity/Satellite

Sensor Data: Beyond Line of Sight (BLOS) SATCOM and Line 

of Sight (LOS) to ROVER customers. Future datalink improvements will provide more robust LOS Tactical Common 

Datalink (TCDL) to ROVER III and ground stations and a more 

robust BLOS datalink.

Interoperability

Sensor data currently provided via proprietary data links. 

Full Motion Video uses proprietary Motion JPEG format for 

BLOS and standard H.261 for ROVER. Future data link improvements will provide FMV via standard MPEG-2 format 

with NGA-standard Key Length Value (KLV) metadata over 

standard TCDL data links. Data sent to ROVER is used by 

forces on ground in direct contact with the enemy.

Compatability Sensor data is compatible with Predator ground stations 

and ROVER receivers

Acquisition Status

Program Status Full rate production

Unit Assignment 11th Reconnaissance Squadron; 15th Reconnaissance 

Squadron; 17th Reconnaissance Squadron

Current Inventory 88
MISSION

198 UNITED STATES AIR FORCE

MQ-9 Reaper 

Mission

Provide persistent and immediate precision direct-strike capability. 

In its “Hunter-Killer” role, MQ-9 Reaper automatically finds, fixes and 

tracks high value targets enabling combatant commanders to rapidly 

prosecute critical emerging Time Sensitive Targets (TSTs) without having to wait for other strike aircraft.

Description 

The MQ-9 Reaper will influence the battle space by providing continuous coverage 

of the area of interest, independent of time of day or weather obscuration, with the 

ability to detect, identify, attack and destroy critical emerging targets (both moving 

and stationary) from endurance altitude within the defined area. The MQ-9 provides 

persistent full-motion video directly to decision makers and warfighters in direct 

contact with the enemy. The MQ-9 can conduct direct strikes using Guided Bomb Unit 

(GBU)-12 laser-guided 500-lb. bombs, GBU-38 Joint Direct Attack Munitions (JDAM), 

laser target designation/illumination, and AGM-114 Hellfire missiles. MQ-9 also provides persistent Intelligence, Surveillance and Reconnaissance (ISR) with day/night 

full-motion video (EO/IR) and a synthetic aperture radar with Ground Moving Target 

Indicator (GMTI).
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 199

STRATEGIC CAPABILITY

M

Q-9

R

eaper 

Contractors

Prime: General Atomics - Aeronautical Systems Incorporated (CA)

Subcontractor(s): L-3 

Communications (UT); Raytheon (TX)

specifications

Size Wingspan: 64 ft.; Length: 36 ft. 

Weight Maximum takeoff weight: 10,000 lb.

Range 1,000 nautical miles (NM) (with 16 hours on station)

Armament Up to 3,000 lb. of GBU-12 laser-guided 500-lb. bombs 

and/or GBU-38 JDAMs; AGM-114s

Coverage

Varies by sensor. Full motion video coverage—electro-optical, infrared and low-light video cameras; Synthetic aperture 

radar coverage—strip map that parallels and is offset from 

aircraft flight path; All are Line of Sight (LOS)

Capacity/Satellite

Sensor Data: Beyond Line of Sight (BLOS) SATCOM and Line 

of Sight (LOS) to ROVER customers; Future datalink improvements will provide more robust LOS Tactical Common 

Datalink (TCDL) to ROVER III and ground stations and a more 

robust BLOS datalink.

Interoperability

Sensor data currently provided via proprietary data links. 

Full Motion Video uses proprietary Motion JPEG format 

for BLOS and standard H.261 for ROVER. Future datalink 

improvements will provide FMV via standard MPEG-2 format 

with NGA-standard Key Length Value (KLV) metadata over 

standard TCDL datalinks. Data is sent to ROVER used by 

forces on ground in direct contact with the enemy

Compatability Sensor data compatible with Predator ground stations and 

ROVER receivers

acquisition status

Program Status System Development and Demonstration (SDD)

Unit Assignment 42nd Attack Squadron (2nd Qtr FY07)

Current Inventory 8
MISSION

200 UNITED STATES AIR FORCE

National Polar-orbiting Operational Environmental

Satellite System (NPOESS) 

Mission

Provide military commanders and civilian leaders with assured, timely, 

high-quality global weather and environmental information to effectively employ weapon systems and protect national resources. 

Description

The National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

is a tri-agency program (DoD, Department of Commerce, and NASA) that will be the 

nation’s primary source of global weather and environmental data for operational 

military and civil use for at least 10 years. NPOESS will fly a suite of instruments 

that will provide visible and infrared cloud-cover imagery and other atmospheric, 

oceanographic, terrestrial, and space environmental information. In all, NPOESS will 

measure environmental parameters such as soil moisture, cloud levels, sea ice, ozone, 

and more.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 201

STRATEGIC CAPABILITY

National Polar-orbi

ting Oper

ational

E

nviron

mental Satellite 

Syste

m (

N

POESS) 

Contractors

Prime: Northrop Grumman Space 

Technology (CA)

Subcontractor(s): Raytheon (CA); 

Ball Aerospace (CO); Instruments

- ITT Industries (IN)

specifications

Size Four-satellite constellation

Weight 14,498 lb. (max)

Coverage 

Global; Low Earth Polar Sun synchronous orbit-two-orbit 

planes with four-hour revisit capability (with reliance on 

the European Meteorological Operational (MetOp) satellite 

in third orbit)

acquisition status

Program Status Engineering and Manufacturing Development (EMD)
MISSION

202 UNITED STATES AIR FORCE

Operationally Responsive Space (ORS)

Mission

Provide assured space power focused on the urgent needs of the Joint 

Forces Commander.

Description

Operationally Responsive Space (ORS) will provide an affordable capability to 

promptly, accurately, and decisively position and operate national and military assets 

in and through space. ORS will be fully integrated and interoperable with current and 

future architectures, and provide space services and critical capabilities to warfighters 

and other users. ORS is a vision for transforming future space operations, integrations 

and acquisition, all at a lower cost.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 203

STRATEGIC CAPABILITY

Oper

ationally 

Res

ponsive Space (ORS)

Contractors

Prime: The Air Force Research Laboratory (NM); U.S. Naval Research 

Laboratory (DC); Air Launch (WA); 

Orbital Sciences Corporation (AZ); 

Space-X (CA)

Subcontractor(s): Delta Velocity 

Corporation (VA); HMX (NV); Honeywell (MD); Jackson & Tull (NM); 

Johns Hopkins APL (MD);

L3 Communications (UT); Orion Propulsion (AL); Praxis (VA); Raytheon (CA); SEAKR 

(CO); Space Vector Corporation (CA); Swales Aerospace (MD); Universal Space Lines 

LLC (CA)

specifications

Range Capable of inserting assigned payloads into orbit

Capacity/Satellite

Goal of Small Launch Vehicle (SLV): 1,000 lb. to 100 

nautical miles (NM), 28.5° orbit; TacSat-1 (Air Force supporting launch ops and range ops): 300 lb. small satellite 

for low resolution tactical imaging and Radio Frequency 

(RF) emitter identification via Secure Internet Protocol 

Router Network (SIPRNet) tasking/exploitation. TacSat-2 

(AF funded): 800 lb. small satellite for higher resolution 

tactical imaging and RF emitter identification via SIPRNET 

tasking/exploitation. TacSat-3 (AF funded): 800 lb. small 

satellite for HyperSpectral imaging and navy ocean buoy 

data collection/communications. TacSat-4 (AF providing 

launch): 836 lb. (planned) small satellite for data exfiltration/collection, Blue Force Situational Awareness (BFSA) 

and communications on the move for underserved users

Interoperability

Launch from both Cape Canaveral Air Force Station (CCAFS) 

and Vandenberg Air Force Base (VAFB), cooperating with 

NASA and commercial launch services

Compatibility Satisfies all payload integration requirements

acquisition status

Program Status System Development & Demonstration (SDD)
MISSION

204 UNITED STATES AIR FORCE

Polar Military Satellite Communications (MILSATCOM)

Mission

Provides secure, survivable communications connectivity required to 

support peacetime, contingency, and wartime operations in the polar 

region.

Description

Polar Military Satellite Communications (MILSATCOM) provides critical tactical users 

24-hour/day coverage with two properly phased satellites and assured, low probability of detection satellite communications in the North polar region.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 205

STRATEGIC CAPABILITY

Polar Mili

tary Satellite Commu

nications (MIL

S

AT

C

OM)

Contractors

Classified

specifications

Size

Interim Polar: Three payload packages hosted on classified 

satellites; Enhanced Polar: Two payload packages hosted on 

classified satellites

Coverage Northern latitudes above 65° N

Capacity/Satellite Interim Polar: Milstar LDR data rates; Enhanced Polar: 

Advanced Extremely High Frequency (AEHF) XDR Format

Compatibility

Interim: Polar package compatible with Low Data Rate 

(LDR) terminals; Enhanced: Polar package compatible with 

Extended Data Rate (XDR) terminals

acquisition status

Program Status All milestones are classified
MISSION

206 UNITED STATES AIR FORCE

RC-26B

Mission

Provide the Air National Guard with a highly mobile aircraft Intelligence, 

Surveillance, and Reconnaissance (ISR) platform for use in counterdrug and counter-narcoterrorism operations, as well as other mission 

support areas.

Description

The RC-26B is a highly mobile ISR platform for use in counter-drug and counter 

narco-terrorism operations. It also provides mission support for SOUTHCOM, NORTHCOM, the Department of Homeland Security, and the United States Secret Service 

supporting national special security events, crisis/disaster response, maritime patrol, 

homeland defense, and the Global War on Terrorism. The RC-26B features a small 

logistics footprint that can rapidly deploy in support of counter-drug and contingency 

operations. The system consists of an ElectroOptical Forward Looking Infrared Radar 

(FLIR) camera for video recording, two still cameras (digital and wet film), a robust 

communication package for first responder, civil, and military communications, and a 

Line of Sight Streaming video transmitter. The aircraft is operated by two pilots and a 

missions system operator. Typically there is a law enforcement official or other agency 

representative on the aircraft to direct the operation and ensure mission requirements are met.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 207

STRATEGIC CAPABILITY

RC-

26B

Contractor

Prime: ATK Mission Research

Integrated Systems (TX); Contract 

maintenance - M7 Aerospace (TX)

specifications

Weight 16,500 lb. gross weight

Range Range: 1,200 nautical miles (NM) ; Service Ceiling: 25,000 

ft.; Top Speed: 250 kN.

Dimensions Wingspan: 57 ft.; Length: 59.35 ft.; Height: 16.66 ft.

Acquisition status

Program Status Operational

Unit Assignment NY, WV, FL, AL, MS, WI, TX, NM, AZ, CA, WA Air National 

Guard units

Current Inventory 11

Future Upgrades

High Definition ElectroOptical Forward Looking Infrared 

Radar (FLIR) and Beyond Line of Sight (BLOS) video transmitters
MISSION

208 UNITED STATES AIR FORCE

RC-135S Cobra Ball

Mission

Collect Measurement and Signature (MASINT) intelligence for the scientific and technical assessment of foreign ballistic missiles and treaty 

verification. 

Description

The RC-135S Cobra Ball is a self-contained Measurement and Signature (MASINT) 

intelligence collection platform that provides scientific and technical assessments of 

foreign ballistic missiles and treaty verification. Cobra Ball’s specialized crew employs 

sensitive telescopic monitoring devices, advanced optics, and infrared sensors to 

provide national and theater command authorities with intercontinental ballistic 

missile treaty verification data and Theater Air Defense warning.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 209

STRATEGIC CAPABILITY

RC-135S Co

b

r

a Ball

Contractors

Prime: Major Subsystems - L-3 

Communications (TX); Textron 

(OH, TX) 

Subcontractor(s): Propulsion 

- General Electric (OH); Airframe 

-Boeing (KS)

specifications

Weight 322,500 lb. maximum take-off gross weight;

160,000 lb. aircraft basic weight

Range 5,000+ miles unrefueled; inflight refueling capable

Dimensions Length: 140 ft.; Wingspan: 131 ft.; Height: 42 ft.

Speed 500 mph

Duration 8–10 hours unrefueled, limited only by aircrew duty 

requirements if aerial refueled

acquisition status

Program Status Modification and Sustainment

Unit Assignment 55th Wing, Offutt AFB, NE

Current Inventory Three mission aircraft plus one flight deck trainer aircraft

Future Upgrades Baseline 2 delivers FY07; Baseline 3 FY07; Baseline 3 delivers 

FY08; Baseline 4 delivers FY11
MISSION

210 UNITED STATES AIR FORCE

RC-135U Combat Sent 

Mission

Collect information used in the development of advanced weapon 

systems and dynamic reprogramming of radar warning gear. 

Description

The RC-135U Combat Sent is a scientific and technical Signals Intelligence (SIGINT) 

collector of information used in the development of advanced weapon systems and 

the dynamic reprogramming of radar warning gear. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 211

STRATEGIC CAPABILITY

RC-135U Combat 

Sent 

Contractors

Prime: Major Subsystems - L-3 

Communications (TX);

Sierra Nevada Corporation (NV) 

Subcontractor(s): Propulsion 

- General Electric (OH); Airframe 

- Boeing (KS)

specifications

Weight 322,500 lb. maximum gross take-off weight;

165,000 lb. aircraft basic weight

Range 5,000+ miles unrefueled; inflight refueling capable

Dimensions Length: 136 ft.; Wingspan: 131 ft.; Height: 42 ft.

Speed 500 mph

Duration 8–10 hours unrefueled, limited only by aircrew duty 

requirements if aerial refueled

acquisition status

Program Status Modification and Sustainment

Unit Assignment 55th Wing, Offut AFB, NB

Current Inventory Two mission aircraft

Future Upgrades Baseline 3 delivers FY07; Baseline 4 delivers FY10
MISSION

212 UNITED STATES AIR FORCE

RC-135V/W Rivet Joint 

Mission

Provide direct tactical Signals Intelligence (SIGINT) support to theater/

component commanders. 

Description

RC-135V/W Rivet Joint is the DoD’s premier manned airborne SIGINT platform. It is 

a self-contained collection, processing, analysis, and dissemination system. Rivet 

Joint rapidly fields tactical SIGINT capabilities to support the full spectrum of combat 

operations and national information needs. Rivet Joint flies over 700 airborne reconnaissance missions each year. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 213

STRATEGIC CAPABILITY

RC-135V/W Rivet 

J

oint 

Contractors

Prime:Major Subsystems 

- L-3 Communications (TX); 

Subcontractor(s): Propulsion 

- General Electric (OH); Airframe

- Boeing (KS)

specifications

Weight 322,500 lb. maximum take-off gross weight; 

170,000 lb. aircraft basic weight

Range 5,000+ miles unrefueled; inflight refueling capable

Dimensions Length: 140 ft.; Wingspan: 131 ft.; Height: 42 ft.

Speed 500 mph

Duration 8–10 hours unrefueled, limited only by aircrew duty 

requirements if aerial refueled

acquisition status

Program Status Modification and Sustainment

Unit Assignment 55th Wing, Offutt AFB, NE

Current Inventory 17 mission aircraft plus two flight deck trainer aircraft

Future Upgrade Baseline 9 delivers FY09; Baseline 10 delivers FY11
MISSION

214 UNITED STATES AIR FORCE

Regional Sector Air Operations Center (RSAOC)

mission

Provide North American Aerospace Defense Command (NORAD) and Pacific Command (PACOM) with a viable, interoperable, open architecture 

Command and Control (C2) node to support their mission of Air Sovereignty and Air Defense. This C2 node will also support NORTHCOM’s 

Homeland Defense (HLD) and Homeland Security (HLS). 

description

RSAOC–also known as the Battle Control System-Fixed (BCS-F) program–which 

supports Operation NOBLE EAGLE, will provide a next-generation battle management 

command and control system with enhanced capability to integrate data from existing and future civil and military defense surveillance systems into a comprehensive 

recognized air picture. This multi-input integrated air control picture will enhance the 

North American Aerospace Defense/Combatant Commander’s (NORAD/CC’s) capability to conduct peacetime air sovereignty, transition, and conventional warfare in the 

event of aggression toward the North American continent. BCS-F systems serve as 

the Air Force’s Homeland Defense battle management, command, and control hubs 

and integrate data from radar sensors, data links and supporting communications 

architecture. They provide the tactical communications and data link capabilities with 

other military and civil systems responsible for conducting the planning, directing, 

coordinating, and controlling forces for air surveillance, air defense, and control of 

sovereign U.S. air space (including the National Capital Region). The BCS-F system is a 

bi-national cooperative program with Canada, ensuring air defense and surveillance 

capability for the entire North American continent.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 215

STRATEGIC CAPABILITY

Regional

S

e

ctor Air Oper

ations Center (RS

A

OC)

contractors

Prime: Thales Raytheon (CA)

Subcontractor(s): Mitre Corp (MA)

specifications

Size Different configurations of office and computer equipment 

(depending on Sector) 

Acquisition status

Program Status Spiral 2 IOC declared by ACC Commander on

October 31, 2006. Spiral 3 is post Milestone B

Future Upgrades

Future spirals include Human-Machine Interface upgrades, 

Remote Workstation capability, security upgrades, integration of additional radars, and enhanced interfaces/integration with the National Capital Region.
216 UNITED STATES AIR FORCE

MISSION MISSION

Rocket Systems Launch Program (RSLP)

Mission

Maintain active control and management of Air Force excess ballistic 

missile assets and provide cost-reimbursable orbital and sub-orbital 

launch services for government agencies using refurbished missile 

motors.

Description 

The Rocket Systems Launch Program (RSLP) stores deactivated Intercontinental Ballistic Missile (ICBM) motors, both Minuteman II and Peacekeepers. It performs aging 

surveillance on stored motors, provides cost-reimbursable launch services including 

payload integration, refurbishment, and transport of motors and boosters. The program provides launch operations via the Orbital/Sub-orbital contract (Minotaur I, II, III, 

IV); the Sounding Rocket contract; or the Responsive Small Spacelift contract (Falcon 1, 

Raptor 1 and Raptor 2). Refurbishment of motors saves government customers ~ $30 

million/year versus the cost of new motors and avoids ~$370 million in missile motor 

destruction costs. The RSLP is designated as a single DoD agency providing launch 

vehicle support for DoD and other government agency RDT&E launches on a cost-reimbursable basis. It has provided launch support for 650 launches since 1962.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 217

R

o

cket 

Syste

ms Lau

n

ch Program (RSLP)

Contractors

Prime: Aerojet (CA); ATK Aerospace 

(UT); Space-X (CA); Orbital Sciences 

(AZ); Coleman Research (FL); 

Lockheed Martin (CO); Space 

Vector (CA)

specifications

Capacity/Satellite

Minotaur I: 1,280 lb. to Low Earth Orbit (LEO); Minotaur IV: 

3,800 lb. to LEO; Falcon 1: 1,075 lb. to LEO; Raptor 1: 1,115 

lb. to LEO; Raptor 2,559 lb. to LEO (expected performance, 

have not launched yet)

Acquisition status

Program Status

Two orbital launches aboard Minotaur I launch vehicles in 

FY05 (Space Test Program (STP)-R1 in 4QFY05; XSS-11 in 

3QFY05); Supporting MDA’s intercept tests by providing 

targets; total of eight launches and four static firings in FY05 

successfully supported Army, Navy, Air Force, and Missile 

Defense Agency missions; transferred Peacekeeper program 

responsibility from ICBM System Program Office (SPO) to 

RSLP on October 1, 2005
MISSION

218 UNITED STATES AIR FORCE

RQ-4A/B Global Hawk 

Mission

Provide persistent, near-real-time intelligence from high-altitude to 

support operations across the spectrum of conflict. 

Description

The RQ-4A/B Global Hawk unmanned aerial weapon system consists of aircraft, 

sensors, ground stations, data links, and trained personnel. It combines high-altitude, 

long endurance, and beyond-line-of-sight (BLOS) communications to provide responsive, persistent intelligence support where needed, throughout the world . The RQ-4 

provides critical information to U.S. and allied decision makers in all weather, day or 

night, throughout all phases of conflict, including peacetime indications and warnings, low-intensity conflict, and large-scale hostilities. The RQ-4 is being developed 

and fielded in capability blocks. Block 10 is currently operational and carries imagery 

intelligence

(IMINT) sensors. Block 20 will employ a larger aircraft with increased payload capacity and improved IMINT. Block 30 will retain the improved IMINT sensors and integrate 

signals intelligence (SIGINT) sensors to achieve simultaneous, multi-INT coverage. 

Block 40 will comprise a separate set of aircraft employing an advanced radar sensor 

to provide improved IMINT and surface/air moving target information in support of 

both battle management and intelligence needs. The RQ-4 is an unmanned, singleengine aircraft. Crews fly the aircraft and control missions from ground stations made 

up of a Launch/Recovery Element (LRE) and a Mission Control Element (MCE). Takeoff 

and landing is controlled from an LRE at the RQ-4 airfield, using line-of-sight (LOS) or 

BLOS communications. During missions, aircraft and sensor control are accomplished 

from an MCE using BLOS links. MCEs may be located in CONUS (normal reachback 

operations) or at any appropriate location that affords the requisite communications 

connectivity. As it is collected, RQ-4 sensor data is transmitted BLOS through the 

MCE to appropriate locations for analysis and dissemination, and may be simultaneously transmitted directly to locations within aircraft LOS. RQ-4 reachback capability 

enables reduced forward footprint and enhanced crew safety while retaining full 

mission effectiveness. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 219

STRATEGIC CAPABILITY

RQ-4A/B Gl

obal Hawk 

Contractors

Prime: Northrop Grumman (CA); 

Raytheon (CA); Raytheon (VA); L-3 

Communications (UT); Vought (TX); 

Rolls Royce (IN); Aurora (WV)

Subcontractor(s): Ground Stations - Raytheon (VA); Propulsion

- Rolls-Royce (IN); TailStructure

- Aurora Flight Systems (WV); Wing

- Vought Aircraft (TX);

Aircraft Sub-assembly - Northrop-Grumman (MS); Sensors - Raytheon (CA); 

Data links - L-3 Communications (UT)

specifications

Size Block 10 - 26,750 lb. takeoff gross weight, Blocks 20, 30 & 40 

- 32,250 lb takeoff gross weight 

Range Block 10 – 9,500 nm; Blocks 20, 30, & 40 – 8,700 nm

Dimensions

Block 10 - Length: 44 ft.; Wingspan: 116 ft.; Height: 14 ft.; 

Blocks 20, 30, and 40 – Length: 48 ft.; Wingspan: 131 ft.; 

Height: 15 ft.

Coverage

Wide area coverage due to high altitude and long endurance. 

Sensor capability varies by block. Block 10 – EO/IR and SAR, 

Block 20 – Enhanced EO/IR and SAR, Block 30 – Simultane- ous enhanced EO/IR and SAR, and SIGINT, Block 40 – MP-RTIP 

radar only, for improved IMINT and Surface/Air MTI

Interoperability

RQ-4 uses commercial Ku BLOS or X-band LOS data links for 

combined C2 and sensor data, with INMARSAT and UHF data 

links as back-up. It is interoperable through the MCE with 

Distributed Common Ground Station (DCGS) nodes, including 

compatible Army, Navy and Marine Corps surface terminals. 

Compatibility

Sensor data can be sent through satellite for BLOS link to 

MCE and relayed to DCGS nodes, and via LOS link directly to 

theater users. IMINT data can be injected by DCGS onto the 

wide area network (WAN) or other appropriate network sites.

Speed Block 10 - 340 knots; Blocks 20, 30 and 40 – 310 knots

Payload

Block 10 - 2,000 lb.; IMINT; Block 20 – 3,000 lb.; enhanced 

IMINT; Block 30 – 3,000 lb.; enhanced IMINT plus SIGINTBlock 

40 – 3,000 lb.; MP-RTIP

Other Specifications Altitude - 60,000 ft; Endurance - 28 hours

Acquisition status

Program Status Low Rate Inititial Production 

Unit Assignment 12th Reconnaissance Squadron

Current Inventory 7 Block 10 aircraft and 2 ground stations

Future Upgrades

Block 20 - Larger aircraft with enhanced IMINT (EO/IR) sen- sors and greater payload capacity; Block 30 - Simultaneous 

IMINT and SIGINT (ASIP) sensors; Block 40 - Single sensor 

(MP-RTIP) for improved imagery and surface/air moving 

target indications
MISSION

220 UNITED STATES AIR FORCE

Space Based Infrared System High (SBIRS High) 

Mission

The Space Based Infrared System’s (SBIRS) primary mission is to 

provide initial warning of a ballistic missile attack on the United States, 

its deployed forces, and allies. 

Description

The Space Based Infrared System High (SBIRS High) is an infrared detecting satellite 

system that is the follow-on to the current Defense Support Program (DSP) missile 

warning satellites. SBIRS consolidates the national and DoD’s infrared detection 

systems into a single overarching architecture that fulfills the nation’s security 

needs in the areas of missile warning, missile defense, technical intelligence, 

and battlespace characterization. SBIRS consists of three Geosynchronous Earth 

Orbit (GEO) satellites, two Highly Elliptical Orbit (HEO) payloads, a Mission Control 

Station and Backup, Relay Ground Stations in Europe and the Pacific, and nine mobile 

multi-mission processors. SBIRS enables continuous global surveillance, tracking, and 

targeting of multiple objects in multiple areas of responsibility, and surveillance of 

infrared sources of operational, intelligence, and national significance. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 221

STRATEGIC CAPABILITY

Space B

ased In

f

r

ared 

Syste

m High (

S

BIRS High) 

Contractors

Prime: Lockheed Martin Space 

Systems (CA) 

Subcontractor(s):

Northrop Grumman Electronic 

Systems (CA) ; Lockheed Martin 

Integrated Systems and Solutions 

(CO)

specifications

Weight 10,229 lb. (GEO)

Coverage Continuous global coverage

Interoperability

Interoperable with Cheyenne Mountain Operations Center 

and other strategic users via the Survivable Communications 

Integrated System, with theater missile warning networks 

via the Integrated Broadcast System in Link 16 format, with 

ballistic missile defense BMC3 (Battle Management Command, Control and Communications), and with the Space 

Battle Management Core System

Acquisition status

Program Status

SBIRS High is in System Development and Demonstration. 

Increment 1 ground segments at the Mission Control Station 

and Interim MCS Backup are operational and process and 

disseminate current DSP data. The Highly Elliptical Orbit 

(HEO) - 1 payload is on-orbit and currently conducting 

nominal operations. HEO-2 payload has been delivered to 

classified host for integration. GEO satellites 1 and 2 have 

over 90 percent of their components delivered and are in 

various stages of assembly, integration, and testing. Relay 

Ground Station-Europe was outfitted with all mission and 

communications equipment in 2005. The Mission Control 

Station Backup-HEO at Schreiver AFB, CO, is in equipment 

fit-up and check out. 
MISSION

222 UNITED STATES AIR FORCE

Space Radar (SR)

Mission 

Provide worldwide, unobtrusive, deep-look, all-weather, day-and-night 

surveillance and reconnaissance capabilities required by both national 

intelligence analysts and by joint warfighters. 

Description

Space Radar will be a modern multifunction Active Electronically Steered Array (AESA) 

radar system that can survey areas of interest anywhere in the world without putting 

aircrews and assets in harm’s way. It will operate with precision providing national 

and military decision makers the most current information about our adversaries’ 

intent. Space Radar’s unique intelligence capabilities and products will reduce enemy 

sanctuary through routine access and observation of vast, deep, denied and terrainmasked areas. It will help to discover and characterize objects, beginning a chain of 

custody, then cue aircraft and other spacecraft sensors to keep custody of fleeting targets during peacetime and war. This unprecedented surveillance capability will allow 

Combatant Commanders to dynamically task the system and fix forces across entire 

theaters of operation several times per hour. Homeland security and civil applications 

are also inherent to the capabilities of this continuously deployed system. 
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 223

STRATEGIC CAPABILITY

Space Ra

d

ar (SR)

Contractors

Prime: Lockheed Martin (CO, AZ, 

PA, MD, CA, MN, VA); Northrop 

Grumman Space Technology (NGST) 

(CA, CT, FL, MD) 

Subcontractor(s): Honeywell (AZ);

Spectrum Astro (AZ); Boeing (CA); 

Raytheon (CA); SAIC (CA); BAE 

Systems (CA); Cisco (CA); Tecolote 

(CA); Integrated Data Systems (CA); 

Ball Aerospace (CO); Partners in Air and Space (CO); SEAKR (CO); Moog (CO); Harris 

Corp. (FL); Northrop Grumman Electronic Systems (MD); Swales (MD); Adcole (MA); 

General Dynamics (MI & VA); Eagle Pitcher (MO); Sheldahl (MN); Minco (MN); MEI 

(TX); Stennis (MS); Design Develop (NM); Integrity Applications Incorporated (VA); 

SRS Technologies (VA); Booz Allen Hamilton (VA); Diligent (VA)

specifications

Weight

Range

Dimensions

Exact surveillance capabilities and numbers of spacecraft are 

subject to technical and trade space considerations that are 

being evaluated as part of the ongoing competitive concept 

development phase.

Payload Active Electronically Steered Array Radar Sensor

Coverage Global

Interoperability Interoperable with Distributed Common Ground Stations and 

National Systems infrastructure

Compatibility Fully network-centric capable

Products

Synthetic Aperture Radar Imagery (SAR); Surface Moving Target Indication (SMTI); Open Ocean Surveillance (OOS); High 

Resolution Terrain Information (HRTI) (3-D Maps) ; Advanced 

Geospatial Information (AGI)

Acquisition status

Program Status Acquisition Phase A (Study Phase), Concept and Architecture 

Development

Additional Information

The Secretary of Defense and the Director of Central Intelligence signed a 2005 

agreement committing to Space Radar as the single space radar capability for the 

nation. The Space Radar Integrated Program Office is located in Chantilly, VA, and 

reports directly to the Under Secretary of the Air Force. The Integrated Program Office 

includes members from Army, Navy, Air Force, the National Geospatial Agency (NGA), 

the Office of the Director of National Intelligence (ODNI), and the National Reconnaissance Office (NRO) with significant support from Electronic Systems Center (MA), 

MITRE Corporation (MA), Air Force Research Laboratory (NY & NM), MIT Lincoln Labs 

(MA), Army Space and Missile Defence Command (AL), and Carnegie Mellon Software 

Engineering Institute (PA).
MISSION

224 UNITED STATES AIR FORCE

Space Situation Awareness (SSA) Systems

mission

Develop, integrate, and disseminate knowledge of all ongoing activities 

related to space operations, including Intelligence, Surveillance, Reconnaissance (ISR), and environmental monitoring activities.

description

Space Situation Awareness (SSA) is provided via a worldwide network of 

electro-optical and radar sensor systems with associated Command and Control (C2), 

data processing, and analysis capabilities. SSA provides data on space events and 

activities, including space object locations/breakups/decaying orbits, satellite attack 

warnings, overhead threat warnings, space treaty monitoring, and object identification/mission payload assessment of foreign satellites. SSA systems can find, fix, track, 

and characterize space objects. Data is gathered, integrated, and disseminated to 

aid C2 for space and other missions. Ongoing efforts are sustaining today’s sensors; 

upgrading selected sensors for greater capability and longevity (Eglin radar; Haystack 

radar); developing new sensors (Space Based Space Surveillance system, or SBSS; 

Space Fence); and improving data integration and dissemination for comprehensive, 

multi-source SSA (the SSA Initiatives).
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 225

STRATEGIC CAPABILITY

Space Si

tuation Awareness (SSA) 

Syste

m

s

contractors

Prime: Eglin Upgrade - ITT 

Industries (CO); Haystack 

Upgrade - MIT Lincoln Laboratory 

(MA); SBSS - Northrop Grumman 

(CA); Space Fence - Contractor TBD; 

SSA Initiatives - Various contractors

Subcontractor(s):SBSS- Boeing 

(CA); Ball Aerospace (CO) 

specifications

Size Characteristics vary per sensor

Dimensions Characteristics vary per sensor

Coverage Worldwide surveillance of near earth and deep space orbits; 

Individual sensor coverage areas vary

Acquisition status

Program Status

Development underway for Eglin Radar Life Extension, 

Haystack radar upgrade, Space-Based Space Surveillance 

(SBSS) optical satellites, Space Fence ground radar, and SSA 

Command and Control (C2)/integration initiatives

Unit Assignment

Various space control squadrons and detachments of the 

21st Space Operations Group in Florida, New Mexico, Hawaii, 

and Virginia. Also located in Spain, and Diego Garcia

Current Inventory

Eight dedicated, eight collateral, and 13 contributing 

sensors. Dedicated assets provide full-time support to the 

SSA mission; collateral sensors provide data for SSA as a 

secondary mission, and contributing assets are operated 

by non-U.S. Strategic Command organizations, but provide 

data under contract

Future Upgrades To be determined
226 UNITED STATES AIR FORCE

MISSION MISSION

Space Test Program (STP) 

Mission

Facilitate the advancement of space systems technology—ultimately 

enabling space superiority by developing new space capabilities. 

Description

The Space Test Program (STP) is DoD’s primary program for spaceflight testing. 

As executive agent, the Air Force provides priority-based, fly before-buy spaceflight 

testing opportunities for research and development (R&D) experiments and technology demonstrations from the entire DoD space research community (e.g., Air Force, 

Navy, Army, Missile Defense Agency, National Reconnaissance Office, and others). 

The types of experiments supported range from basic research to advanced development. The STP acts as the primary interface between NASA’s Human Spaceflight 

programs (including the Space Shuttle and International Space Station) and the DoD. 

It performs risk reduction through direct flight test of prototype components and is 

responsible for all auxiliary payload flight opportunities on Air Force launch vehicles. 

STP flight tests new space system technologies and improves operational spacecraft 

design by characterizing the space environment, event, or sensor physics proposed 

for a operational system/system upgrade.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 227

Space 

Test Program (STP) 

Contractors

Prime: Communication/Navigation Outage Forecasting System 

(C/NOFS) - Spectrum Astro (AZ); 

STP-1 - AeroAstro (VA); STP-1 - Boeing (FL) ; SIV Contractor - 

Ball Aerospace (CO)

Subcontractor(s): Shuttle 

Integrator - Muniz Engineering (TX) 

Specifications

Size Efforts support multiple experiments ranging from 3 to 

4,393,710 cubic in.

Weight Efforts support multiple experiments ranging from 0.33 to 

9,193 lb.

Range Efforts support multiple experiments ranging from 48.6 NM 

to 19,438 NM

Dimensions Efforts support multiple experiments ranging from 3 to 

4,393,710 cubic in.

Coverage Dependent upon specific experiment

Capacity/Satellite Dependent upon specific experiment

Interoperability Dependent upon specific experiment

Compatibility

Dependent upon specific experiment with emphasis on 

improving operational spacecraft design by characterizing 

the space environment, event, or sensor physics proposed 

for an operational system/system upgrade and provides 

early operational capabilities to evaluate usefulness or 

quickly react to new developments

Acquisition status

Program Status

Nine successful missions in the last year including CloudSat, 

a NASA weather experiment. STP is providing on-orbit 

operations for the mission. STP-1: STP mission utilizing the 

first Evolved Expendable Launch Vehicle (EELV) Secondary 

Payload Adapter (ESPA) on an EELV Medium (Atlas V), which 

will launch six satellites from 11 experimental programs 

including DARPA’s Orbital Express which will demonstrate 

autonomous satellite servicing including on-orbit refueling. 

Scheduled to launch in early 2007. The Standard Interface 

Vehicle Contract was awarded in FY06. C/NOFS mission on 

Pegasus: Forecast ionospheric scintillations that degrade 

communication, navigation, and surveillance systems. 

Launch scheduled for 2QFY08.
228 UNITED STATES AIR FORCE

MISSION MISSION

T-1A Jayhawk 

Mission

Provide advanced-phase Specialized Undergraduate Pilot Training 

(SUPT) for students selected to fly airlift or tanker aircraft. 

Description

The T-1A Jayhawk is a medium-range, twin-engine jet trainer used in the advanced 

phase of SUPT. It is also used to support navigator training for the U.S. Air Force, Navy, 

Marine Corps, and international military services. It features cockpit seating for an 

instructor and two students and is powered by twin turbofan engines capable of an 

operating speed of Mach .78.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 229

T-1A Jayh

awk 

Contractors

Prime: Raytheon (KS)

Specifications

Weight 16,100 lb.

Range 2,222 nautical miles (NM) 

Dimensions Length: 48 ft. 5 in.; Height: 13 ft. 11 in.; Wingspan: 43 ft. 6 in. 

Acquisition status

Program Status Sustainment

Unit Assignment Laughlin AFB, TX; Randolph AFB, TX; Vance AFB, OK; 

Columbus AFB, MS
230 UNITED STATES AIR FORCE

MISSION MISSION

T-6A Texan II

Mission

Train entry-level pilots in the fundamentals of flight.

Description 

The T-6A Texan II is the Joint Primary Aircraft Training System (JPATS) aircraft. It 

replaces the USAF T-37B and the USN T-34C. The JPATS improves training, enhances 

safety, and offers increased aircrew accommodation. It also includes a Ground-Based 

Training System (GBTS) that includes Aircrew Training Devices (ATD), a Computer 

Based Training System (CBTS), courseware, and a Training Integration Management 

System (TIMS).
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 231

Contractors

Prime: Raytheon (KS) 

Subcontractor(s): Engine - Pratt 

& Whitney Canada (WV); Escape 

System - Martin Baker Aircraft/

Middlesex (UK); Avionics - Honeywell Aerospace Electronic Systems/ 

Olathe (KS), Smiths Aerospace 

Electronic Systems/Cheltenham 

(UK); Ground-Based Training 

System (GBTS) - Flight Safety 

Services Corp. (CO)

Specifications

Weight 6,500 lb.

Range 800+ nautical miles (NM) 

Dimensions Wingspan: 33.4 ft.; Length: 33.3 ft.; Height 10.6 ft.

Interoperability Joint US Air Force/US Navy (USAF/USN) primary trainer 

aircraft

Compatibility Joint USAF/USN primary trainer aircraft

Service Ceiling Maximum Operating Altitude - 31,000 ft. 

Speed 320 mph

Acquisition status

Program Status

Full Rate Production (Fielding and Sustainment); for FY07, 

acquire 48 USAF and 21 USN aircraft; continue GroundBased Training System (GBTS) acquisition; production 

planned through FY08 (USAF) and FY13 (USN); Projected 

Inventory: 779 total (451 USAF and 328 USN)

Unit Assignment Laughlin AFB, TX; Randolph AFB, TX; Vance AFB, OK; 

Columbus AFB, MS; Sheppard AFB, TX; Moody AFB, GA

 Future Upgrades Numerous minor enhancements; Traffic Alert and Collision 

Avoidance System (TCAS) upgrade

T-6A 

Tex

an II
232 UNITED STATES AIR FORCE

MISSION MISSION

T-37B Tweet 

Mission

Provide the primary phase—Phase II—of Specialized Undergraduate 

Pilot Training to fill Air Force requirements for new pilots.

Description

The T-37B Tweet is a twin-engine jet used for training joint specialized undergraduate 

pilot students in the fundamentals of aircraft handling and instrument, formation, 

and night flying. The T-37B has been used since the 1950s to train Air Force pilots. 

Since the mid-1990s, the Air Force has gradually been procuring the T-6A Texan II 

as a follow-on aircraft to replace the aging T-37. All T-37s will be retired by the 

end of FY08.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 233

T-37B 

Tweet 

Contractors

Prime:Cessna (KS)

Specifications

Weight 6,625 lb.

Range 460 nautical miles (NM) 

Dimensions Length: 29 ft. 3 in.; Height: 9 ft. 2 in.; Wingspan: 33 ft. 8 in.

Acquisition status

Program Status All T-37s will be retired by the end of FY08

Unit Assignment Randolph AFB, TX; Vance AFB, OK; Columbus AFB, MS; 

Sheppard AFB, TX

Current Inventory Active Force, 419; Air National Guard (ANG), 0; Reserve, 0
234 UNITED STATES AIR FORCE

MISSION MISSION

T-38A/AT-38B/T-38C Talon 

Mission

Provide specialized pilot training, meeting pilot requirements 

of fighter/bomber crews.

Description

The T-38A Talon is a twin-engine, high-altitude, supersonic jet trainer used in a 

variety of training roles, including Phase III of Specialized Undergraduate Pilot Training (SUPT) and Introduction to Fighter Fundamentals (IFF). The T-38 is also used as 

a companion trainer for some Air Combat Command aircraft such as the U-2, B-2, 

and F-117. Several T-38s are used as part of the Air Force Test Pilot School program. 

The T-38A has swept wings, a streamlined fuselage, and tricycle landing gear with 

a steerable nose wheel. The T-38B has a gun sight and practice bomb dispenser. The 

T-38C incorporates a “glass cockpit” with integrated avionics displays, head-up display 

and an electronic “no drop bomb” scoring system. 
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 235

T-38A/AT-38B/

T-38C Talon 

Contractors

Prime: Airframe - Northrop 

Grumman (CA); Avionics - Boeing 

(MO); Engines - GE (MA); Escape 

System - Martin Baker Aircraft/

Middlesex (UK)

Specifications

Weight 12,093 lb.

Range 1,093 nautical miles (NM) 

Dimensions Length: 46 ft., 4 in.; Height: 12 ft., 10 in.; Wingspan: 25 ft.,

3 in.

Acquisition status

Program Status

By the end of FY07, all Air Education and Training Command T-38s will be upgraded to T-38C status, which installs 

a “glass” cockpit and Global Positioning System. Current 

service life for the T-38C is projected to 2020. The T-38A 

and AT-38B are both going through the Avionics Upgrade 

Program (AUP) to be converted to the T-38C. 

Unit Assignment Randolph AFB, TX; Vance AFB, TX; Sheppard AFB,TX; 

Laughlin AFB,TX; Moody AFB, GA; Columbus AFB, MS
236 UNITED STATES AIR FORCE

MISSION MISSION

T-43A 

Mission

Provide navigator training for Air Force personnel.

Description

The T-43A is the Air Force’s primary navigation trainer and provides the pipeline for 

new navigators. Graduates are awarded the rating of basic navigator. The T-43A crew 

consists of the flight crew, 12 student navigators, and six instructors. The T-43A will 

be retired by FY10 and replaced with consolidated navigator training at Pensacola 

NAS, FL, in accordance with Base Realignment and Closure (BRAC) requirements.
Strategic Capability AGILE COMBAT SUPPORT

THE AIR FORCE HANDBOOK 2007 237

T-43A 

Contractors

Prime: Boeing (WA)

Specifications

Weight 115,000 lb.

Range 2,995 nautical miles (NM) 

Dimensions Length: 100 ft.; Height: 37 ft.; Wingspan: 93 ft.

Acquisition status

Program Status Sustainment

Unit Assignment Randolph AFB, TX
MISSION

238 UNITED STATES AIR FORCE

Tactical Air Control Party (TACP) 

and Air Support Operations Center (ASOC)

Mission

Advise ground commanders regarding the capabilities and limitations 

of air power and assist the ground commander in planning, requesting, 

and coordinating close air support (CAS.) 

Description

The TACP is a subordinate operational component of the theater air control system 

designed to provide air liaison to land forces and for the control of aircraft (JP 3-09.3). 

The TACP is usually co-located with the senior Army operational command post from 

corps through battalion level and below, if jointly validated. It can also support other 

organizations (e.g., special operations, coalition forces and police) and other missions 

requiring long-haul communications or procedural airspace control (e.g., humanitarian). The TACP provides advice and assistance in planning for the employment of air 

and space power assets including, but not limited to: CAS; air interdiction; and Intelligence, Surveillance and Reconnaissance (ISR). TACPs prepare and submit immediate 

air support requests to the ASOC using the Joint Air Request Net. It conducts detailed 

target planning and transmits a mission briefing to aircraft upon check-in. The TACP 

provides terminal attack control during attack execution and forwards battle damage 

assessment to C2 organizations.

The ASOC is the principle command and control node for integrating air and space 

power into counterland operations. A direct subordinate element of the air operations 

center (AOC), the ASOC is responsible for the direction and control of air operations 

directly supporting the ground combat element. Normally co-located with the senior 

Army tactical echelon, ASOCs coordinate operations with their permanently aligned 

TACP, Army Fire Support Cell (FSC), and AOC. The ASOC may also support units from 

other organizations (e.g., coalition forces), or augment other missions requiring 

procedural airspace control (e.g., humanitarian efforts). The ASOC executes the air 

tasking order in accordance with the ground commander’s priorities, provides procedural control of CAS aircraft operating inside the fire support coordination line (FSCL), 

obtains clearance of fires from the FSC, and integrates, coordinates and synchronizes 

other air and space operations occurring inside the FSCL.
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 239

STRATEGIC CAPABILITY

Tac

tical Air Contro

l Party (

TACP) 

and Air Support Oper

ations Center (ASOC)

Contractors

Prime:To be determined

Specifications

Size

Total Force: Officers - 428, Enlisted - 2,381; Active Duty only: 

Officers - 261, Enlisted - 1,637. Total Force increasing by 201 

officer and 361 enlisted to support Army Transformation FY 

08-11.

Acquisition status

Program Status To be determined

Unit Assignment Worldwide
MISSION

240 UNITED STATES AIR FORCE

Theater Battle Management Control Systems (TBMCS)

Mission

Provide the Joint Forces Air Component Commander (JFACC) the means 

to plan, direct, and control all theater air operations during peacetime, 

exercise, and wartime environments. 

Description

Theater Battle Management Control Systems (TBMCS) is the Combat Air Force 

information and decision support system supporting combined and joint air 

operations for the Joint Forces Air Component Commander (JFACC). 

TBMCS Force Level (FL) refers to the Headquarters elements of an operating 

command, Numbered Air Force, Unified Command or Joint Task Force, to create 

and execute a battle plan conducted at an Air and Space Operations Center-Weapon 

System (AOC WS). TBMCS is the Joint System of Record for exchanging/facilitating 

air battle planning and intelligence operations and executions with participating 

services and allies.

TBMCS Unit Level (UL) refers to the wings and squadrons that take direction from FL 

to carry out the battle plan. TBMCS UL Operations (OPS) and UL Intel are both wing 

level command and control (C2) systems. UL OPS is used to control and monitor unit 

level operations during wartime, contingencies, and exercises. UL Intel is used to 

analyze the taskings specified in the Air Tasking Order (ATO) and maintain base-level 

real-time intelligence support to the AOC, as well as the targeting and mission 

planning communities.
GLOBAL REACH GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 241

STRATEGIC CAPABILITY

The

ater B

att

le M

a

n

age

ment Contro

l

Syste

ms (

TBMC

S)

Contractors

Prime: Lockheed Martin Integrated 

Systems & Solutions (CO)

Specifications

Interoperability

TBMCS is an integrated command and control (C2) system 

which provides standardized, secure, automated decision 

support for Air Force, Joint, and Allied commanders worldwide. 

The system is specifically designed to interface with C2 systems 

from the US Army, Navy, Marines, and selected Allied/Coalition 

Nations. TBMCS provides automated air operations planning, execution management and intelligence capabilities. It 

supports a full range of functions including: Air Tasking Order 

(ATO)/Airspace Control Order (ACO) production and re-planning; 

threat assessment; target selection; mission execution; battle 

damage assessment; resource management; time critical 

target identification and prosecution; and defensive planning. 

It also supports interaction with subordinate/command units 

for mission execution. It provides a capability to obtain resource 

information, and to plan and execute the next day’s missions. 

TBMCS has in-garrison and deployable configurations.

Acquisition status

Program Status ACAT IAC; Fielding FL Sp 1.1.3, UL Ops Sp 8.5N, UL Intel 

Sp 10.0

Future Upgrades

Force Level – Spiral 1.1.4: Integration with collaboration 

tools; Consolidated database for planning/execution; Reduction of decision support process cycle times; Decision quality 

information; Automate capability to support integrated

air and space effects-based dynamic strategy development 

and assessment; Net ready compliance; Unit Level Ops 

– Spiral 8.5N, 9: Unit to Force interoperability (unit contract 

information services); Ops to Intel interoperability (alert, 

MISREP added to Intel web page); Map Edit capability; Webbased air crew sortie scheduling viewing; Automated Report 

Generator; Unclassified UL Ops; Web enabled base map with 

geospatial and Geobase capability; Client Windows XP O/S 

migration; Unit Level Intel – Spiral 10: Migration to GCCS-I3 

Disconnected Operations; Leverage TBMCS FL 1.1.4 web 

services; Migration to Common Geopositioning Services 

(CGS) from Raindrop & Raindrop Extension as part of the 

TAW solution; Windows XP Professional Operating System
MISSION

242 UNITED STATES AIR FORCE

Transformational Satellite Communications System (TSAT)

Mission

Provide wideband tactical, protected tactical, mobile tactical, strategic, 

and relay type satellite-based communications to DoD, government, 

and allied forces/international partners.

Description

The Transformational Satellite Communications System (TSAT) is a next-generation 

communication satellite system that provides strategic and tactical protected communications. TSAT incorporates laser communications and packet routing/switching 

protocols to provide a high bandwidth environment. It extends the DoD groundbased Global Information Grid network to deployed and mobile users and provides 

assured command and control to strategic forces. It delivers medium and high-datarate wideband communications exfiltration from Intelligence, Surveillance, and 

Reconnaissance (ISR) assets. TSAT increases throughput to tactical users, allowing 

communications-on-the-move and persistent worldwide connectivity of ISR 

assets. TSAT interfaces across the satellite communications (SATCOM) systems of other 

agencies. It consists of a five-satellite space segment with associated command and 

control, ground gateways, and the TSAT Mission Operations System (TMOS).
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 243

STRATEGIC CAPABILITY

T

r

ans

formational Satellite Commu

nications 

Syste

m (TS

AT)

Contractors

Prime: Space Segment - Lockheed 

Martin Space Systems (CA), Boeing 

Space & Intelligence Systems (CA); 

TMOS/Network Segment - 

Lockheed Martin Integrated 

Systems and Solutions (CA); 

Systems Engineering and 

Integration - Booz Allen 

Hamilton (VA) 

Subcontractor(s): Northrop Grumman (CA); Raytheon (CO, MA); Ball Aerospace 

(CO); Verizon (VA)

Specifications

Weight TBD

Coverage Global Coverage 65° N–65° S

Capacity/Satellite

Protected EHF: 45 Mbps max data rate; 2,340 Mbps loaded 

throughput; Wideband Ka: 311 Mbps max data rate (uplink 

only); 1,866 Mbps loaded throughput (uplink only); Laser: 

2,440 Mbps data rate; 4.880 Mbps (Block I) 9,760 Mbps 

(Block II) loaded throughput; 4,880 Mbps loaded throughput (terminal constrained); 10,000 Mbps laser crosslinks

Interoperability Space-based component of DoD Global Information Grid

Compatability Backwards compatible to Advanced Extremely High Frequency (AEHF) Extended Data Rate (XDR) terminals

Acquisition Status

Program Status

System Requirements Review - 1QFY04); TMOS contract 

award - 2QFY06; System Design Review - 3QFY07; Space 

Segment contract award - 1QFY08; First launch planned 

for 1QFY16
MISSION

244 UNITED STATES AIR FORCE

Tunner 60K Loader

Mission

Provide single-system cargo loading, off-loading, and transport

between warehouses and aircraft.

Description

The Tunner 60K Loader has a total loading capacity of 60,000 pounds. It will replace 

older 40,000-pound capacity loaders in the Air Force inventory. The Loader can carry 

up to six cargo pallets at once, drive on and off C-5 and C-17 aircraft, and load and 

unload cargo from all military and commercial cargo aircraft. Other advantages of the 

Loader include an improved turning radius, higher top speed, and mechanized rollers 

that greatly enhance the loading and unloading process. The Loader is five times 

more reliable than its predecessors and 150 to 350 percent more capable.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 245

STRATEGIC CAPABILITY

Tunner 60

K Lo

ader

Contractors

Prime: DRS Technologies, Inc. (MO) 

(Formerly Systems & Electronics, Inc) 

Subcontractor(s): Hydraulics 

- Linde Hydraulics (OH); Castings 

- Carondolet Foundry (MO); Engine 

- Detroit Diesel (MI); Hydraulic 

Cylinders - Commercial Intertech 

(MN); Hydraulic fittings, hoses 

- Parker Hanifin (OH); Wheel hubs

- Fairfield Manufacturing (OH)

Specifications

Weight Approx 65,000 lb. 

Dimension

Transport: Length - 591 inches, Width - 111 inches, 

Height - 94 inches; Operation: Length - 591 inches, 

Width - 171 inches; Height - 94 inches 

Deck Height 39 in. to 18.5 ft.

Speed 23 mph (governed) 

Payload 60,000 lb. (6 pallets) 

Acquisition Status

Program Status Sustainment; delivery completed 31 Mar 05 

Unit Assignment 75 locations worldwide

Current Inventory 318

Future Upgrades None
MISSION

246 UNITED STATES AIR FORCE

U-2S Dragon Lady

Mission

Provide near-real-time intelligence from high-altitude/near space to 

support operations across the spectrum of conflict. 

Description

The U-2 weapon system consists of the aircraft, sensors, and data links, and combines 

high-altitude/near space, over-flight, and stand-off sensor capabilities. The U-2 

provides all-weather surveillance and reconnaissance, day or night, in direct support 

of U.S. and allied forces. It delivers critical Imagery Intelligence (IMINT), Signals 

Intelligence (SIGINT), and Measurement and Signature Intelligence (MASINT) to 

decision makers throughout all phases of conflict, including peacetime indications 

and warnings, low-intensity conflict, and large-scale hostilities. The U-2S is a 

single-seat, single-engine aircraft. Long and narrow wings give the U-2 glider-like 

characteristics and allow it to quickly lift heavy sensor payloads to unmatched 

altitudes, keeping them there for extended periods of time.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 247

STRATEGIC CAPABILITY

U-2S

D

r

agon L

ady

Contractors

Prime: Airframe - Lockheed Martin 

(CA) 

Subcontractor(s):Sensors - 

Raytheon (CA); Major Subsystem

- L-3 Communications (VA); 

Propulsion - General Electric 

(UT); Sensors - B.F. Goodrich (OH); 

Northrop Grumman (VT); BAE (GA) 

Specifications

Size 40,000 lb. takeoff gross weight

Range 7,000+ miles

Dimensions Length: 63 ft.; Wingspan: 104 ft.; Height: 16 ft.

Coverage

Wide Area coverage due to high altitude. Sensor Data: Varies by aircraft/sensor configurations - Radar and SIGINT, or 

EO/IR and SIGINT; includes an Optical Bar Camera capability 

configuration that provides Synoptic Broad Area coverage

Interoperability

Sensor data currently provided via Ku or X-band Line of 

Sight (LOS) or government Beyond Line of Sight (BLOS) 

data links, or both simultaneously, and is interoperable 

with Distributed Common Ground Station (DCGS) systems 

(including compatible Army, Navy and Marine Corp) surface 

terminals. IMINT sensor data meets National Imagery 

Transmission Format. 

Compatability

Sensor data can be sent to MOBSTR (ground relay station), 

direct to satellite for BLOS link, and DCGS ground stations. 

IMINT data can be injected onto the WAN by DCGS for use by 

other intelligence network customers.

Altitude 70,000+ ft. 

Endurance >10 hours

Payload 5,000 lb.; Multi-INT (simultaneous)

Speed 410+ knots (475+ mph)

Acquisition Status

Program Status Sustainment

Current Inventory 33 aircraft - 28 single seat and five two-seat trainers 

Future Upgrades

Aircraft wiring, cockpit, and sensor upgrades; Glass Cockpit 

(Block-20); Defensive System RWR/JAM; ASARS-2A Radar; 

Sensor upgrades: SYERS-2A EO/IR; Dual Data Link/Link-16; 

SIGINT
MISSION

248 UNITED STATES AIR FORCE

UH-1N Helicopter (Variants: 1H/Vm, UV-18B) 

Mission

Provide Intercontinental Ballistic Missile (ICBM) and range security, 

distinguished visitor evacuation and airlift, and test and survival school 

support.

Description

The UH-1N Huey is a light-lift utility helicopter used at 10 operating locations at six 

major commands. The UH-1N and its variants, 1H/VM and UV-18B, provide ICBM 

and range security, distinguished visitor evacuation and airlift, and test and survival 

school support. 
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 249

STRATEGIC CAPABILITY

Contractors

Prime: Bell Helicopter 

Company (TX) 

Subcontractor(s): Aerospace 

Integration Corporation (FL) 

Specifications

Range 300 nautical miles (NM)

Dimensions Length: 57 ft., 7 in.; Width: 9 ft., 5 in.; Height: 12 ft., 10 in.; 

Rotor: 48 ft.

Acquisition Status

Program Status Fielded 

Unit Assignment

Andrews AFB, MD; Malmstrom AFB, MT; Vandenburg AFB, 

CA; F.E. Warren AFB, WY; Minot AFB, ND; Kirtland AFB, NM; 

Eglin AFB, FL; Hurlburt AFB, FL; Yakota AFB, Japan

Future Upgrades Undergoing life extension programs

U

H-1N

H

elic

o

pter (Va

riants: 1H/V

m, UV-18B) 
MISSION

250 UNITED STATES AIR FORCE

VC-25A 

Mission

Provide worldwide air transport for the President of the United States.

Description

The VC-25A is a military variant of the commercial Boeing 747-200 equipped with 

robust communications and data transfer systems that enable the president to 

implement the constitutional roles of commander-in-chief of the Armed Forces, head 

of state, and chief executive while travelling. It is known as “Air Force One” when the 

president is aboard.
GLOBAL REACH

THE AIR FORCE HANDBOOK 2007 251

STRATEGIC CAPABILITY

VC-25A 

Contractors

Prime: Airframe, Engines - Boeing 

Integrated Defense System (OK)

Specifications

Weight 833,000 lb.

Range 6,800 nautical miles (NM) 

Dimensions Length: 232 ft.; Height: 63 ft.; Wingspan: 196 ft.

Service Ceiling 45,000 ft.

Speed 570 mph (Mach 0.84)

Passenger Capacity 76 passengers and 26 crew

Acquisition Status

Program Status Sustainment

Unit Assignment Andrews AFB, MD

Current Inventory 2

Future Upgrades Presidential Data System (PDS), Communications, Navigation, Surveillance/Air Traffic Management (CNS/ATM)
MISSION

252 UNITED STATES AIR FORCE

WC-135 Constant Phoenix 

Mission

Supports national level consumers by collecting particulate and gaseous effluents and debris from accessible regions of the atmosphere in 

support of the Limited Nuclear Test Ban Treaty of 1963, which prohibits 

any nation from above ground nuclear weapons testing. 

DeScription

Constant Phoenix is currently the only aircraft in the inventory conducting air-sampling operations. The aircraft’s on-board atmospheric collection suite allows the 

mission crew to detect radioactive clouds in real-time. The aircraft is equipped with 

external flow-through devices to collect particulates on filter paper and a compressor 

system for whole air samples collected in holding spheres.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 253

STRATEGIC CAPABILITY

WC-135 Constant Phoenix 

Contractors

Prime: Major Subsystems: L-3 

Communications, Raytheon, Harris 

Information Systems (TX)

Subcontractor(s): PropulsionPratt & Whitney (CT); AirframeBoeing (WA)

Specifications

Weight 299,000 lb. maximum gross take-off weight;

130,000 lb. aircraft basic weight

Range 5,000 + miles unrefueled; inflight refueling capable

Dimensions Length: 140 ft.; Wingspan: 131 ft.; Height: 42 ft.

Speed 500 mph

Duration 8–10 hours unrefueled, limited only by aircrew duty 

requirements if aerial refueled

Acquisition Status

Program Status Modification and Sustainment

Unit Assignment 55th Wing, Offutt AFB, NE

Current Inventory Two mission aircraft
MISSION

254 UNITED STATES AIR FORCE

Wideband global satcom (WGS) system

Mission

Provide beyond-line-of-sight and long-haul communication relay from 

geosynchronous orbit 22,000 miles above the earth’s surface.

Description 

The Wideband Global SATCOM (WGS) system provides unprotected wideband communications for deployed forces and warfighter communications using existing 

terminals. It is a follow-on to Defense Satellite Communications System (DSCS) satellites and takes on the Global Broadcast Service (GBS) mission. The system consists of 

five satellites using existing and new wideband terminals.
GLOBAL VIGILANCE

THE AIR FORCE HANDBOOK 2007 255

STRATEGIC CAPABILITY

Wideband g

l

obal s

at

c

o

m (WGS) 

Contractors

Prime: Boeing Satellite Systems (CA)

Subcontractor(s): Harris Corporation (CO), ITT Industries (CO), Logicon 

(CA), SAIC (CA)

specifications

Size Five-satellite constellation

Weight 10,262 lb.

Coverage Global Coverage: 65° N–65° S

Capacity/Satellite Wideband Ka / X mix: 137 (SV 1-3), 274 (SV 4-5) Mbps max 

data rate; 2,100 Mbps loaded throughput

Compatibility Compatible with existing wideband terminals

acquisition status

Program Status

Concept Design Review (CDR) - 4QFY02; WGS 4, 5, and 

option for 6 Contract Award - 1QFY07; First launch planned 

for 3QFY07
MISSION

256 UNITED STATES AIR FORCE

Wind Corrected Munitions Dispenser (WCMD)

and WCMD-Extended Range (WCMD-ER)

Mission 

Provide accurate dispenser weapon capability when delivered from 

medium to high altitudes.

Description

The Wind Corrected Munitions Dispenser (WCMD) is a tail kit for use on inventory 

cluster weapons such as the Combined Effects Munition (CEM) and the Sensor Fused 

Weapon (SFW). The CEM is an anti-armor/anti-personnel weapon. The SFW is an 

anti-armor weapon. Development of the WCMD-Extended Range (ER) began in 2003 

to add a wing kit and to integrate GPS into the WCMD-ER wing kit. 
GLOBAL POWER

THE AIR FORCE HANDBOOK 2007 257

STRATEGIC CAPABILITY

Wind Corre

cted M

u

nitions Di

s

penser (

WCM

D) 

and 

WCM

D-Extended Range (

WCM

D-ER)

Contractors

Prime: Lockheed Martin (FL, GA)

Subcontractor(s): Honeywell 

Military Avionics (MN); 

B.F. Goodrich (VT); General 

Technology Corporation (NM); 

Kurt Manufacturing (MN)

Specifications

Weight 100 lb.

Dimensions Length: 1.42 ft.; Width: 1.75 ft.; Height: 1.75 ft.

Compatability CBU-87, CBU-89, and CBU-97

Acquisition Status

Program Status WCMD no longer in production; WCMD-ER terminated.

Current Inventory 24,000
258 UNITED STATES AIR FORCE
appendices

THE AIR FORCE HANDBOOK 2007 259

Air Force Demographics

Air Force Units of Operation

combat wings

air force installation locations

Glossary of Terms/Acronyms

Systems by Contractor

Systems by State
260 UNITED STATES AIR FORCE
AIR FOR

C

E DE

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C

S

THE AIR FORCE HANDBOOK 2007 261

Strength Figures

Air Force Reserve Selected Reserve strength, fiscal years 48–07

334,200

167,184

65,776

107,000

74,900

264,424

1,000,000

900,000

800,000

700,000

600,000

500,000

400,000

300,000

200,000

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

1,000,000

900,000

800,000

700,000

600,000

500,000

400,000

300,000

200,000

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

Enlisted strength, fiscal years 48–07

200,000

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

Officer strength, fiscal years 48–07

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

200,000

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

Air National Guard strength, fiscal years 48–07

400,000

300,000

200,000

100,000

Fiscal Year 48 50 55 60 65 70 75 80 85 90 95 00 05

Civilian strength, fiscal years 48–07

Active duty strength, fiscal years 48–07

Data shown in red indicates 2007 projections

air force demographics
262 UNITED STATES AIR FORCE

Personnel facts

19.7% women

60.6% married

AF Population by Gender

(total active force)

Marital Status

(total active force)

57.8% married

Marital Status

(active enlisted)

71.4% married

Marital Status

(active officers)

80.3% men

23% overseas

77% stateside

Assignments

(stateside vs. overseas)

47.9% officers 52.1% enlisted

Female Air Force

(officers vs. enlisted)

50.5% officers 49.5% enlisted

Male Air Force

(officers vs. enlisted)

42.9% AFROTC 19.5% USAFA

Commissioning Source

(active force)

21.1% OTS

16.5% other

sources

Air force Demographics
AIR FOR

C

E DE

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THE AIR FORCE HANDBOOK 2007 263

74.4% White

14.8% Black or African-American

2.3% Asian

5.7% not identified

0.8% Native Hawaiian or 

other Pacific Islander

1.4% more than one category

0.6% American Indian or 

Alaska Native

Racial Breakdown

(total active force)

88.1% not “Hispanic/Latino”

Ethnicity

(total active force)

8.8% call themselves 

“Hispanic/Latino*”

3.0% declined to respond

73.3% high school plus 

some college

16.2% associate’s degree

0.7% master’s degree

or higher

5.1% unknown

Highest Academic Education Attained

(active enlisted)

4.7% bachelor’s degree

50.8% bachelor’s

degree 39.4% master’s

degree

8.5% professional degree

1.3% doctorate

Highest Academic Education Attained

(active officers)

*“Hispanic” or “Latino” is considered an 

ethnic category that is registered separately

and in addition to the above racial categories. 
Air force Demographics

264 UNITED STATES AIR FORCE

Mission Intra- Tanker Rescue

Theater

Airlift

InterTheater

Airlift

Bomber Fighter Special C2

Ops

ISR

20%

30%

10%

40%

60%

80%

100%

50%

70%

90% Air National Guard

Air Force Reserve

LEGEND

Active Duty

OIF/OEF Missions Performed by Components

(FY07 Percentages)
Air For

ce Units o

f Oper

ation

THE AIR FORCE HANDBOOK 2007 265

Organization of the U.S. Air Force

The Department of the Air Force was created with the National Security Act of 1947. 

It became effective Sept. 18, 1947 and, in 1958, the departments of the Army, Navy, 

and Air Force were eliminated from the chain of operational command. Commanders of unified and specified commands became responsible to the president and the 

Secretary of Defense through the Joint Chiefs of Staff.

Air Force Management

The Headquarters of the Air Force incorporates all elements of the U.S. Air Force. It 

is administered by a civilian Secretary appointed by the President and is supervised 

by a military Chief of Staff. To ensure unit preparedness and overall effectiveness of 

the Air Force, the Secretary of the Air Force is responsible for and has the authority to 

conduct all affairs of the Department of the Air Force.

The Secretary’s responsibilities include research and development, and any other 

activity assigned by the President or the Secretary of Defense. The Secretary of the Air 

Force exercises authority through civilian assistants and the Chief of Staff, but retains 

immediate supervision of activities that involve vital relationships with Congress, the 

Secretary of Defense, other governmental officials, and the public.

The Air Staff

The Chief of Staff, U.S. Air Force, is appointed by the President, with the consent of the 

Senate, from among Air Force general officers, customarily for a term of four-years. 

The Chief of Staff serves as a member of the Joint Chiefs of Staff and the Armed Forces 

Policy Council. In this capacity, the Chief is one of the military advisors to the President, the National Security Council, and the Secretary of Defense. Also, the Chief is 

the principal advisor to the Secretary of the Air Force on Air Force activities.

The Chief of Staff presides over the Air Staff, transmits Air Staff plans and recommendations to the Secretary of the Air Force, and acts as the Secretary’s agent in 

carrying them out. The Chief is responsible for the efficiency of the Air Force and 

the preparation of its forces for military operations. The Chief of Staff supervises the 

administration of Air Force personnel assigned to unified organizations and unified 

and specified commands. Also, the Chief supervises support of these forces assigned 

by the Air Force as directed by the Secretary of Defense. In addition, the Chief of Staff 

has responsibility for activities assigned to the Air Force by the Secretary of Defense.

Field Organizations

The Air Force has eleven major commands, 32 field operating agencies, and five direct 

reporting units with subordinate elements to carry out its mission. In addition, there 

are two Reserve components: the Air Force Reserve, which is also a major command, 

and the Air National Guard.

Air Force Units of Operation
Air Force Units of Operation

266 UNITED STATES AIR FORCE

Major commands are organized on a functional basis in the United States and on a 

geographic basis overseas. They accomplish designated phases of Air Force worldwide 

activities. Also, they organize, administer, equip, and train their subordinate elements 

for the accomplishment of assigned missions. Major commands generally are assigned specific responsibilities based on functions. In descending order of command, 

elements of major commands include numbered air forces, wings, groups, squadrons, 

and flights.

The Wing

The basic unit for generating and employing combat capability is the wing. Composite wings operate more than one kind of aircraft, and may be configured as self-contained units designated for quick air intervention anywhere in the world. Other wings 

continue to operate a single aircraft type ready to join air campaigns anywhere they 

are needed. Air base and specialized mission wings such as training, intelligence, and 

test also support the Air Force mission.

Group

A group is a large Air Force formation usually composed of four or more squadrons 

and the bases from which they operate.

Squadron

A squadron is the basic unit of the Air Force, usually consisting of ten to eighteen 

aircraft

Flight

The flight is an air force unit that is smaller than a squadron

Field Operating Agencies and Direct Reporting Units

Field operating agencies and direct reporting units are other Air Force subdivisions 

and report directly to Headquarters U.S. Air Force. They are assigned a specialized 

mission that is restricted in scope when compared to the mission of a major command. Field operating agencies carry out field activities under the operational control 

of a Headquarters U.S. Air Force functional manager. Direct reporting units are not 

under the operational control of a Headquarters U.S. Air Force functional manager 

because of a unique mission, legal requirements or other factors.

Air Force Units of Operation
Air For

ce Units o

f Oper

ation

THE AIR FORCE HANDBOOK 2007 267

In an effort to accurately capture the breadth, depth, and scope of Combatant Commander requirements, the Air Force set out to define a common measure for all units 

of action. The simplest way to do this was to group by capabilities and count by 

assets.

Combat Wings depict aggregate combat power in terms of fighters, bombers, C4ISR, 

mobility, space, missiles, SOF, Battlefield Airmen, and Air Operations Centers. The 

Combat Wing is equal to the number of combat assets (aircraft, missiles, etc.) divided 

by the normal number of assets per squadron divided by the number of squadrons 

per wing. 

NUMBER OF ASSETS ÷ ASSETS PER SQUADRON ÷ 

SQUADRONS PER WING = COMBAT WING

Combat Wings represent the capability picture. After consulting the National Security 

Strategy and the National Military Strategy, the Air Force determined that 86 Combat 

Wings were the essential number needed to fully execute the mission. The Combat 

Wing delivers a more complete comparison between historical, current, and future 

demands of collective combat power for commanders by providing the necessary 

framework to ensure a leaner, more capable force framework, allowing combat 

forces the effects they need, when they need them. The added utility provided by the 

Combat Wing will continue to be employed in the Air and Space Expeditionary Forces 

(AEF) to ensure flexible, cost effective, and tailored expeditionary requirements of the 

Combatant Commanders.

Combat wings

Air For

ce installation 

l

ocations

THE AIR FORCE HANDBOOK 2007 269

ALABAMA

Maxwell AFB

Montgomery, AL

• Air University, AETC

• 42nd Air Base Wing, AETC

• 908th Airlift Wing, AFRC 

• Air Force Doctrine Center 

• Air Force Historical Research Agency

• Civil Air Patrol 

Gunter Annex

Montgomery, AL

• Air Force Logistics Management 

Agency

Fort Rucker

Dale County, AL

• 23rd Flying Training Squadron, AETC

117 Air Refueling Wing, ANG

Birmingham Arpt., AL

187 Fighter Wing, ANG

Montgomery Regional Arpt.

ALASKA

Eielson AFB

Fairbanks, AK

• 354th Fighter Wing, PACAF

Elmendorf AFB

Anchorage, AK

• 3rd Wing, PACAF

• 11th Air Force, PACAF

Clear AFS

Anderson, AK

176 Wing, ANG

Kulis ANGB, AK

ARIZONA

Davis-Monthan AFB

Tucson, AZ

• 12th Air Force, ACC

• 55th Electronic Combat Group, ACC

• 355th Wing, ACC

• 563rd Rescue Group, AFSOC

• 943rd Rescue Group, AFRC 

• Aerospace Maintenance & Regeneration Center, AFMC

Luke AFB

Phoenix, AZ

• 56th Fighter Wing, AETC

• 944th Fighter Wing, AFRC

161 Air Refueling Wing, ANG

Sky Harbor Arpt., AZ

162 Fighter Wing, ANG

Tucson Arpt., AZ

ARKANSAS

Little Rock AFB

Little Rock, AR

• 314th Airlift Wing, AETC

• 463rd Airlift Group, AMC

188 Fighter Wing, ANG

Fort Smith Arpt., AR

CALIFORNIA

Beale AFB

Marysville, CA

• 9th Reconnaissance Wing, ACC

• 940th Air Refueling Wing, AFRC

Edwards AFB

Rosamond, CA

• 95th Air Base Wing, AFMC

• 412th Test Wing, AFMC 

• Air Force Flight Test Center, AFMC

Los Angeles AFB

El Segundo, CA

• Space and Missile Systems Center, 

AFSPC

March ARB

Riverside, CA

• 4th Air Force, AFRC

• 452nd Air Mobility Wing, AFRC

McClellan AFB

Sacramento, CA

Air force installation locations

THE AIR FORCE HANDBOOK 2007 269
Air Force Installation Locations

270 UNITED STATES AIR FORCE

Travis AFB

San Francisco, CA

• 15th Expeditionary Mobility Task 

Force, AMC

• 60th Air Mobility Wing, AMC

• 349th Air Mobility Wing, AFRC

• 615th Contingency Response Wing, 

AMC

Vandenberg AFB

Lompoc, CA

• 14th Air Force, AFSPC

• 30th Space Wing, AFSPC

• 381st Training Group, AETC

Onizuka AFS

Sunnyvale, CA

129 Refueling Wing, ANG

Moffett Field, CA 

144 Fighter Wing, ANG

Fresno Yosemite Arpt., CA

146 Airlift Wing, ANG

Channel Islands ANGS, CA

COLORADO

Buckley AFB

Denver, CA

• 460th Space Wing, AFSPC

Peterson AFB, Colorado Springs

• Air Force Space Command

• 21st Space Wing, AFSPC

• 302nd Airlift Wing, AFRC

Schriever AFB

Colorado Springs, CO

• 50th Space Wing, AFSPC

• 310th Space Group, AFRC 

United States Air Force Academy

Colorado Springs, CO

• 306th Flying Traing Group, AETC

137th Space Warning Squadron, ANG

Greeley ANGB, CO

Cheyenne Mountain AFS

Cheyenne Mountain, CO

Air Reserve Personnel Center

CONNECTICUT

103th Fighter Wing, ANG

Bradley Arpt., CT

DELAWARE

Dover AFB

Dover, DE

• 436th Airlift Wing, AMC

• 512th Airlift Wing, AFRC

166 Airlift Wing, ANG

New Castle County Arpt., DE

DISTRICT OFCOLUMBIA

Bolling AFB

Washington, DC

• Air Force District of Washington

• Air Force Legal Services Agency 

Headquarters Air Force

Washington, DC

• Air Force Studies and Analyses Agency

• Air Force Audit Agency

• Air Force Pentagon Communications 

Agency

• Air Force Personnel Operations Agency

• Air Force Medical Operations Agency

• Air Force Nuclear Weapons and Counter Proliferation Agency

• Air Force Operations Group

FLORIDA

Eglin AFB

Niceville/Valparaiso, FL

• 9th Special Operations Squadron, 

AFSOC

• 33rd Fighter Wing, ACC

• 53rd Wing, ACC

• 46th Test Wing, AFMC
Air For

ce installation 

l

ocations

THE AIR FORCE HANDBOOK 2007 271

• 96th Air Base Wing, AFMC

• Air Armament Center, AFMC

• Air-to-Air Missile Systems Wing, AFMC

• Air-to-Ground Munitions Systems 

Wing, AFMC

Hurlburt Field

Fort Walton Beach, FL

• Air Force Special Operations Command

• 16th Special Operation Wing, AFSOC

• 18th Flight Test Squadron, AFSOC

• 505th Command and Control Wing, 

ACC

• 720th Special Tactics Group, AFSOC

• USAF Special Operations School, 

AFSOC

MacDill AFB

Tampa, FL

• 6th Air Mobility Wing, AMC

Patrick AFB, Cocoa Beach

• 45th Space Wing, AFSPC

• 920th Rescue Wing, AFRC

• Air Force Technical Applications 

Center

Tyndall AFB

Panama City, FL

• 1st Air Force, ANG

• 53rd Weapons Evaluation Group, ACC

• 325th Fighter Wing, AETC

• Air Force Civil Engineer Support 

Agency 

Cape Canaveral AFS

• 45th Space Wing, AFSPC

919th Special Ops Wing, AFRC

Duke Field, FL

482nd Fighter Wing, AFRC

Homestead ARB, FL

125 Fighter Wing, ANG

Jacksonville Arpt., FL

Air Force Agency for Modeling and 

Simulation

GEORGIA

Dobbins ARB

Atlanta, GA

• 22nd Air Force, AFRC

• 94th Airlift Wing

Moody AFB

Valdosta, GA

• 347th Rescue Wing, AFSOC 

• 479th Flying Training Group, AETC 

Robins AFB

Warner Robins, GA

• Air Force Reserve Command

• 19th Air Refueling Group, AMC

• 116th Air Control Wing, ACC

• 78th Air Base Wing, AFMC

• 330th Aircraft Sustainment Wing, 

AFMC

• 402nd Maintenance Wing, AFMC

• 542nd Combat Sustainment Wing, 

AFMC

• AFRC Recruiting Service

• Warner Robins Air Logistics Center, 

AFMC 

165 Airlift Wing, ANG

Savannah Hilton Head Arpt., GA

GUAM

Andersen AFB

Yigo, Guam

• 36th Wing, PACAF

HAWAII

Hickam AFB

Honolulu, HI

• Pacific Air Forces

• 13th Air Force/Kenney Warfghting 

Hq., PACAF

• 15th Airlift Wing, PACAF

• 715th Air Mobility Operations Group, 

AMC
Air Force Installation Locations

272 UNITED STATES AIR FORCE

IDAHO

Mountain Home AFB

Boise, ID

• 366th Fighter Wing, ACC

124 Wing, ANG

Boise Air Terminal, ID

ILLINOIS

Scott AFB

Belleville, IL

• Air Mobility Command

• 18th Air Force, AMC

• 375th Airlift Wing, AMC

• 932nd Airlift Wing, AFRC

• Air Force Communications Agency

182 Airlift Wing, ANG

Greater Peoria Arpt., IL

183 Fighter Wing, ANG

Abraham Lincoln Capital Arpt., IL

INDIANA

Grissom ARB

Kokomo, IN

• 434th Air Refueling Wing, AFRC

122 Fighter Wing, ANG

Fort Wayne Arpt., IN

181 Fighter Wing, ANG

Hulman Arpt., IN

IOWA

132 Fighter Wing, ANG

Des Moines Arpt., IA

185 Air Refueling Wing, ANG

Sioux Gateway Arpt./Col. Bud Day Field, 

IA

KANSAS

McConnell AFB

Wichita, KS

• 22nd Air Refueling Wing, AMC

• 931st Air Refueling Group, AFRC

190 Air Refueling Wing, ANG

Forbes Field, KS

KENTUCKY

123 Airlift Wing, ANG

Louisville Arpt./AGS, KY

LOUISIANA

Barksdale AFB, ACC

Bossier City, LA

• 8th Air Force, ACC

• 2nd Bomb Wing, ACC

• 917th Wing, AFRC

926th Fighter Wing, AFRC

NAS JRB, LA

159 Fighter Wing, ANG

NAS JRB, LA

MAINE

101 Air Refueling Wing, ANG

Bangor Arpt., ME

MARYLAND

Andrews AFB

Andrews AFB, MD

• 89th Airlift Wing, AMC

• 459th Air Refueling Wing, AFRC 

• Air Force Flight Standards Agency

• Air Force Office of Special Investigations

• Air Force Review Boards Agency

• Air National Guard Readiness Center

Fort Meade

Laurel, MD

• 70th Intelligence Wing, ACC

175 Wing, ANG

Martin State Arpt., MD
Air For

ce installation 

l

ocations

THE AIR FORCE HANDBOOK 2007 273

MASSACHUSETTS

Hanscom AFB

Boston, MA

• 66th Air Base Wing, AFMC

• Battle Management Systems Wing, 

AFMC

• C2ISR Systems Wing, AFMC

• Electronic Systems Center, AFMC

• Network Centric Ops/Integration 

Systems Wing, AFMC

• Operations Support Systems Wing, 

AFMC

Cape Cod AFS

439th Airlift Wing, AFRC

Westover ARB, AFRC

102 Fighter Wing, ANG

Otis ANGB, MA

104 Fighter Wing, ANG

Barnes Arpt., MA

MICHIGAN

927th Air Refueling Wing, AFRC

Selfridge ANGB, MI

110 Fighter Wing, ANG

W.K. Kellogg Arpt., MI

127 Wing, ANG

Selfridge ANGB, MI

MINNESOTA

934th Airlift Wing, AFRC

Minneapolis-St. Paul Arpt./ARS, MN

133 Airlift Wing, ANG

Minneapolis-St. Paul Arpt./ARS , MN

148 Fighter Wing, ANG

Duluth Arpt., MN

MISSISSIPPI

Columbus AFB

Columbus, MS

• 14th Flying Training Wing, AETC

Keesler AFB

Biloxi, MS

• 2nd Air Force, AETC

• 45th Airlift Squadron, AETC

• 81st Training Wing, AETC

• 403rd Wing, AFRC

172 Airlift Wing, ANG

Allen C. Thompson Field, MS

186 Air Refueling Wing, ANG

Key Field, MS

MISSOURI

Whiteman AFB

Knob Noster, MO

• 442nd Fighter Wing, AFRC

• 509th Bomb Wing, ACC

131 Fighter Wing, ANG

Lambert-St. Louis Arpt., MO

139 Airlift Wing, ANG

Rosecrans Memorial Arpt., MO

MONTANA

Malmstrom AFB

Great Falls, MT

• 341st Space Wing, AFSPC

120 Fighter Wing, ANG

Great Falls Arpt., MT

NEBRASKA

Offutt AFB

Omaha, NE

• 55th Wing, ACC

• Air Force Weather Agency

155 Air Refueling Wing, ANG

Lincoln Arpt., NE
Air Force Installation Locations

274 UNITED STATES AIR FORCE

NEVADA

Creech AFB

Indian Springs, NV

Nellis AFB

Las Vegas, NV

• 57th Wing, ACC

• 58th Range Wing

• 98th Range Wing, ACC

• 99th Air Base Wing, ACC 

• USAF Warfare Center, ACC

152 Airlift Wing, ANG

Reno/Tahoe Arpt., NV

NEW HAMPSHIRE

157 Air Refueling Wing, ANG

Pease Intl. Tradeport ANGS, NH

NEW JERSEY

McGuire AFB

Trenton, NJ

• 21st Expeditionary Mobility Task 

Force, AMC 

• 305th Air Mobility Wing, AMC

• 514th Air Mobility Wing, AFRC

• 621st Contingency Response Wing, 

AMC

Fort Dix

New Hanover Township, NJ

• Air Mobility Warfare Center, AMC

177 Fighter Wing, ANG

Atlantic City Arpt., NJ

NEW MEXICO

Cannon AFB

Clovis, NM

• 27th Fighter Wing, ACC

Holloman AFB

Alamogordo, NM

• 49th Fighter Wing

Kirtland AFB

Albuquerque, NM

• 58th Special Operations Wing, AETC

• 377th Air Base Wing, AFMC

• 498th Air Armament Systems Wing, 

AFMC

• Air Force Inspection Agency 

• Air Force Operational Test and Evaluation Center

• Air Force Safety Center

• Nuclear Weapons Center, AFMC

NEW YORK

914th Airlift Wing, AFRC

Niagara Falls Arpt./ARS, NY

105 Airlift Wing, ANG

Stewart ANGB, NY

106 Rescue Wing, ANG

Francis S. Gabreski Arpt., NY

107 Air Refueling Wing, ANG

Niagara Falls Arpt./ARS, NY

109 Airlift Wing, ANG

Schenectady County Arpt., NY

174 Fighter Wing, ANG

Hancock Field, NY

NORTH CAROLINA

Pope AFB

Fayetteville, NC

• 23rd Fighter Group, ACC

• 43rd Airlift Wing, AMC 

Seymour Johnson AFB

Goldsboro, NC

• 4th Fighter Wing, ACC

• 916th Air Refueling Wing, AFRC

145 Airlift Wing, ANG

Charlotte/Douglas Arpt., NC
Air For

ce installation 

l

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THE AIR FORCE HANDBOOK 2007 275

NORTH DAKOTA

Grand Forks AFB

Grand Forks, ND

• 319th Air Refueling Wing, AMC

Minot AFB

Minot, ND

• 5th Bomb Wing, ACC

• 91st Space Wing, AFSPC

Cavalier AFS

119 Fighter Wing, ANG

Hector Arpt., ND

OHIO

Wright-Patterson AFB

Dayton, OH

• Air Force Materiel Command

• 88th Air Base Wing, AFMC

• 445th Airlift Wing, AFRC 

• Aeronautical Systems Center, AFMC

• Agile Combat Support Systems Wing, 

AFMC

• Air Force Research Laboratory, AFMC

• Air Force Security Assistance Center, 

AFMC

• Fighter Attack Systems Wing, AFMC

• Long Range Strike Systems Wing, 

AFMC

• Mobility Systems Wing, AFMC

• National Air and Space Intelligence 

Center (NASIC)

• National Museum of the US Air Force, 

AFMC

• Reconnaissance Systems Wing, AFMC

910th Airlift Wing, AFRC

Youngstown-Warren Arpt./ARS, OH

121 Air Refueling Wing, ANG

Rickenbacker ANGB, OH

178 Fighter Wing, ANG

Springfield-Beckley Arpt., OH

179 Airlift Wing, ANG

Mansfield Lahm Arpt., OH

180 Fighter Wing, ANG

Toledo Express Arpt., OH

OKLAHOMA

Altus AFB

Oklahoma City, OK

• 97th Air Mobility Wing, AETC

Tinker AFB

Oklahoma City, OK

• 72nd Air Base Wing, AFMC

• 76th Maintenance Wing, AFMC

• 327th Aircraft Sustainment Wing, 

AFMC

• 448th Combat Sustainment Wing, 

AFMC 

• 507th Air Refueling Wing, AFRC

• 513th Air Control Group, AFRC

• 552nd Air Control Wing, ACC

• Oklahoma City Air Logistics Center, 

AFMC

Vance AFB

Enid, OK

• 71st Flying Training Wing, AETC

138 Fighter Wing, ANG

Tulsa Arpt., OK

137 Airlift Wing, ANG

Will Rogers World Arpt., OK

OREGON

939th Air Refueling Wing, AFRC

Portland Arpt., OR

142 Fighter Wing, ANG

Portland Arpt., OR

173 Fighter Wing, ANG

Klamath Falls Arpt., OR

PENNSYLVANIA

911th Airlift Wing, AFRC

Pittsburgh Arpt., PA

913th Airlift Wing, AFRC

Willow Grove ARS, PA
Air Force Installation Locations

276 UNITED STATES AIR FORCE

111 Fighter Wing, ANG

Willow Grove ARS, PA

171 Air Refueling Wing, ANG

Pittsburgh Arpt./ARS, PA

193 Special Operations Wing, ANG 

Harrisburg Arpt., PA

PUERTO RICO

156th Airlift Wing, ANG

Luis Munoz Marin Arpt., PR

RHODE ISLAND

143 Airlift Wing, ANG

Quonset State Arpt., RI

SOUTH CAROLINA

Charleston AFB

Charleston, SC

• 315th Airlift Wing, AFRC

• 437th Airlift Wing, AMC

Shaw AFB

Sumter, SC

• 9th Air Force, ACC

• 20th Fighter Wing, ACC

169 Fighter Wing, ANG

McEntire ANGS, SC

SOUTH DAKOTA

Ellsworth AFB

Rapid City, SD

• 28th Bomb Wing, ACC

114 Fighter Wing, ANG

Joe Foss Field, SD

TENNESSEE

Arnold AFB

Manchester, TN

• Arnold Engineering Development 

Center, AFMC

118 Airlift Wing, ANG

Nashville Arpt., TN

134 Air Refueling Wing, ANG

McGhee Tyson Arpt., TN

164 Airlift Wing, ANG, Memphis Arpt.

TEXAS

Brooks City-Base

Brooks City, TN

• 311th Human Systems Wing, AFMC

• Air Force Center for Environmental 

Excellence

• Air Force Medical Support Agency

Dyess AFB

Abilene, TX

• 7th Bomb Wing, ACC

• 317th Airlift Group, AMC

Goodfellow AFB

San Angelo, TX

• 17th Training Wing, AETC

Kelly Field Annex

San Antonio, TX

Lackland AFB

San Antonio, TX

• 37th Training Wing, AETC

• 59th Medical Wing, AETC

• 67th Information Operations Wing, 

ACC

• 433rd Airlift Wing, AFRC

• Air Force Security Forces Center

• Air Intelligence Agency, ACC

Laughlin AFB, Del Rio

• 47th Flying Training Wing, AETC

Randolph AFB

San Antonio, TX

• 12th Flying Training Wing, AETC

• 19th Air Force, AETC 

• 340th Flying Training Group

• Air Education and Training Command

• Air Force Manpower Agency

• Air Force Personnel Center

• Air Force Recruiting Service, AETC

• Air Force Security Assistance Training 

Squadron, AETC
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Sheppard AFB

Wichita Falls, TX

• 80th Flying Training Wing, AETC

• 82nd Training Wing, AETC

Air Force News Agency

Air Force Services Agency

Naval Air Station, Joint Reserve 

Base

Fort Worth, TX

• 10th Air Force, AFRC

• 301st Fighter Wing, AFRC

147 Fighter Wing, ANG

Ellington Field, TX

149 Fighter Wing, ANG

Kelly Field, TX

UTAH

Hill AFB

Salt Lake City, UT

• 75th Air Base Wing, AFMC

• 84th Combat Sustainment Wing, 

AFMC

• 309th Maintenance Wing, AFMC

• 388th Fighter Wing, ACC

• 419th Fighter Wing, AFRC

• 508th Aircraft Sustainment Wing, 

AFMC

• 526th ICBM Systems Wing, AFMC 

• Ogden Air Logistics Center, AFMC

151 Air Refueling Wing, ANG

Salt Lake City Arpt., UT

VERMONT

158 Fighter Wing, ANG

Burlington Arpt., VT

VIRGINIA

Langley AFB, ACC

Hampton, VA

• Air Combat Command

• 1st Fighter Wing, ACC 

• 307th Fighter Squadron, AFRC

• 480th Intelligence Wing, ACC

• Air and Space Expeditionary Force 

Center

• Air Force Command and Control & 

Intelligence, Surveillance and Reconnaissance Center

• Air Force Rescue Coordination Center, 

AFSOC

192 Fighter Wing, ANG

Richmond Arpt., VA

Air Force Cost Analysis Agency

Air Force Frequency Management 

Agency

Air Force National Security 

Emergency Preparedness Agency

Air Force Real Property Agency

WASHINGTON

Fairchild AFB

Spokane, WA

• 92nd Air Refueling Wing, AMC 

• 336th Training Group, AETC

McChord AFB

Tacoma, WA

• 62nd Airlift Wing, AMC

• 446th Airlift Wing, AFRC

WEST VIRGINIA

130 Airlift Wing, ANG

Yeager Arpt., WV

167 Airlift Wing, ANG

Eastern West Virginia Arpt., WV

WISCONSIN

440th Airlift Wing, AFRC

General Mitchell Arpt., WI

115 Fighter Wing, ANG

Truax Field, WI

128 Air Refueling Wing, ANG

General Mitchell Arpt./ARS, WI
Air Force Installation Locations

WYOMING

F.E. Warren AFB

Cheyenne, WY

• 20th Air Force, AFSPC

• 90th Space Wing, AFSPC

153 Airlift Wing, ANG

Cheyenne Arpt., WY

Air Force Overseas Installations

GERMANY

Ramstein AB

• 16th Air Force, USAFE

• 86th Airlift Wing, USAFE

• 435th Air Base Wing, USAFE

• 721st Air Mobility Operations Group, 

AMC

Sembach AB

• 38th Combat Support Wing, USAFE

Spangdahlem AB

• 52nd Fighter Wing, USAFE

GREENLAND

Thule AB 

ITALY

Aviano AFB

• 31st Fighter Wing, USAFE

JAPAN

Kadena AB

• 18th Wing, PACAF

• 353rd Special Operations Group, 

AFSOC

Misawa AB

• 35th Fighter Wing, PACAF

Yokota AB

• 5th Air Force, PACAF

• 374th Fighter Wing, PACAF

SINGAPORE

Paya Lebar Airfield

• 497th Fighter Training Squadron, 

PACAF

SOUTH KOREA

Kunsan AB

• 8th Fighter Wing, PACAF

Osan AB

• 7th Air Force, PACAF

• 51st Fighter Wing, PACAF

THE AZORES

Lajes Field

• 65th Air Base Wing, USAFE

TURKEY

Incirlik AB

• 39th Air Base Wing, USAFE

UNITED KINGDOM

RAF Lakenheath

• 48th Fighter Wing, USAFE

RAF Mildenhall

• 100th Air Refueling Wing, USAFE

• 352nd Special Operations Group, 

AFSOC

• 501st Combat Support Wing, USAFE

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AEF – Air and Space Expeditionary Force

AEFC – Air and Space Expeditionary Force Center

AEHF – Advanced Extremely High Frequency

AETF – Air and Space Expeditionary Task Force

ALCM – Air-Launched Cruise Missile. An air-launched vehicle designed to deliver a 

nuclear warhead in an air-to-ground mission.

AMRAAM – Advanced Medium Range Air-to-Air Missile

AMTI – Air Moving Target Indicator

ANGB – Air National Guard Base

AOC – Air Operations Center

ARB – Air Reserve Base

ARS – Air Reserve Station

ASOC – Air and Space Operations Center. The senior agency of the Air Force component commander that provides command and control of Air Force air and space 

operations and coordinates with other components and services. Also called AOC.

BDA – Battle Damage Assessment

BLOS – Beyond Line of Sight

C2 – Command and Control

CAS – Close Air Support

CBU – Cluster Bomb Unit

CDR – Concept Design Review

CEM – Combined Effects Munition

CID – Combat Identification

CNS/ATM – Communication, Nagivation and Safety/Air Traffic Management

COCOM – Combatant Commander

CSAR – Combat Search and Rescue. Combat search and rescue is how the Air Force 

accomplishes the personnel recovery task. It is the Air Force’s preferred mechanism for 

personnel recovery execution in uncertain or hostile environments and denied areas.

DE – Directed Energy

Glossary of Terms/Acronyms
280 UNITED STATES AIR FORCE

Glossary of Terms/Acronyms

DSP – Defense Support Program

DT&E – Developmental Test and Evaluation. Any testing used to assist in the development and maturation of products, product elements, or manufacturing or support 

processes; any engineering-type test used to verify status of technical progress and 

minimize design risks, substantiate achievement of contract technical performance, 

and certify readiness for Initial Operational Testing (IOT).

ECM – Electronic Counter Measures

ERP – Enterprise Resource Planning

FAC – Forward Air Control

FFS – Forward Framing Sensor

Force Development – A series of experiences and challenges, combined with education and training opportunities, that is directed at producing Airmen who possess 

the requisite skills, knowledge, experience, and motivation to lead and execute the 

full spectrum of Air Force missions.

Force Protection – Actions taken to prevent or mitigate hostile actions against 

Department of Defense personnel (including family members), resources, facilities, 

and critical information.

FRP – Full Rate Production. Contracting for economic production quantities following stabilization of the system design and validation of the production process. 

FYDP – Future Years Defense Program. A massive DoD database and internal accounting system that summarizes forces and resources associated with programs 

approved by the Secretary of Defense.

GIG – Global Information Grid.The globally interconnected, end-to-end set of information capabilities, associated processes, and personnel for collecting, processing, 

storing, disseminating, and managing information on demand to warfighters, policy 

makers, and support personnel.

Global Mobility – The capability to move people and equipment across the world 

quickly, ensuring the right force anywhere, at any time.

GMTI – Ground Moving Target Indicator

GWOT – The Global War on Terrorism

HUMRO – Humanitarian Relief Operations 

IMINT – Imagery Intelligence

INS/GPS – Inertial Navigation System/Global Positioning System
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IOC – Initial Operational Capability

IOT – Initial Operational Testing

ISR – Intelligence, Surveillance, and Reconnaissance. Integrated capabilities to collect, process, exploit and disseminate accurate and timely information that provides 

the battlespace awareness necessary to successfully plan and conduct operations.

JAOC – Joint Air Operations Center. A jointly staffed facility established for planning, 

directing, and executing joint air operations in support of the joint force commander’s 

operation or campaign objectives. Also called Combined Air Operations Center (CAOC).

JCOMs – Joint Commands

JDAM – Joint Direct Attack Munition

JFACC – Joint Force Air Component Commander.The commander within a unified 

command, subordinate unified command, or joint task force responsible to the establishing commander for making recommendations on the proper employment of air 

forces; planning and coordinating air operations; or accomplishing such operational 

missions as may be assigned. The joint force air component commander is given the 

authority necessary to accomplish missions and tasks assigned by the establishing 

commander.

JFC – Joint Force Commander

JRB – Joint Reserve Base

LANTIRN – Low-Altitude Navigation and Targeting Infrared for Night

LOS – Line of Sight

LRIP – Low Rate Initial Production. The first effort of the Production and Deployment 

(P&D) phase. The purpose of this effort is to establish an initial production base for 

the system, permit an orderly ramp-up sufficient to lead to a smooth transition to Full 

Rate Production (FRP), and to provide production representative articles for Initial 

Operational Test and Evaluation (IOT&E) and full-up live fire testing. This effort concludes with a Full Rate Production Decision Review (FRPDR) to authorize the Full Rate 

Production and Deployment (FRP&D) effort.

MANPADS – Man Portable Air Defense Systems

MASINT – Measurement and Signature Intelligence

MCO – Major Combat Operation 

MS – Milestone. The point at which a recommendation is made and approval sought 

regarding starting or continuing an acquisition program, e.g., proceeding to the next 

phase. Milestones established by DoDI 5000.2 include the following:
282 UNITED STATES AIR FORCE

Glossary of Terms/Acronyms

• MS A approves entry into the Technology Development (TD) phase;

• MS B approves entry into the System Development and Demonstration (SDD) phase; 

 and

• MS C approves entry into the Production and Deployment (P&D) phase.

Also of note are the Concept Decision (CD) that approves entry into the Concept 

Refinement (CR) phase; the Design Readiness Review (DRR) that ends the System 

Integration (SI) effort and continues the SDD phase into the System Demonstration 

(SD) effort; and the Full Rate Production Decision Review (FRPDR) at the end of the 

Low Rate Initial Production (LRIP) effort of the P&D phase that authorizes Full Rate 

Production (FRP) and approves deployment of the system to the field or fleet.

NAS – Naval Air Station

Operationally Response Space – The ability to rapidly deploy and employ communication, ISR, and other space capabilities.

OT&E – Operational Test and Evaluation. The field test, under realistic conditions, of 

any item (or key component) of weapons, equipment, or munitions for the purpose of 

determining the effectiveness and suitability of the weapons, equipment, or munitions for use in combat by typical military users. It includes the evaluation of the 

results of such tests. 

P3I – Preplanned Product Improvement. Planned future improvement of developmental systems for which design considerations are effected during development 

to enhance future application of projected technology. It includes improvements 

planned for ongoing systems that go beyond the current performance envelope to 

achieve a needed operational capability. 

PDR – Preliminary Design Review. A multi-disciplined technical review to ensure 

that a system is ready to proceed into detailed design and can meet stated performance requirements within cost (program budget), schedule (program schedule), 

risk, and other system constraints.

Persistent C4ISR – The successful use of Command, Control, Communications, 

Computers, Intelligence, Surveillance, Reconnaissance (C4ISR), to ensure the ability to 

see first, think first, and act first in the battle space.

PLS – Personnel Locator System

PR – Personnel Recovery

RAIDRS – Rapid Attack Identification Detection and Reporting System

Rapid Strike – The Air Force’s ability to control air and space to deliver a precise, 

tailored effect anywhere, at any time.
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RDT&E – Research, Development, Test, and Evaluation. Activities for the development of a new system or to expand the performance of fielded systems.

RPA – Remotely Piloted Aircraft, i.e., Global Hawk

S&T – Science and Technology Program. Consists of projects in basic research, applied 

research, and Advanced Technology Development (ATD).

SA – Situational Awareness

SAM – Surface-to-Air Missile

SAR – Synthetic Aperture Radar

SATCOM – Satellite Communications

SD – System Demonstration. The second effort of the System Development and Demonstration (SDD) phase. A program enters SD after the Program Manager (PM) has 

demonstrated the system in prototype articles or Engineering Development Models 

(EDMs). The effort is intended to demonstrate the ability of the system to operate in 

a useful way consistent with the approved Key Performance Parameters (KPPs). This 

effort ends when the system is demonstrated in its intended environment using the 

selected prototype; meets approved requirements; industrial capabilities are reasonably available; and the system meets or exceeds exit criteria and Milestone C entrance 

requirements.

SDB – Small Diameter Bomb

SDD – System Development and Demonstration

SEAD/DEAD – Suppression/Destruction of Enemy Air Defenses

SIGINT – Signals Intelligence

SMTI – Surface Moving Target Indication

SOF – Special Operations Force

SSA – Space Situational Awareness

Sustainment – Execute support program to meet operational support performance 

requirements and sustain systems in the most cost-effective manner over its life 

cycle. Includes supply, maintenance, transportation, sustaining engineering, data 

management, Configuration Management (CM), manpower, personnel, training, 

habitability, survivability, environment, safety (including explosives safety), occupational health, protection of critical program information, anti-tamper provisions, 

Information Technology (IT) (including National Security Systems (NSSs)), supportability, and interoperability functions.
SDD – System Development and Demonstration. The third phase of a system life 

cycle. This phase consists of two efforts, System Integration (SI) and System Demonstration (SD), and begins after Milestone B. It also contains a Design Readiness 

Review (DRR) at the conclusion of the SI effort.

SRR – System Requirements Review. A review conducted to ascertain progress in 

defining system technical requirements. This review determines the direction and 

progress of the systems engineering effort and the degree of convergence upon a 

balanced and complete configuration.

T&E – Test and Evaluation. Process by which a system or components are exercised 

and results analyzed to provide performance-related information. The information 

has many uses including risk identification and risk mitigation and empirical data to 

validate models and simulations. T&E enables an assessment of the attainment of 

technical performance, specifications, and system maturity to determine whether 

systems are operationally effective, suitable and survivable for intended use, and/or 

lethal.

TARS – Theater Airborne Reconnaissance System

Threat – The sum of the potential strengths, capabilities, and strategic objectives of 

any adversary that can limit or negate U.S. mission accomplishment or reduce force, 

system, or equipment effectiveness. 

TST – Time Sensitive Targeting

UAS – Unmanned Aerial System. Also called UAV.

UCAV – Unmanned Combat Aerial Vehicle

WMD – Weapons of Mass Destruction

Glossary of Terms/Acronyms

284 UNITED STATES AIR FORCE
Glossary of Terms/Acronyms

Syste

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THE AIR FORCE HANDBOOK 2007 287

ADC 

Launch & Test Range System (LTRS) 

Adcole

Space Radar (SR)

AeroAstro

Space Test Program (STP) 

Aerojet

CBU-89/104 Gator

Evolved Expendable Launch Vehicle (EELV) 

LGM-30G Minuteman III 

Medium Launch Vehicle (MLV) 

Rocket Systems Launch Program (RSLP)

Aerospace Integration Corporation

UH-1N Helicopter (Variants: UH-1N, 1H/Vm UV-18B) 

Aero-Thrust

C-9C

Air Force Research Laboratory

Operationally Responsive Space (ORS)

Air Launch

Operationally Responsive Space (ORS)

Alcatel

Launch & Test Range System (LTRS) 

Alliant Tech Systems

AGM-65 Maverick

CBU-87/103 Combined Effects Munition (CEM)

CBU-89/104 Gator

CBU-97/105 Sensor Fused Weapon (SFW)

Evolved Expendable Launch Vehicle (EELV) 

LGM-30G Minuteman III 

Medium Launch Vehicle (MLV) 

Allied Signal Aerospace 

Evolved Expendable Launch Vehicle (EELV) 

Allison Transmissions

Halvorsen (formerly Next Generation Small Loader (NGSL))

Systems by Contractor

THE AIR FORCE HANDBOOK 2007 287
288 UNITED STATES AIR FORCE

Systems by Contractor

ARINC

C-5 Galaxy

KC-10 Extender 

Arrowhead Products 

Evolved Expendable Launch Vehicle (EELV) 

ASR 

Launch & Test Range System (LTRS) 

ATK Aerospace

Rocket Systems Launch Program (RSLP)

ATK Mission Research , Integrated Systems 

C-130H Scathe View 

RC-26B

Aurora Flight Systems

RQ-4 Global Hawk

Ball Aerospace

National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

Space Radar (SR)

Space Situation Awareness (SSA) Systems

Space Test Program (STP) 

Transformational Satellite Communications System (TSAT)

BAE 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS)

Air Force Combat Identification (AFCID )

EC-130H COMPASS CALL 

F16-TARS (Theater Airborne Reconnaissance System)

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter

Military Satellite Communication (MILSATCOM) Terminals 

Mission Planning Systems (MPS)

Space Radar (SR)

U-2S Dragon Lady

Bell Helicopter Company

UH-1N Helicopter (Variants: UH-1N, 1H/Vm UV-18B) 

BEA 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

Bell-Boeing

CV-22B 
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B.F. Goodrich 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

C-5 Galaxy

Evolved Expendable Launch Vehicle (EELV) 

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)

Boeing

AC-130H Spectre 

AC-130U Spooky 

AGM-86 B Air Launched Cruise Missile (ALCM)

AGM-86 C/D Conventional Air Launched Cruise Missile (CALCM)

AGM-130 Standoff Attack Weapon

Air Force Combat Identification (AFCID )

Airborne Laser (ABL)

B-1B Lancer

C-17 Globemaster III

C-32A

C-40B/C

Combat Survivor Evader Locator (CSEL)

Combatant Commanders Integrated Command and Control System (CCIC2S)

E-8C Joint STARS 

F-15A-D Eagle

F-15E Strike Eagle 

F-22A Raptor

GBU-31, GBU-32, GBU-38--Joint Direct Attack Munition (JDAM)

GBU-39/B Small Diameter Bomb (SDB) 

Global Positioning System (GPS)

Joint Helmet Mounted Cueing System (JHMCS)

KC-10 Extender 

KC-135 Stratotanker 

Launch & Test Range System (LTRS) 

LGM-30G Minuteman III 

MC-130E Combat Talon 

MC-130H Combat Talon II 

MC-130P Combat Shadow 

Military Satellite Communication (MILSATCOM) Terminals 

Mission Planning Systems (MPS)

RC-135S Cobra Ball 

RC-135U Combat Sent 

RC-135V/W Rivet Joint 

Space Radar (SR)

Space Situation Awareness (SSA) Systems

Space Test Program (STP) 

T-38A/AT-38B/T-38C Talon 
290 UNITED STATES AIR FORCE

Systems by Contractor

T-43A 

WC-135 Constant Phoenix 

Boeing Aerospace Company

E-3 Airborne Warning and Control System (AWACS)

Boeing Aerospace Operations

E-4B National Airborne Operations Center (NAOC)

Boeing Aircraft

B-52H Stratofortress

Boeing Integrated Defense System

VC-25A 

Boeing Satellite Systems

National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

Boeing Space & Intelligence Systems

Transformational Satellite Communications System (TSAT)

Boeing Wichita Development and Modernization Center (KS)

E-4B National Airborne Operations Center (NAOC)

Booz Allen Hamilton

Space Radar (SR)

Transformational Satellite Communications System (TSAT)

Carbon Advanced Technologies, Inc

Hypersonic Technology Vehicle (HTV)

Carondolet Foundry

Tunner 60K Loader

CDI Corp 

Launch & Test Range System (LTRS) 

Cessna

T-37B Tweet 

CFM International

C-40B/C

Chelton Microwave

Global Broadcast Service (GBS)

Cincinnati Electronics

Evolved Expendable Launch Vehicle (EELV) 

Cisco

Space Radar (SR)
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contractor

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Clover Hydraulics 

Halvorsen (formerly Next Generation Small Loader (NGSL))

Coleman Research

Rocket Systems Launch Program (RSLP)

Commercial Intertech

Tunner 60K Loader

Computer Science Corp.

Combatant Commanders Integrated Command and Control System (CCIC2S)

Computer Sciences Corp./ADP

C-21A

Computer Sciences Corp Federal Sector Defense Group

Deliberate Crisis and Action Planning and Execution Segments (DCAPES)

Computer Sciences/Raytheon

Launch & Test Range System (LTRS)

Contraves 

Evolved Expendable Launch Vehicle (EELV) 

Launch & Test Range System (LTRS) 

Cubic

E-8C Joint STARS 

Dallas Airmotive

C-20B/H

C-21A

Dana Corporation

Halvorsen (formerly Next Generation Small Loader (NGSL))

Day & Zimmerman Inc

CBU-97/105 Sensor Fused Weapon (SFW)

DCS Corp

Launch & Test Range System (LTRS) 

Delta Velocity Corporation

Operationally Responsive Space (ORS)

Design Develop

Space Radar (SR)

Detroit Diesel

Tunner 60K Loader

Halvorsen (formerly Next Generation Small Loader (NGSL))
292 UNITED STATES AIR FORCE

Diligent

Space Radar (SR)

Digital Net (BAE-IT)

Combatant Commanders Integrated Command and Control System (CCIC2S)

Dolphin 

Launch & Test Range System (LTRS) 

DRC

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

DRS Technologies, Inc

Tunner 60K Loader

E-Spectrum

AGM-86 B Air Launched Cruise Missile (ALCM)

AGM-129 A Advanced Cruise Missil e (ACM)

Eagle Pitcher

Space Radar (SR)

EJM

MH-53J/M Pave Low III/IV

Elbit Systems (Israel)

Joint Helmet Mounted Cueing System (JHMCS)

EMD

A-10/OA-10 Thunderbolt II 

ENSCO 

Launch & Test Range System (LTRS) 

Excel 

Launch & Test Range System (LTRS) 

Fairfield Manufacturing

Tunner 60K Loader

Fiber Innovations

Joint Air-to-Surface Standoff Missile (JASSM) 

Flight Safety Services Corp

T-6A Texan II 

FMC Technologies Inc.

Halvorsen (formerly Next Generation Small Loader (NGSL))

Systems by Contractor
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Ford Aerospace

AIM-9M Sidewinder

Freescale Semiconductor Inc 

Launch & Test Range System (LTRS) 

GDE Systems 

Evolved Expendable Launch Vehicle (EELV) 

General Atomics – Aeronautical Systems Incorporated

MQ-1 Predator

MQ-9 Reaper 

General Electric

B-1B Lancer

C-5 Galaxy

F-16 Fighting Falcon 

F-117 Nighthawk 

KC-10 Extender 

KC-135 Stratotanker 

RC-135S Cobra Ball 

RC-135U Combat Sent 

RC-135V/W Rivet Joint 

T-38A/AT-38B/T-38C Talon 

U-2S Dragon Lady

General Electric/Rolls-Royce Fighter Engine Team

F-35 Lightning II, Joint Strike Fighter 

General Dynamics 

AIM-7M Sparrow

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

CBU-89/104 Gator

EC-130H COMPASS CALL 

CBU-97/105 Sensor Fused Weapon (SFW)

Space Radar (SR)

General Technology Corporation

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMDER)

GKN Aerospace

C-130J

GTSI

Global Broadcast Service (GBS)
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Gulfstream

C-37A

Harris Corp.

Counterspace Systems 

Global Positioning System (GPS)

Space Radar (SR)

WC-135 Constant Phoenix 

Wideband Global SATCOM (WGS) System 

Hi Shear

CBU-97/105 Sensor Fused Weapon (SFW)

HMX

Operationally Responsive Space (ORS)

Honeywell

B-52H Stratofortress

C-5 Galaxy

CBU-87/103 Combined Effects Munition (CEM)

CBU-89/104 Gator

Evolved Expendable Launch Vehicle (EELV) 

F-15A-D Eagle

F-15E Strike Eagle 

LGM-30G Minuteman III 

Medium Launch Vehicle (MLV) 

Operationally Responsive Space (ORS)

Space Radar (SR)

Honeywell Aerospace Electronic Systems/ Olathe

T-6A Texan II 

Honeywell International

F-16 Fighting Falcon 

Honeywell Military Avionics

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMDER)

Honeywell Technical Services, Inc.

Air Force Satellite Control Network (AFSCN)

Hughes Space 

Launch & Test Range System (LTRS) 

IBM

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

Systems by Contractor
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InDyne, Inc

Launch & Test Range System (LTRS) 

Integral Systems, Inc.

Counterspace Systems 

Defense Meteorological Satellite Program (DMSP)

Integrated Data Systems

Space Radar (SR)

Integrity Applications Incorporated

Space Radar (SR)

Interstate Electronics Corp

Combat Survivor Evader Locator (CSEL)

Israel Aircraft Industries

F-16 Fighting Falcon 

ISS

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

ITT Avionics

CV-22B

ITT Industries

B-52H Stratofortress

Launch & Test Range System (LTRS) 

National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

Space Situation Awareness (SSA) Systems

Wideband Global SATCOM (WGS) System 

Jackson & Tull

Operationally Responsive Space (ORS)

Johns Hopkins APL

Operationally Responsive Space (ORS)

Johnstown Welding & Fabrication

Halvorsen (formerly Next Generation Small Loader (NGSL))

KAMAG

Evolved Expendable Launch Vehicle (EELV) 

Keystone Engineering 

Evolved Expendable Launch Vehicle (EELV) 

Klune 

Joint Air-to-Surface Standoff Missile (JASSM)
296 UNITED STATES AIR FORCE

Kodak 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

KSS (Kelly’s Logistics Support Services) Scitor

Launch & Test Range System (LTRS)

Kurt Manufacturing

CBU-97/105 Sensor Fused Weapon (SFW)

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMDER)

L-3 Communications 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

C-130 SENIOR SCOUT

E-4B National Airborne Operations Center (NAOC)

EC-130H COMPASS CALL 

F16-TARS (Theater Airborne Reconnaissance System)

F-117 Nighthawk 

Launch & Test Range System (LTRS) 

MC-130E Combat Talon 

MC-130H Combat Talon II 

MQ-1 Predator

MQ-9 Reaper 

Operationally Responsive Space (ORS)

RC-135S Cobra Ball 

RC-135U Combat Sent 

RC-135V/W Rivet Joint 

RQ-4 Global Hawk

U-2S Dragon Lady

WC-135 Constant Phoenix 

L-3 Communications Telemetry 

Joint Air-to-Surface Standoff Missile (JASSM) 

L-3 Communications/Vertex Aerospace

C-12C/D/F/J

La Barge 

Evolved Expendable Launch Vehicle (EELV) 

Lincoln Composites 

Evolved Expendable Launch Vehicle (EELV) 

Linde Hydraulics

Tunner 60K Loader

Systems by Contractor
Syste

ms 

by 

contractor

THE AIR FORCE HANDBOOK 2007 297

Lockheed Martin 

AC-130H Spectre 

Advanced Extremely High Frequency (AEHF) System 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

A-10/OA-10 Thunderbolt II 

Airborne Laser (ABL)

C-5 Galaxy

C-130J

C-9C

Combatant Commanders Integrated Command and Control System (CCIC2S)

Defense Meteorological Satellite Program (DMSP)

F-16 Fighting Falcon 

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter 

F-117 Nighthawk 

GBU-31, GBU-32, GBU-38--Joint Direct Attack Munition (JDAM)

Global Positioning System (GPS)

HC-130P/N King 

Hypersonic Technology Vehicle (HTV)

Joint Air-to-Surface Standoff Missile (JASSM) 

Launch & Test Range System (LTRS) 

LGM-30G Minuteman III 

MC-130E Combat Talon 

MC-130H Combat Talon II 

MC-130P Combat Shadow 

MH-53J/M Pave Low III/IV 

Military Satellite Communication (MILSATCOM) Terminals 

Mission Planning Systems (MPS)

Rocket Systems Launch Program (RSLP)

Space Radar (SR)

U-2S Dragon Lady

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMDER)

Lockheed Martin Aeronautics Company

C-130 Hercules

Lockheed Martin Integrated Systems & Solutions

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

C-130 SENIOR SCOUT

Space Based Infrared System High (SBIRS High)

Theater Battle Management Control Systems (TBMCS)

Transformational Satellite Communications System (TSAT)
298 UNITED STATES AIR FORCE

Lockheed Martin Missiles and Space 

Defense Satellite Communications System (DSCS) III

Military Strategic and Tactical Relay (Milstar) 

Lockheed Martin Space Systems

Space Based Infrared System High (SBIRS High) 

Transformational Satellite Communications System (TSAT)

Lockheed Martin Tactical Aircraft Systems

Launch & Test Range System (LTRS) 

Lockheed Martin Technical Operations 

Launch & Test Range System (LTRS) 

Logicon

Wideband Global SATCOM (WGS) System 

M7 Aerospace

C-20B/H

RC-26B

Martin Baker Aircraft/Middlesex

T-6A Texan II 

T-38A/AT-38B/T-38C Talon 

Marvin Engineering 

AGM-65 Maverick

MEI

Space Radar (SR)

Minco

Space Radar (SR)

MIT Lincoln Laboratory

Space Situation Awareness (SSA) Systems

Mitre Corp (MA)

Regional Sector Air Operations Center (RSAOC)

Mitsubishi Heavy Industries 

Evolved Expendable Launch Vehicle (EELV) 

Moog Inc. 

AGM-65 Maverick

Evolved Expendable Launch Vehicle (EELV) 

Space Radar (SR)

Systems by Contractor
Syste

ms 

by 

contractor

THE AIR FORCE HANDBOOK 2007 299

MTC

MH-53J/M Pave Low III/IV 

Muniz Engineering

Space Test Program (STP) 

Net Acquire 

Launch & Test Range System (LTRS) 

Northrop Grumman 

Advanced Extremely High Frequency (AEHF) System 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

Air Force Combat Identification (AFCID )

A-10/OA-10 Thunderbolt II 

Airborne Laser (ABL)

B-1B Lancer

B-2 Spirit

Defense Meteorological Satellite Program (DMSP)

Defense Support Program (DSP) 

Distributed Mission Operations (DMO)

E-3 Airborne Warning and Control System (AWACS)

E-8C Joint STARS 

F-15A-D Eagle

F-15E Strike Eagle 

F-16 Fighting Falcon 

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter 

Military Satellite Communication (MILSATCOM) Terminals 

Mission Planning Systems (MPS)

RQ-4 Global Hawk

Space Situation Awareness (SSA) Systems

Transformational Satellite Communications System (TSAT)

T-38A/AT-38B/T-38C Talon 

U-2S Dragon Lady

Northrop Grumman Electronic Systems

Combatant Commanders Integrated Command and Control System (CCIC2S)

Space Based Infrared System High (SBIRS High) 

Space Radar (SR)

Northrop Grumman Mission Systems

LGM-30G Minuteman III 

Northrop Grumman Space Technology

National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

Space Radar (SR)
300 UNITED STATES AIR FORCE

NPO Enerogomash 

Evolved Expendable Launch Vehicle (EELV) 

Orbital Sciences Corporation

Operationally Responsive Space (ORS)

Rocket Systems Launch Program (RSLP)

Orion Propulsion

Operationally Responsive Space (ORS)

Pacific Scientific

CBU-97/105 Sensor Fused Weapon (SFW)

Parker Hanifin

Tunner 60K Loader

Partners in Air and Space

Space Radar (SR)

PEMCO

KC-135 Stratotanker 

Pioneer Aerospace

CBU-97/105 Sensor Fused Weapon (SFW)

Pratt & Whitney

B-52H Stratofortress

C-12C/D/F/J

C-17 Globemaster III

C-32A

Evolved Expendable Launch Vehicle (EELV) 

F-15A-D Eagle

F-15E Strike Eagle 

F-16 Fighting Falcon 

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter 

KC-135 Stratotanker 

Medium Launch Vehicle (MLV) 

WC-135 Constant Phoenix 

Pratt & Whitney Canada

T-6A Texan II 

Praxis

Operationally Responsive Space (ORS)

Systems by Contractor
Syste

ms 

by 

contractor

THE AIR FORCE HANDBOOK 2007 301

Raytheon 

AN/GSQ -272 AIR FORCE DISTRIBUTED COMMON GROUND SYSTEM (AFDCGS) 

AGM-65 Maverick

AGM-129 A Advanced Cruise Missil e (ACM)

AIM-9X Sidewinder

AIM-9M Sidewinder

AGM-88 High Speed Anti-Radiation Missile (HARM)

AIM-120 (AMRAAM) Advanced Medium Range Air-to-Air Missile

AIM-7M Sparrow

Air Force Combat Identification (AFCID )

CV-22B

E-4B National Airborne Operations Center (NAOC)

F-15A-D Eagle

F-15E Strike Eagle 

F-16 Fighting Falcon 

LGM-30G Minuteman III 

MC-130E Combat Talon 

MH-53J/M Pave Low III/IV 

MQ-1 Predator

MQ-9 Reaper 

National Polar-orbiting Operational Environmental Satellite System (NPOESS) 

Operationally Responsive Space (ORS)

RQ-4 Global Hawk

Space Radar (SR)

T-1A Jayhawk 

T-6A Texan II 

Transformational Satellite Communications System (TSAT)

U-2S Dragon Lady

WC-135 Constant Phoenix 

Raytheon Intelligence & Information Systems

Global Broadcast Service (GBS)

Raytheon Missile Systems

F-16 HARM Targeting System (HTS) R6 and R7

Raytheon Systems Corporation

EC-130H COMPASS CALL 

Raytheon Technology Services

Global Broadcast Service (GBS)

Raytheon-Texas Instruments

F-117 Nighthawk 
Systems by Contractor

302 UNITED STATES AIR FORCE

Reynard Corp

CBU-97/105 Sensor Fused Weapon (SFW)

Robinson & Robinson

Launch & Test Range System (LTRS) 

Rocketdyne

Medium Launch Vehicle (MLV) 

Rockwell

Military Satellite Communication (MILSATCOM) Terminals 

Rockwell Automation

E-4B National Airborne Operations Center (NAOC)

Rockwell Collins

AC-130H Spectre 

AC-130U Spooky 

E-8C Joint STARS 

GBU-31, GBU-32, GBU-38--Joint Direct Attack Munition (JDAM)

Joint Helmet Mounted Cueing System (JHMCS)

KC-135 Stratotanker 

MC-130E Combat Talon 

MC-130H Combat Talon II 

MC-130P Combat Shadow 

Rolls Royce

C-130J

C-20B/H

CV-22B

C-37A

F-35 Lightning II, Joint Strike Fighter 

RQ-4 Global Hawk

RT Logic 

Launch & Test Range System (LTRS) 

SAIC

AN/USQ -163 Falconer Air and Space Operations Center Weapon System (AOC-WS)

Deliberate Crisis and Action Planning and Execution Segments (DCAPES)

Mission Planning Systems (MPS)

Space Radar (SR)

Wideband Global SATCOM (WGS) System 
Syste

ms 

by 

contractor

THE AIR FORCE HANDBOOK 2007 303

SEAKR

Operationally Responsive Space (ORS)

Space Radar (SR)

SEI

AC-130H Spectre 

AC-130U Spooky 

MC-130H Combat Talon II 

Senior Systems Technology

Combat Survivor Evader Locator (CSEL)

Sensis Group 

Control and Reporting Center (CRC)

Sheldahl

Space Radar (SR)

Sierra Nevada Corporation

C-130 SENIOR SCOUT

RC-135U Combat Sent 

Sikorsky

HH-60G Pave Hawk

MH-53J/M Pave Low III/IV

Smith Aerospace 

C-130J

Smith Electric

Launch & Test Range System (LTRS) 

Smiths Aerospace Electronic Systems/Cheltenham 

T-6A Texan II 

Space Vector Corporation

Operationally Responsive Space (ORS)

Rocket Systems Launch Program (RSLP)

Space-X

Operationally Responsive Space (ORS)

Rocket Systems Launch Program (RSLP)

Spectrum Astro

Space Radar (SR)

Space Test Program (STP)

SRI International

Launch & Test Range System (LTRS) 
Systems by Contractor

304 UNITED STATES AIR FORCE

SRS Technologies

Space Radar (SR)

Stennis

Space Radar (SR)

Superior 

Launch & Test Range System (LTRS)

Swales Aerospace

Operationally Responsive Space (ORS)

Space Radar (SR)

System Integration

A-10/OA-10 Thunderbolt II 

Technology Services Corp.

Control and Reporting Center (CRC)

Tecolote

Space Radar (SR)

Teledyne Continental Engine

Joint Air-to-Surface Standoff Missile (JASSM) 

Textron

GBU-31, GBU-32, GBU-38--Joint Direct Attack Munition (JDAM)

CBU-97/105 Sensor Fused Weapon (SFW)

RC-135S Cobra Ball 

Thales Raytheon

Control and Reporting Center (CRC)

Regional Sector Air Operations Center (RSAOC)

Thales Communications

Combat Survivor Evader Locator (CSEL)

Thiokol

Medium Launch Vehicle (MLV) 

TRAK Microwave 

Launch & Test Range System (LTRS) 

Tundra Semiconductor

CBU-97/105 Sensor Fused Weapon (SFW)

Tybrin Corp

Mission Planning Systems (MPS)
Syste

ms 

by 

contractor

THE AIR FORCE HANDBOOK 2007 305

United Engineering Co

Evolved Expendable Launch Vehicle (EELV) 

United Launch Alliance

Evolved Expendable Launch Vehicle (EELV)

Medium Launch Vehicle (MLV) 

Universal Space Lines LLC

Operationally Responsive Space (ORS)

U.S. Naval Research Laboratory

Operationally Responsive Space (ORS)

Verizon

Transformational Satellite Communications System (TSAT)

Viasat

Global Broadcast Service (GBS)

Vision Systems International

Joint Helmet Mounted Cueing System (JHMCS)

Volt 

Launch & Test Range System (LTRS) 

Vought Aircraft

C-17 Globemaster III

RQ-4 Global Hawk 

Williams International

Joint Air-to-Surface Standoff Missile (JASSM) 

Wyman-Gordon Forgings

Joint Air-to-Surface Standoff Missile (JASSM) 

Syste

ms 

by state o

f M

a

nufac

t

ure

THE AIR FORCE HANDBOOK 2007 307

Systems by State Of Manufacture

Alabama

C-5 Galaxy

Evolved Expendable Launch Vehicle (EELV)

Joint Air-to-Surface Standoff Missile (JASSM)

KC-135 Stratotanker

Medium Launch Vehicle (MLV)

Operationally Responsive Space (ORS)

Arizona

AGM-65 Maverick

AGM-88 High Speed Anti-Radiation Missile (HARM)

AGM-129 A Advanced Cruise Missile (ACM)

AIM-7M Sparrow

AIM-9M Sidewinder

AIM-9X Sidewinder

AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM)

 AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

CBU-97/105 Sensor Fused Weapon (SFW)

Evolved Expendable Launch Vehicle (EELV)

F-16 HARM Targeting System (HTS) R6 and R7

Operationally Responsive Space (ORS)

Rocket Systems Launch Program (RSLP)

Space Radar (SR)

Space Test Program (STP)

Arkansas

Evolved Expendable Launch Vehicle (EELV)

California

Advanced Extremely High Frequency (AEHF) System

AGM-130 Standoff Attack Weapon

Air Force Combat Identification (AFCID )

Airborne Laser (ABL)

AN/GSQ-272 Air Force Distributed Common Ground System (AF DCGS)

B-1B Lancer

B-2 Spirit

C-17 Globemaster III

CBU-89/104 Gator

CBU-97/105 Sensor Fused Weapon (SFW)

Combatant Commanders Integrated Command and Control System (CCIC2S)

Combat Survivor Evader Locator (CSEL)

Control and Reporting Center (CRC)

Defense Meteorological Satellite Program (DMSP)

Defense Support Program (DSP)

EC-130H Compass Call

Evolved Expendable Launch Vehicle (EELV)

F-15A-D Eagle

F-15E Strike Eagle

F-16 Fighting Falcon
systems by state of Manufacture

308 UNITED STATES AIR FORCE

F-35 Lightning II, Joint Strike Fighter

F-117 Nighthawk

Global Positioning System (GPS)

Hypersonic Technology Vehicle (HTV)

Joint Helmet Mounted Cueing System (JHMCS)

KC-10 Extender

Launch & Test Range System (LTRS)

Medium Launch Vehicle (MLV)

Military Satellite Communication (MILSATCOM) Terminals

MQ-1 Predator

MQ-9 Reaper

National Polar-orbiting Operational Environmental Satellite System (NPOESS)

Operationally Responsive Space (ORS)

Regional Sector Air Operations Center (RSAOC)

Rocket Systems Launch Program (RSLP)

RQ-4 Global Hawk

Space Based Infrared System High (SBIRS High)

Space Radar (SR)

Space Situation Awareness (SSA) Systems

T-38A/AT-38B/T-38C Talon

Transformational Satellite Communications System (TSAT)

U-2S Dragon Lady

Wideband Global SATCOM (WGS) System

Colorado

Air Force Satellite Control Network (AFSCN)

Air Force Weather Weapon System (AFWWS)

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

C-130 SENIOR SCOUT 

Combatant Commanders Integrated Command and Control System (CCIC2S)

Evolved Expendable Launch Vehicle (EELV)

Launch & Test Range System (LTRS)

Medium Launch Vehicle (MLV)

National Polar-orbiting Operational Environmental Satellite System (NPOESS)

Operationally Responsive Space (ORS)

Space Based Infrared System High (SBIRS High)

Space Radar (SR)

Space Situation Awareness (SSA) Systems

Space Test Program (STP)

T-6A Texan II

Theater Battle Management Control Systems (TBMCS)

Transformational Satellite Communications System (TSAT)

Wideband Global SATCOM (WGS) System

Connecticut

C-17 Globemaster III

C-32A

CBU-97/105 Sensor Fused Weapon (SFW)
Syste

ms 

by state o

f M

a

nufac

t

ure

THE AIR FORCE HANDBOOK 2007 309

F-15A-D Eagle

F-15E Strike Eagle

F-16 Fighting Falcon

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter

HH-60G Pave Hawk

MH-53J/M Pave Low III/IV

Space Radar (SR)

WC-135 Constant Phoenix

District of Columbia

Operationally Responsive Space (ORS)

Florida

AC-130H Spectre

AC-130U Spooky

AIM-7M Sparrow

AIM-9M Sidewinder

B-52H Stratofortress

C-9C

CBU-89/104 Gator

Counterspace Systems

Distributed Mission Operations (DMO)

E-4B National Airborne Operations Center (NAOC)

E-8C Joint STARS

Evolved Expendable Launch Vehicle (EELV)

Global Positioning System (GPS)

Halvorsen (formerly Next Generation Small Loader (NGSL))

Joint Air-to-Surface Standoff Missile (JASSM)

Launch & Test Range System (LTRS)

LGM-30G Minuteman III

Military Satellite Communication (MILSATCOM) Terminals

MC-130E Combat Talon

MC-130H Combat Talon II

MC-130P Combat Shadow

Medium Launch Vehicle (MLV)

MH-53J/M Pave Low III/IV

Rocket Systems Launch Program (RSLP)

Space Radar (SR)

Space Test Program (STP)

UH-1N Helicopter (Variants: UH-1N, 1H/Vm UV-18B)

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)

Georgia

C-5 Galaxy

C-130J

C-37A

 F-22A Raptor
systems by state of Manufacture

310 UNITED STATES AIR FORCE

MC-130E Combat Talon

MC-130H Combat Talon II

MH-53J/M Pave Low III/IV

U-2S Dragon Lady

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)

Illinois

F-15A-D Eagle

F-15E Strike Eagle

Indiana

C-130J

CV-22B

EC-130H Compass Call

F-35 Lightning II, Joint Strike Fighter

Halvorsen (formerly Next Generation Small Loader (NGSL))

Military Satellite Communication (MILSATCOM) Terminals

National Polar-orbiting Operational Environmental Satellite System (NPOESS)

RQ-4 Global Hawk

Iowa

AC-130H Spectre

AC-130U Spooky

GBU-31/ GBU-32/ GBU-38 Joint Direct Attack Munition (JDAM)

MC-130E Combat Talon

MC-130H Combat Talon II

MC-130P Combat Shadow

Military Satellite Communication (MILSATCOM) Terminals

Kansas

Airborne Laser (ABL)

B-52H Stratofortress

CBU-97/105 Sensor Fused Weapon (SFW)

E-4B National Airborne Operations Center (NAOC)

KC-135 Stratotanker

RC-135S Cobra Ball

RC-135U Combat Sent

RC-135V/W Rivet Joint

T-1A Jayhawk

T-6A Texan II

T-37B Tweet

Louisiana

E-8C Joint STARS

Evolved Expendable Launch Vehicle (EELV)

Maine

CBU-97/105 Sensor Fused Weapon (SFW)
Syste

ms 

by state o

f M

a

nufac

t

ure

THE AIR FORCE HANDBOOK 2007 311

Maryland

Air Force Combat Identification (AFCID )

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

B-1B Lancer

C-5 Galaxy

C-130 Hercules

Combat Survivor Evader Locator (CSEL)

Control and Reporting Center (CRC)

Counterspace Systems

Defense Meteorological Satellite Program (DMSP)

E-3 Sentry Airborne Warning and Control System (AWACS)

F-16 Fighting Falcon

F-22A Raptor

Global Broadcast Service (GBS)

Operationally Responsive Space (ORS)

Space Radar (SR)

Massachusetts

AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM)

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

AN/USQ -163 Air Force Distributed Common Ground System (AOC-WS)

CBU-97/105 Sensor Fused Weapon (SFW)

F-117 Nighthawk

GBU-31/ GBU-32/ GBU-38 Joint Direct Attack Munition (JDAM)

Global Broadcast Service (GBS)

Joint Air-to-Surface Standoff Missile (JASSM)

LGM-30G Minuteman III

Military Satellite Communication (MILSATCOM) Terminals

Regional Sector Air Operations Center (RSAOC)

Space Radar (SR)

Space Situation Awareness (SSA) Systems

T-38A/AT-38B/T-38C Talon

Transformational Satellite Communications System (TSAT)

Michigan

Halvorsen (formerly Next Generation Small Loader (NGSL))

Joint Air-to-Surface Standoff Missile (JASSM)

Space Radar (SR)

Tunner 60K Loader

Minnesota

CBU-87/103 Combined Effects Munition (CEM)

CBU-89/104 Gator

CBU-97/105 Sensor Fused Weapon (SFW)

F-16 Fighting Falcon

GBU-31/ GBU-32/ GBU-38 Joint Direct Attack Munition (JDAM)

Space Radar (SR)

Tunner 60K Loader

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)
systems by state of Manufacture

312 UNITED STATES AIR FORCE

Mississippi

C-12C/D/F/J

F-15A-D Eagle

F-15E Strike Eagle

RQ-4 Global Hawk

Space Radar (SR)

Missouri

AC-130H Spectre

AC-130U Spooky

AGM-86 C/D Conventional Air Launched Cruise Missile (CALCM)

C-17 Globemaster III

Evolved Expendable Launch Vehicle (EELV)

F-15A-D Eagle

F-15E Strike Eagle

GBU-31/ GBU-32/ GBU-38 Joint Direct Attack Munition (JDAM)

GBU-39/B Small Diameter Bomb (SDB)

Joint Helmet Mounted Cueing System (JHMCS)

MC-130H Combat Talon II

Space Radar (SR)

T-38A/AT-38B/T-38C Talon

Tunner 60K Loader

Nebraska

Air Force Weather Weapon System (AFWWS)

Evolved Expendable Launch Vehicle (EELV)

New Hampshire

EC-130H COMPASS CALL

F-22A Raptor

Military Satellite Communication (MILSATCOM) Terminals

New Jersey

B-52H Stratofortress

CV-22B

F-16 Fighting Falcon 

GBU-31/ GBU-32/ GBU-38 Joint Direct Attack Munition (JDAM)

New Mexico

C-5 Galaxy

Evolved Expendable Launch Vehicle (EELV)

F-15A–D Eagle

F-15E Strike Eagle

F-16 Fighting Falcon

Operationally Responsive Space (ORS)

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)

New York

A-10/OA-10 Thunderbolt II

Air Force Combat Identification (AFCID)
Syste

ms 

by state o

f M

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t

ure

THE AIR FORCE HANDBOOK 2007 313

 AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

Control and Reporting Center (CRC)

Evolved Expendable Launch Vehicle (EELV)

F16-TARS (Theater Airborne Reconnaissance System)

Launch & Test Range System (LTRS)

Nevada

C-130 SENIOR SCOUT

Operationally Responsive Space (ORS)

RC-135U Combat Sent

North Carolina

C-5 Galaxy

Ohio

B-1B Lancer

Evolved Expendable Launch Vehicle (EELV)

F-16 Fighting Falcon

F-35 Lightning II, Joint Strike Fighter

Joint Air-to-Surface Standoff Missile (JASSM)

LGM-30G Minuteman III

RC-135S Cobra Ball

RC-135U Combat Sent Tunner 60K Loader

U-2S Dragon Lady

Oklahoma

E-4B National Airborne Operations Center (NAOC)

KC-10 Extender

KC-135 Stratotanker

VC-25A

Pennsylvania

CV-22B

Global Positioning System (GPS)

Halvorsen (formerly Next Generation Small Loader (NGSL))

Hypersonic Technology Vehicle (HTV)

Joint Air-to-Surface Standoff Missile (JASSM)

LGM-30G Minuteman III

Space Radar (SR)

South Carolina

C-9C

HC-130P/N King

MC-130E Combat Talon

MC-130H Combat Talon II

MC-130P Combat Shadow

Texas

AGM-65 Maverick

AGM-86 B Air Launched Cruise Missile (ALCM)
systems by state of Manufacture

314 UNITED STATES AIR FORCE

AGM-129A Advanced Cruise Missile (ACM)

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

C-17 Globemaster III

C-20B/H

C-21A 

C-130 SENIOR SCOUT

C-130H Scathe View

CV-22B

E-4B National Airborne Operations Center (NAOC)

Evolved Expendable Launch Vehicle (EELV)

F-16 Fighting Falcon

F-22A Raptor

F-35 Lightning II, Joint Strike Fighter

F-117 Nighthawk

Hypersonic Technology Vehicle (HTV)EC-130H COMPASS CALL

Joint Air-to-Surface Standoff Missile (JASSM)

Joint Helmet Mounted Cueing System (JHMCS)

KC-10 Extender

KC-135 Stratotanker

Launch & Test Range System (LTRS)

MC-130E Combat Talon

MC-130H Combat Talon II

Medium Launch Vehicle (MLV)

MH-53J/M Pave Low III/IV

MQ-1 Predator

MQ-9 Reaper

RC-26B

RC-135S Cobra Ball

RC-135U Combat Sent

RC-135V/W Rivet Joint

RQ-4 Global Hawk

Space Radar (SR)

Space Test Program (STP)

UH-1N Helicopter (Variants: UH-1N, 1H/Vm UV-18B)

WC-135 Constant Phoenix

Utah

AGM-65 Maverick 

AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM)

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

C-130 SENIOR SCOUT

F16-TARS (Theater Airborne Reconnaissance System)

Joint Air-to-Surface Standoff Missile (JASSM)

LGM-30G Minuteman III

Medium Launch Vehicle (MLV)

Military Satellite Communication (MILSATCOM) Terminals

MQ-1 Predator

MQ-9 Reaper

314 UNITED STATES AIR FORCE
Syste

ms 

by state o

f M

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ure

THE AIR FORCE HANDBOOK 2007 315

Operationally Responsive Space (ORS)

Rocket Systems Launch Program (RSLP)

RQ-4 Global Hawk

U-2S Dragon Lady

Vermont

U-2S Dragon Lady

Wind Corrected Munitions Dispenser (WCMD) and WCMD-Extended Range (WCMD-ER)

Virginia

AN/GSQ -272 Air Force Distributed Common Ground System (AF DCGS)

AN/USQ -163 Air Force Distributed Common Ground System (AOC-WS)

Combatant Commanders Integrated Command and Control System (CCIC2S)

Deliberate Crisis and Action Planning and Execution Segments (DCAPES)

Global Broadcast Service (GBS)

Military Satellite Communication (MILSATCOM) Terminals

Operationally Responsive Space (ORS)

RQ-4 Global Hawk

Space Radar (SR)

Space Test Program (STP)

Transformational Satellite Communications System (TSAT)

U-2S Dragon Lady

Washington

AGM-86 B Air Launched Cruise Missile (ALCM)

Air Force Combat Identification (AFCID )

C-32A

C-40B/C

CBU-97/105 Sensor Fused Weapon (SFW)

E-3 Sentry Airborne Warning and Control System (AWACS)

F-22A Raptor

Launch & Test Range System (LTRS)

Operationally Responsive Space (ORS)

T-43A

WC-135 Constant Phoenix

West Virginia

C-12C/D/F/J

CBU-97/105 Sensor Fused Weapon (SFW)

RQ-4 Global Hawk

T-6A Texan II

Wisconsin

CBU-97/105 Sensor Fused Weapon (SFW)

Halvorsen (formerly Next Generation Small Loader (NGSL))