Lockheed Martin F-22 Raptor

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F-22- Raptor- ,take-off-stealth

From Wikipedia, the free encyclopedia
The Lockheed Martin/Boeing F-22 Raptor is a single-seat, twin-engine fifth-generation fighter aircraft that uses stealth technology. It was designed primarily as an air superiority fighter, but has additional capabilities that include ground attack, electronic warfare, and signals intelligence roles.

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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^[2][189])
• Loaded weight: 64,460 lb (29,300 kg^[190])
• 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^[191] (104 kN) each
  • Thrust with afterburner: 35,000+ lb^[2][191] (156+ kN) each
• Fuel capacity: 18,000 lb (8,200 kg) internally,^[2][189] or 26,000 lb (11,900 kg) with two external fuel tanks^[2][189]

Performance

• Maximum speed:
  
  
  • At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)^[90]
  • Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)^[90]
• Range: 1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
• Combat radius: 410 nmi^[188] (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 design g-load: -3.0/+9.0 ^[90]