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The Teledyne CAE J402 is an American small turbojet engine. Several variants have been developed to power unmanned air vehicles such as missiles and target drones. Developed in the 1970s for the Harpoon anti-ship missile, the J402 was the first jet engine to be designed as a "wooden round", meaning that the engine had to be able to sit for long periods without maintenance or inspection and ...
Basically identical to the -8/-8B, the aircraft was equipped with a fresh water spray system that flushed salt deposits out of the engine before takeoff and after shutdown. [8] J46-WE-18 This variant produced an increased 6,100 lbf (27.1 kN) of A/B thrust for the proposed A2U-1 attack aircraft, an attack variant of the F7U. This variant was ...
The AL-7 had supersonic airflow through the first stage of the compressor.TR-7 prototype, developing 6,500 kgf (14,330 lb f, 63.7 kN) of thrust, was tested in 1952, and the engine was initially intended for Ilyushin's Il-54 bomber.
The XJ37 was being worked on at the same time as competing Westinghouse axial-flow designs undergoing development, the 19A and 19B, were being test-run through the 1943-45 period, resulting in America's first production axial-flow turbojet engine, the Westinghouse J30, of which some 260 examples were made for the earliest American military jets ...
As certified, the Hansa Jet can carry up to 12 passengers. Its General Electric CJ610 turbojet engines enabled the aircraft to achieve a maximum speed of 900 km/h (486 kn) along with a maximum endurance in excess of 2,200 km (1,200 nmi). [6] The decision to mount these engines far aft contributed to the relatively quiet cabin. [2]
Data from: Aircraft engines of the World 1953, [1] Flight 20 March 1959 :AERO ENGINES 1959 . . ., [2] Aircraft engines of the World 1957 [3] XJ44 Prototypes of the J44 J44-R-1 United States Air Force (USAF) engine, similar to the United States Navy (USN) -6, 950 lbf (4.2 kN). J44-R-2 Same as -6 but with different installation. J44-R-3
The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle . The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine (that drives the compressor).
The YJ93 started life as the General Electric J79-X275, an enlarged version of the General Electric J79 turbojet with "275" meaning Mach 2.75, the engine's target operating speed. [2] This design evolved into the X279 when Mach 3 cruise became a requirement, and ultimately became the YJ93. [3] The engine used a special high-temperature JP-6 fuel.
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