Specifications
Data from Frawley
General characteristics
- Crew: 1
- Length: 45.01 ft (13.72 m)
- Wingspan: 36 ft (10.97 m)
- Height: (5.28 m)
- Wing area: 590 ft² (54.8 m²)
- Max. takeoff weight: 38,000 lb (17,200 kg)
- Powerplant: 1 × Pratt & Whitney F119 derivative afterburning turbofan
- Dry thrust: 28,000 lbf (125 kN)
- Thrust with afterburner: 43,000 lbf (191 kN)
Performance
- Maximum speed: Mach 1.6 (1,200 mph, 1,931 km/h) at altitude
- Range on USAF mission profile: 850 nmi (1,574 km)
- Range on USN mission profile: 750 nmi (1,389 km)
- Range on USMC/RN mission profile: 600 nmi (1,112 km)
Armament
- 20 mm M61A2 cannon, or 27 mm Mauser BK-27 cannon
- Internal: 6 AMRAAM air-air missiles or 2 AMRAAM air-air missiles and 2 x 2,000 lb (900 kg) class guided bombs
- External: Approx. 15,000 lb (6,800 kg) of full range of external stores including guided weapons, anti-radiation missile, air-to-surface weapons, auxiliary fuel tanks
Read more about this topic: Boeing X-32
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