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The General Electric XA102 is an American adaptive cycle engine demonstrator being developed by General Electric (GE). It is competing with the Pratt & Whitney XA103 as the powerplant for the United States Air Force's sixth generation fighter program, the Next Generation Air Dominance (NGAD).
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The Super Heavy booster is reusable, and is recovered via large arms on the tower capable of catching the descending vehicle. [7] As of January 2025, 0 boosters have been refurbished and subsequently flown at least a second time, though 2 boosters, Booster 12 and Booster 14, has been recovered after flight, with Booster 12 having damage to one ...
The KAI T-50 Golden Eagle uses a single General Electric F404-GE-102 turbofan engine with Full Authority Digital Engine Control (FADEC) system; the engine is similar to the F404-402, but with additional redundancies built in for single-engine operations. The aircraft has a maximum speed of Mach 1.5.
JATO (acronym for jet-assisted take-off) is a type of assisted take-off for helping overloaded aircraft into the air by providing additional thrust in the form of small rockets. The term JATO is used interchangeably with the (more specific) term RATO , for rocket-assisted take-off (or, in RAF parlance, RATOG , for rocket-assisted take-off gear ).
The driven axle is on the right; the booster normally hangs behind it. Diagram showing how a booster is installed and connected. A locomotive booster for steam locomotives is a small supplementary two-cylinder steam engine back-gear-connected to the trailing truck axle on the locomotive or one of the trucks on the tender.
The GE F110 turbofan fighter jet engine is a derivative of the F101, designed using data from the F101-powered variant of the F-16 Fighting Falcon tested in the early 1980s. [ 2 ] [ 3 ] The F101 also became the basis for the highly successful CFM56 series of civil turbofans.
This initial version of the CF6 has a single-stage fan with one core booster stage, driven by a 5-stage LP (low pressure) turbine, turbocharging a 16-stage HP (high pressure) axial compressor driven by a 2-stage HP turbine; the combustor is annular; separate exhaust nozzles are used for the fan and core airflows. The 86.4-in (2.19-m) diameter ...