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The Lockheed L-133 was an exotic design started in 1939 which was proposed to be the first jet fighter of the United States Army Air Forces (USAAF) during World War II.The radical design was to be powered by two axial-flow turbojets with an unusual blended wing-body canard design capable of 612 mph (985 km/h) in level flight.
The P-59Bs were assigned to the 412th Fighter Group to familiarize AAF pilots with the handling and performance characteristics of jet aircraft. [17] While the P-59 was not a great success, the type did give the USAAF and the USN experience with the operation of jet aircraft, in preparation for the more advanced types that would shortly become ...
Lockheed YF-94 (S/N 48-373). This was the second aircraft built (from TF-80C) On 16 April 1949, the first YF-94 prototype performed its maiden flight. [6] To accelerate development, these early test aircraft were converted from existing T-33s; they maintained roughly 75% commonality in terms of components with those used in the earlier F-80 and T-33As.
The McDonnell FH Phantom is a twinjet, straight-wing, carrier-based fighter aircraft designed and first flown during late World War II for the United States Navy.As a first-generation jet fighter, the Phantom was the first purely jet-powered aircraft to land on an American aircraft carrier [2] [N 1] and the first jet deployed by the United States Marine Corps.
The Grumman F9F Panther is an early carrier-based jet fighter designed and produced by the American aircraft manufacturer Grumman.It was the first jet-powered fighter aircraft to see air-to-air combat with the United States Navy as well as being Grumman’s first jet fighter.
Two pilots demonstrated the differences between the fighter jets, referencing dogfight footage and using quickly made paper airplanes.
Data from The Encyclopedia of World Aircraft General characteristics Crew: 1 Length: 28 ft 9 in (8.76 m) Wingspan: 20 ft 8 in (6.30 m) Height: 9 ft 3 in (2.82 m) Wing area: 125 sq ft (11.6 m 2) Airfoil: RAE 102 Gross weight: 4,500 lb (2,041 kg) Powerplant: 1 × Armstrong Siddeley Viper 101 turbojet engine, 1,640 lbf (7.3 kN) thrust Performance Maximum speed: 600 mph (970 km/h, 520 kn) Service ...
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