Difference between revisions of "F-22"
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Latest revision as of 10:27, 21 October 2018
| F-22 | |
|---|---|
| Lua error: Internal error: The interpreter exited with status 127. | |
| Role | |
| Manufacturer | Nyland Group |
| Introduction | 1529 |
| Retired | n/a |
| Status | operational |
| Produced | ### |
History
Design
Variants
Specifications (F-22C)
- Crew: one
- Length: 49 ft 5 in (15.06 m)
- Wingspan: 32 ft 8 in (9.96 m)
- Height: 16 ft (4.88 m)
- Empty weight: 18,900 lb (8,570 kg)
- Loaded weight: 26,500 lb (12,000 kg)
- Max. takeoff weight: 42,300 lb (19,200 kg)
- Powerplant: 1 × afterburning turbofans
- Dry thrust: 17,155 lbf (76.3 kN)
- Thrust with afterburner: 28,600 lbf (127 kN)
- Maximum speed: Mach 1.2 (915 mph, 1,470 km/h)
- Combat radius: 340 mi (295 nmi, 550 km)
- Ferry range: 2,280 nmi (2,620 mi, 4,220 km)
- Service ceiling: 50,000+ ft (15,240+ m)
- Rate of climb: 50,000 ft/min (254 m/s)
- Guns: x1 20 mm canons, 511 rounds/cannon
- Hardpoints: 11 total (x2 wing-tip, x6 under-wing, x3 under-fuselage with a capacity of 17,000 lb (7,700 kg)
