F-22 Raptor Maiden Flight Lockheed And Skunk Works Stealth Tactical Fighter FULL DOCUMENTARY

The maiden flight of the F-22 Raptor took place on September 7 1997 at Edwards Air Force Base in California. The aircraft was piloted by Lockheed Martin test pilot Paul Metz. The F-22 was developed by Lockheed Martin and Boeing as a stealthy highly maneuverable air superiority fighter. The F-22s first flight was a significant milestone in the development of the aircraft. The flight lasted for around 50 minutes during which the aircraft performed a series of maneuvers to test its flight characteristics and systems. The F-22 performed well with no major issues reported during the flight. The F-22 Raptor is considered to be one of the most advanced fighters in the world. It is designed to be stealthy highly maneuverable and able to fly at supersonic speeds without using afterburners. The aircraft is also equipped with advanced avionics and weapons systems making it a formidable opponent in air-to-air combat. The F-22s first flight was a major achievement for the United States Air Force and the companies involved in its development. The aircraft has since gone on to become a key component of the U.S. Air Forces air superiority fleet. The F-22 is currently in service with the United States Air Force and the Royal Australian Air Force. The maiden flight of the F-22 marked the beginning of a new era in air superiority fighters and the aircraft continues to be a vital asset to the U.S. military. The F-22s advanced capabilities and stealth capabilities are a testament to the capabilities of modern aircraft technology and the dedication of the engineers and pilots who developed and fly the aircraft. 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: 43340 lb 19700 kg Gross weight: 64840 lb 29410 kg Max takeoff weight: 83500 lb 38000 kg Fuel capacity: 18000 lb 8200 kg internally or 26000 lb 12000 kg with two 2 600 US gal tanks Powerplant: 2 Pratt Whitney F119-PW-100 augmented turbofans 26000 lbf 116 kN thrust each dry 35000 lbf 156 kN with afterburner Performance Maximum speed: Mach 2.25 1500 mph 2414 kmh at altitude Mach 1.21 800 knots 921 mph 1482 kmh at sea level Mach 1.82 1220 mph 1963 kmh supercruise at altitude Range: 1600 nmi 1800 mi 3000 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 1093 km clean subsonic Ferry range: 1740 nmi 2000 mi 3220 km Service ceiling: 65000 ft 20000 m g limits: 9.03.0 Wing loading: 77.2 lbsq ft 377 kgm2 Thrustweight: 1.08 1.25 with loaded weight and 50 internal fuel Armament Guns: 1 20 mm M61A2 Vulcan rotary cannon 480 rounds Internal weapons bays: Air-to-air mission loadout: 6 AIM-120 AMRAAM 2 AIM-9 Sidewinder Air-to-ground mission loadout: 2 1000 lb 450 kg JDAM or 8 250 lb 110 kg GBU-39 Small Diameter Bombs 2 AIM-120 AMRAAM 2 AIM-9 Sidewinder Hardpoint external: 4 under-wing pylon stations can be fitted to carry weapons each with a capacity of 5000 lb 2270 kg or 600 U.S. gallon 2270 L drop tanks 4x AIM-120 AMRAAM external Avionics ANAPG-77 or ANAPG-77V1 radar: 125150 miles 201241 km against 1 m2 11 sq ft targets estimated range more than 250 miles 400 km in narrow beams ANAAR-56 Missile Launch Detector MLD ANALR-94 electronic warfare system: 250 nautical miles 460 km or more detection range for radar warning receiver RWR Integrated CNI Avionics MJU-3940 flares for protection against IR missiles f22 f22raptor aircraft,

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