Design by eWings

Lockheed Martin / Boeing F-22 Raptor

Specifications

General characteristics

Crew: 1

Length: 62 ft 1 in (18.90 m)

Wingspan: 44 ft 6 in (13.56 m)

Height: 16 ft 8 in (5.08 m)

Wing area: 840 ft² (78.04 m²)

Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip

Empty weight: 43,430 lb (19,700 kg)

Loaded weight: 64,460 lb (29,300 kg)

Max takeoff weight: 83,500 lb (38,000 kg)

Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans

Dry thrust: 23,500 lb (104 kN) each

Thrust with afterburner: 35,000+ lb (156+ kN) each

Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (11,900 kg) with two external fuel tanks

Performance

Maximum speed:

At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)

Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)

Range: 1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks

Combat radius: 410 nmi (471 mi, 759 km)

Ferry range: 2,000 mi (1,738 nmi, 3,219 km)

Service ceiling: 65,000 ft (19,812 m)

Wing loading: 77 lb/ft² (375 kg/m²)

Thrust/weight: 1.08 (1.26 with loaded weight & 50% fuel)

Maximum g-load: -3.0/+9.0 g[87]

Armament

Guns: 1× 20 mm (0.787 in) M61A2 Vulcan gatling gun in starboard wing root, 480 rounds

Air to air loadout:

6× AIM-120 AMRAAM

2× AIM-9 Sidewinder

Air to ground loadout:

2× AIM-120 AMRAAM and

2× AIM-9 Sidewinder for self-protection, and one of the following:

2× 1,000 lb (450 kg) JDAM or

2× Wind Corrected Munitions Dispensers (WCMDs) or

8× 250 lb (110 kg) GBU-39 Small Diameter Bombs

Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg).

Avionics

RWR (Radar warning receiver): 250 nmi (463 km) or more

Radar: 125-150 miles (200-240 km) against 1 m2 (11 sq ft) targets (estimated range)

Chemring MJU-39/40 flares for protection against IR missiles.


Data from USAF, F-22 Raptor Team web site, Lockheed Martin, Aviation Week, and Journal of Electronic Defense

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