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liquid-fuel rocket engine

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  • F-1 (rocket engine) — The F 1 is a rocket engine developed by Rocketdyne and used in the Saturn V. Five F 1 engines were used in the S IC first stage of each Saturn V, which served as the main launch vehicle in the Apollo program. History The F 1 was originally… …   Wikipedia

  • Rocket engine — RS 68 being tested at NASA s Stennis Space Center. The nearly transparent exhaust is due to this engine s exhaust being mostly superheated steam (water vapor from its propellants, hydrogen and oxygen) …   Wikipedia

  • Liquid air cycle engine — A liquid air cycle engine (LACE) is a spacecraft propulsion engine that attempts to gain efficiency by gathering part of its oxidizer from the atmosphere. In a LOX/LH2 bipropellant rocket the liquid oxygen needed for combustion is the majority of …   Wikipedia

  • rocket engine — n. a reaction engine carrying its liquid fuel and liquid oxidizing agent in separate tanks: the fuel and oxidizer are brought together and ignited in a combustion chamber to create hot, explosive gas that escapes through a nozzle, providing a… …   English World dictionary

  • RD-170 (rocket engine) — The RD 170 is the world s most powerful multi nozzle multi chamber liquid bipropellant rocket engine. It burns the Russian equivalent of RP 1 fuel and LOX oxidizer in four combustion chambers supplied by a single turbo pump according to a staged… …   Wikipedia

  • Rocket engine test facility — A rocket engine test facility is a location where rocket engines may be tested on the ground, under controlled conditions. A ground test program is generally required before the engine is certified for flight. Ground testing is very inexpensive… …   Wikipedia

  • Rocket Engine Test Facility — Infobox nrhp name =Rocket Engine Test Facility nrhp type = nhl caption = 1982 photograph location= Lewis Research Center, Cleveland, Ohio locmapin = Ohio area = built =1957 architect= National Advisory Committee for Aeronautics (NACA)… …   Wikipedia

  • Rocket engine nozzle — A rocket engine nozzle is a propelling nozzle usually of the de Laval type used in a rocket engine to expand and accelerate the combustion gases, from burning propellants, so that the exhaust gases exit the nozzle at hypersonic… …   Wikipedia

  • rocket liquid-fuel engine — skystojo kuro raketinis variklis statusas T sritis Energetika apibrėžtis Skystu raketiniu kuru veikiantis reaktyvinis variklis. atitikmenys: angl. rocket liquid fuel engine vok. Flüssigkeitsraketentriebwerk, n rus. жидкостный ракетный двигатель,… …   Aiškinamasis šiluminės ir branduolinės technikos terminų žodynas

  • Cryogenic rocket engine — Vulcain engine of Ariane 5 rocket …   Wikipedia

  • M-1 (rocket engine) — Aerojet s M 1 was the largest and most powerful liquid hydrogen fueled rocket engine to be designed and built. It offered a baseline thrust of 1.5 million pounds force and 1.8 million pounds force as its immediate growth target. The M 1 was… …   Wikipedia

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