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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).
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 ...
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 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 ...
The P-409 engine was also proposed for use in the EA-6B ADVCAP, [10] but that program was canceled after three prototypes were built and flown. The P-409 would have been available as a new engine or as an upgrade kit for P-408 engines, but was never ordered in significant quantities. [11] [12] PW1212 J52-P-409 re-designated PW1216
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]
The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg).
The Rolls-Royce RB.37 Derwent is a 1940s British centrifugal compressor turbojet engine, the second Rolls-Royce jet engine to enter production. It was an improved version of the Rolls-Royce Welland, which itself was a renamed version of Frank Whittle's Power Jets W.2B.