- air turborocket
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a jet engine where a gas generator drives the turbine that drives the inlet compressor
Wikipedia foundation.
Wikipedia foundation.
Air turborocket — The air turborocket as described in Chapter 14 of Tactical Missile Propulsion (Volume 170 of American Institute for Aeronautics and Astronautics Tactical Missile Book Series) is a form of combined cycle jet propulsion. The basic layout includes a … Wikipedia
Turborocket — A turborocket is a type of aircraft engine combining elements of a jet engine and a rocket.Once a jet engine goes high enough in an atmosphere, there is insufficient oxygen to burn the jet fuel. The idea behind a turborocket is to supplement the… … Wikipedia
Airbreathing jet engine — An airbreathing jet engine (or ducted jet engine) is a jet engine propelled by a jet of hot exhaust gases formed from air that is drawn into the engine via an inlet duct. All practical airbreathing jet engines are internal combustion engines that … Wikipedia
Single-stage-to-orbit — The VentureStar was a proposed SSTO spaceplane. A single stage to orbit (or SSTO) vehicle reaches orbit from the surface of a body without jettisoning hardware, expending only propellants and fluids. The term usually, but not exclusively, refers… … Wikipedia
ATR — 1. Acceptance Test Review Contributor: CASI 2. Advanced Test Reactor Contributor: CASI 3. Air Transport Rating Contributor: CASI 4. Air Turbo Ramjet Contributor: GSFC 5. Air Turborocket Contributor: CASI … NASA Acronyms
Lanceur orbital monoétage — Le VentureStar était une proposition de lanceur spatial SSTO Un lanceur orbital monoétage (en anglais SSTO single stage to orbit) est un engin spatial capable d atteindre l orbite terrestre et la vitesse de satellisation sans avoir à larguer un… … Wikipédia en Français
Jet engine — For a general overview of aircraft engines, see Aircraft engine. A Pratt Whitney F100 turbofan engine for the … Wikipedia
Reaction Engines SABRE — infobox rocket engine imsize=220 caption=A model of the SABRE name=Reaction Engines SABRE country of origin=UK status=R D type=liquid fuel=Liquid hydrogen oxidiser=LOX cycle=combined cycle precooled jet engine + closed cycle rocket engine… … 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
Reusable launch system — A reusable launch system (or reusable launch vehicle, RLV) is a launch system which is capable of launching a launch vehicle into space more than once. This contrasts with expendable launch systems, where each launch vehicle is launched once and… … Wikipedia