Lockheed Aircraft

Lockheed F-22A Raptor

Lockheed F-22A Raptor

Early Fighter United States Army Air Corps

Lockheed Aircraft

Commercial Aircraft

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L-749 Constellation
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Transport Aircraft

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Recon aircraft

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US Navy

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Lockheed T-33 Shootingstar

Millitary Aircraft WW2

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Lockheed Aircraft

The Lockheed Martin F-22 Raptor is an American single-seat, twin-engine, all-weather stealth tactical fighter aircraft

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Lockheed C-5M Galaxy

The Lockheed Martin F-22 Raptor is an American single-seat, twin-engine, all-weather stealth tactical fighter aircraft developed exclusively for the United States Air Force (USAF). The result of the USAF’s Advanced Tactical Fighter (ATF) program, the aircraft was designed primarily as an air superiority fighter, but also has ground attackelectronic warfare, and signal intelligence capabilities.[2] The prime contractor, Lockheed Martin, built most of the F-22’s airframe and weapons systems and conducted final assembly, while Boeing provided the wings, aft fuselage, avionics integration, and training systems.


The F-22 Raptor is a fifth-generation fighter that is considered fourth generation in stealth aircraft technology by the USAF.[94] It is the first operational aircraft to combine supercruisesupermaneuverability, stealth, and sensor fusion in a single weapons platform.[95] The F-22 has four empennage surfaces, retractable tricycle landing gear, and clipped delta wings with reverse trailing edge sweep and leading edge extensions running to the upper outboard corner of the inlets. Flight control surfaces include leading-edge flapsflaperonsaileronsrudders on the canted vertical stabilizers, and all-moving horizontal tails (stabilators); for speed brake function, the ailerons deflect up, flaperons down, and rudders outwards to increase drag

RoleStealth air superiority fighter
National originUnited States
ManufacturerLockheed Martin Aeronautics
Boeing Defense, Space & Security
First flight7 September 1997; 23 years ago
Introduction15 December 2005
StatusIn service
Primary userUnited States Air Force
Number built195 (8 test and 187 operational aircraft)[1]
Developed fromLockheed YF-22
Developed intoLockheed Martin X-44 MANTA
Lockheed Martin FB-22


As the program moved to full-scale development, or Engineering & Manufacturing Development (EMD), the production version had notable differences from the YF-22, despite having a similar configuration. The wing’s leading edge sweep angle was decreased from 48° to 42°, while the vertical stabilizers were shifted rearward and decreased in area by 20%.[15] To improve pilot visibility, the canopy was moved forward 7 inches (18 cm) and the engine intakes moved rearward 14 inches (36 cm). The shapes of the wing and stabilator trailing edges were refined to improve aerodynamics, strength, and stealth characteristics.[16][17] Increasing weight during development caused slight reductions in range and maneuver performance

Specifications (F-22A) Data from Data from Flight Global

  • General characteristics

    • Crew: 1
    • Length: 62 ft 1 in (18.92 m)
    • Wingspan: 44 ft 6 in (13.56 m)
    • Height: 16 ft 8 in (5.08 m)
    • Wing area: 840 sq ft (78.04 m2)
    • Aspect ratio: 2.36
    • Airfoil: NACA 6 series airfoil
    • Empty weight: 43,340 lb (19,700 kg)
    • Gross weight: 64,840 lb (29,410 kg)
    • Max takeoff weight: 83,500 lb (38,000 kg)
    • Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (12,000 kg) with two 2× 600 US gal tanks
    • Powerplant: 2 × Pratt & Whitney F119-PW-100 augmented turbofans, 26,000 lbf (116 kN) thrust each dry, 35,000 lbf (156 kN) with afterburner[

Specifications (F-22A)



  • Maximum speed: Mach 2.25 (1,500 mph, 2,414 km/h) at altitude
    • Mach 1.21, 800 knots (921 mph; 1,482 km/h) at sea level
    • Mach 1.82 (1,220 mph, 1,963 km/h) supercruise at altitude
  • Range: 1,600 nmi (1,800 mi, 3,000 km) or more with 2 external fuel tanks
  • Combat range: 460 nmi (530 mi, 850 km) clean with 100 nmi (115 mi, 185 km) in supercruise
    • 590 nmi (679 mi, 1,093 km) clean subsonic[N 9]
  • Ferry range: 1,740 nmi (2,000 mi, 3,220 km)
  • Service ceiling: 65,000 ft (20,000 m)
  • g limits: +9.0/−3.0
  • Wing loading: 77.2 lb/sq ft (377 kg/m2)
  • Thrust/weight: 1.08 (1.25 with loaded weight and 50% internal fuel)