F-22 Raptor

Product Type:

5th Generation Air Dominance Fighter

Using Service (US):

Air Force (USAF)

Program Status:

In Service - No new aircraft planned.

Prime Contractors:

Lockheed Martin Corporation
The Boeing Company
Engines: Pratt & Whitney (United Techn.)

Specifications Armament DoD Spending FY2015 Budget

The F-22 Raptor

About the F-22 Raptor:

The Lockheed Martin/Boeing F-22 Raptor is a twin-engine single-seat air dominance fighter. It is a first-of-a-kind multi-mission fighter aircraft that combines stealth, supercruise, advanced maneuverability, and integrated avionics to make it the world's most capable combat aircraft. The Raptor is a fifth generation fighter aircraft and is designed to penetrate enemy airspace and achieve a first-look, first-kill capability against multiple targets. The aircraft made its combat debut in Syria on September 22, 2014. The F-22 has unprecedented survivability and lethality, ensuring the joint forces have freedom from attack, freedom to maneuver, and freedom to attack. The U.S. Government has prohibited the sale of F-22 aircraft to any foreign nation.

The F-22 is powered by two Pratt & Whitney F119-PW-100 afterburning turbofan engines, each providing 35,000 pounds of thrust. Supercruise (the ability to operate at supersonic speed without afterburning) gives the aircraft exceptional combat performance without compromising mission range. The aircraft's Northrop Grumman AN/APG-77 AESA radar system is able to detect enemy aircraft radar at distances of up to 285 miles (460 km). The AN/APG-77 system itself exhibits a very low radar cross section. The F-22's avionics package also includes the BAE Systems AN/ALR-94 radar warning receiver (RWR), the Lockheed Martin AN/AAR-56 MLD missile warning system (MWS), and BAE Systems AN/ALE-52 countermeasures dispenser. The cockpit features six full colour multifunction displays, including the 8x8" primary display from Kaiser Electronics (now Rockwell Collins). A BAE Systems head-up display (HUD) provides target status, weapon status, and weapon envelopes data and shoot cues. Also, a video camera records data for the HUD for post-mission analysis. The F-22 is equipped with the ACES II ejection seat system manufactured by Goodrich (now United Technologies). Goodrich also supplied the aircraft's landing gear.

In the production of the F-22, Lockheed Martin was responsible for program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets); the center fuselage; the leading edges of the wings; fins and stabilators; flaps; ailerons; landing gear; stores management; integrated navigation and electronic warfare systems; communications, navigation, and identification systems; the weapon support system; and final assembly of the aircraft. At its facilities in Seattle, Washington, Boeing built the wings and aft fuselage and was responsible for avionics integration, 70% of mission software, the training system, and life-support and fire-protection systems.

The F-22 is mainly made of titanium alloys and composites. Radar absorbent materials are used to reduce the aircraft's radar signature. Also, the shape of the F-22 makes it more difficult to detect on radar. The F-22's structural weight is comprised of 39% titanium alloys (highest in any U.S. aircraft design since the SR-71A), 24% composites, 16% aluminium alloys, and 1% thermoplastics - with other materials making up the remaining 20%. The wings are made of 42% titanium, 35% composites, and 23% aluminum and other materials (by structural weight).

The Advanced Tactical Fighter program (which would eventually bring about the F-22) entered the demonstration and validation phase in 1986. The prototype aircraft YF-22 and YF-23 completed their first flights in 1990 and the YF-22 was later selected as the best design. Engineering and manufacturing development efforts began in 1991 with contracts awarded to Lockheed Martin and Boeing for the airframe and Pratt & Whitney for the engines. Flight testing began in 1997 (first flight on September 7, 1997) and in 2001, the F-22 program was approved for low-rate initial production (LRIP). The first production F-22 was delivered to the Air Force in 2002. Initial operational and test evaluation was completed in 2004 and the following year, the program went into full rate production. The F-22 achieved initial operational capability in December 2005.

In December 2011, the 187th and final production F-22 Raptor came off the production line at Lockheed Martin's facility in Marietta, Georgia and was delivered to the Air Force on May 2, 2012. With the final aircraft complete, the F-22 production line will be shut down. Including flight test and initial production aircraft, a grand total of 195 F-22s have been built. As of September 2013, of the 182 aircraft in the Air Force inventory, 20 are assigned to Air National Guard units.

The F-22 program has struggled with an issue in the pilot oxygen supply system, which has been blamed for a series of incidents in which pilots struggled to breath and experienced dizziness and blackouts. In the worst incident, Air Force pilot Capt. Jeff Haney lost his life on November 16, 2010, when his F-22 crashed near Joint Base Elmendorf-Richardson in Alaska. To fix these problems, the Air Force is installing new valves on the pilot life-support system.

Lockheed Martin is currently under contract to modernize the F-22, which includes the development of system upgrades, additional capabilities and performance enhancements. The contract ceiling is $6.9 billion and covers work until February 2023.


The F-22 is equipped with a General Dynamics M61-A2 Vulcan 20mm six-barreled gatling gun and has four under-wing hardpoints and three internal weapons bays. The aircraft carries AIM-9M/X Sidewinder air-to-air missiles, AIM-120 AMRAAM air-to-air missiles, GBU-32 Joint Direct Attack Munitions (JDAM), and GBU-39/40 Small Diameter Bombs. For more detail, see specifications below.

Price/Unit Cost:

The F-22 is no longer in production. In 2007, the unit cost of the F-22A was $136.2 million ($148.7 million flyaway cost or $179.7 million incl. support costs). The airframe's cost was $87.74 million, the F119-PW-100 engine cost $10.03 million, and the avionics cost $28.36 million.


The F-22 provides an enhanced U.S. air superiority capability against projected threats and will replace the F-15 Eagle.

FY 2014 DoD F-22 Program:

FY 2014 continues critical F-22 modernization through incremental capability upgrades and key reliability and maintainability efforts. Procurement funds in the amount of $238.1M have been allocated for F-22 modifications, support equipment and spares. The primary modifications in FY 2014 are RAMMP, F119 Engine Modifications, the SRP, and Increment 3.2.

FY 2015 DoD F-22 Program:

FY 2015 continues critical F-22 modernization through incremental capability upgrades and key reliability and maintainability efforts to include the Reliability, Availability, and Maintainability Maturation Program (RAMMP), which provides for the development and integration of upgrades for F-22 aircraft to reach mature reliability, availability and maintainability. Procurement funds in the amount of $217.9M have been allocated for F-22 modifications, support equipment and spares.

FY 15 continues to retrofit the combat-coded F-22 fleet with Increment 3.1, which provides an initial ground attack kill chain capability via inclusion of emitter-based geolocation of threat systems, ground-looking synthetic aperture radar modes, electronic attack capability, and initial integration of the Small Diameter Bomb (SDB-1).

FY 15 continues development of Increment 3.2, providing Advanced Medium Range Air-to-Air Missile-120D and Air Intercept Missile-9X integration, radar electronic protection, enhanced speed and accuracy of target geo-location, intraflight data link improvements, Automatic Ground- Collision Avoidance System, and other enhancements to improve system safety and effectiveness. Supports advance procurement in FY 2015 to begin 3.2B retrofit.

For more information, you can access downloadable budget data in PDF format below.

Sources: U.S. Department of Defense (DoD), Lockheed Martin Corp.,
The Boeing Company, BAE Systems, Pratt & Whitney, and Northrop Grumman.

Last Update: September 24, 2014.

By Joakim Kasper Oestergaard /// (jkasper@bga-aeroweb.com)

External Resources:

Lockheed Martin: F-22 Raptor

Northrop Grumman: AN/APG-77 AESA Radar
Lockheed Martin: AN/AAR-56 MLD MWS
General Dynamics: M61-A2 20mm Vulcan Gatling Gun

YouTube: F-22 Raptor | YouTube Videos

Fact Sheet: Lockheed Martin | F-22 Fact Sheet
Product Card: Lockheed Martin | Raptor Product Card

F-22A U.S. Defense Budget Charts:

DoD Spending on the F-22-Raptor program in FY 2011, FY 2012, FY 2013, FY 2014 and FY 2015
DoD Purchases of F-22-Raptor Aircraft in FY 2011, FY 2012, FY 2013, FY 2014 and FY 2015
Defense Budget Data

Go to Top

DoD Spending, Procurement and RDT&E: FY 2011/12/13 + Budget for FYs 2014 + 2015

DoD Defense Spending, Procurement, Modifications, Spares, and RDT&E for the F-22-Raptor Defense Program

Download Official U.S. Department of Defense (DoD) Budget Data:

Purchases of F-22 Aircraft (USAF-2014) Modification of F-22 Aircraft (USAF) Increment 3.2B Mods (USAF)
Spares and Repair Parts (USAF)

Aircraft Specifications: F-22A Raptor

Go to Top

Primary Function: Air dominance multi-role fighter
Prime Contractors: Lockheed Martin Corp.; The Boeing Co.
Power Plant: 2x Pratt & Whitney F119-PW-100 turbofan engine with two-dimensional thrust vectoring nozzles
Thrust: 35,000 pounds (each engine)
Wingspan: 44 ft 6 in (13.6 m)
Length: 62 ft 1 in (18.9 m)
Height: 16 ft 8 in (5.1 m)
Weight (Empty): 43,340 lbs (19,700 kg)
Maximum Takeoff Weight (MTOW): 83,500 lbs (38,000 kg)
Fuel Capacity: Internal: 18,000 lbs (8,200 kg); with 2 external wing fuel tanks: 26,000 lbs (11,900 kg)
Payload: Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks
Speed: Max: Mach 2.25/1,303 kts/1,500 mph (2,414 km/h); Supercruise: Mach 1.82/1,060 kts/1,220 mph (1,964 km/h)
Service Ceiling: 65,000 ft (19,810 m)
Range: 1,600+ nm/1,841+ miles (2,963+ km) with 2 external wing fuel tanks
Combat Radius: 410 nm/472 miles (760 km)
Crew: One
Price/Unit Cost: $148.7 million flyaway cost (in FY 2007)
First Flight: September 7, 1997 (YF-22 prototype: September 29, 1990)
Deployed: Initial Operational Capability (IOC) in December 2005
Total: 187 /// Active: 169 and ANG: 18 (as of September 2012)
Total: 182 /// Active: 162 and ANG: 20 (as of September 2013)

1x General Dynamics M61-A2 Vulcan 20mm six-barreled gatling gun with 480 rounds;
Air-to-Air Configuration:
2x AIM-9M/X Sidewinder and 6x AIM-120 AMRAAM.
Air-to-Ground Configuration:
2x AIM-9M/X Sidewinder + 2x AIM-120 AMRAAM + 2x GBU-32 1,000-pound Joint Direct Attack Munition (JDAM) or
8x 250-pound GBU-39/40 Small Diameter Bombs.

Northrop Grumman AN/APG-77 AESA Radar
Lockheed Martin AN/AAR-56 Missile Warning System (MWS)
BAE Systems AN/ALR-94 Radar Warning Receiver (RWR)
BAE Systems AN/ALE-52 countermeasures dispensing system
BAE Systems head-up display (HUD)

Defense Program

Aircraft Programs Missile Programs Space Programs Shipbuilding Programs Vehicle Programs