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searching for gas-generator cycle 11 found (165 total)

alternate case: Gas-generator cycle

Viking (rocket engine) (529 words) [view diff] no match in snippet view article

The Viking rocket engines were members of a series of bipropellant engines for the first and second stages of the Ariane 1 through Ariane 4 commercial
Reaction Motors XLR99 (457 words) [view diff] no match in snippet view article find links to article
The Reaction Motors LR99 engine was the first large, throttleable, restartable liquid-propellant rocket engine. Development began in the 1950s by the Reaction
Rolls-Royce RZ.2 (594 words) [view diff] no match in snippet view article find links to article
The RZ.2 was a British design for a liquid oxygen (LOX) / kerosene-fuelled rocket engine to power the Blue Streak (missile). The design was a development
Walter HWK 109-509 (1,426 words) [view diff] no match in snippet view article find links to article
The Walter HWK 109-509 was a German liquid-fuel bipropellant rocket engine that powered the Messerschmitt Me 163 Komet and Bachem Ba 349 aircraft. It was
Rocketdyne E-1 (1,238 words) [view diff] no match in snippet view article find links to article
Rocketdyne's E-1 was a liquid propellant rocket engine originally built as a backup design for the Titan I missile. While it was being developed, Heinz-Hermann
Rocketdyne AR2 (507 words) [view diff] no match in snippet view article find links to article
The Rocketdyne AR2, also known by the military designation LR42, was a family of liquid-fuelled rocket engines designed and produced in the United States
Pistonless pump (929 words) [view diff] no match in snippet view article find links to article
They cannot use either a staged combustion or expander cycle. A gas generator cycle is also difficult to integrate with the pistonless pump. The generated
Relativity Space (2,869 words) [view diff] no match in snippet view article find links to article
The Aeon R engine, currently under development, is a high pressure gas generator cycle LOX/subcooled Methane propellants engine designed to produce 258
Masten Space Systems (4,606 words) [view diff] no match in snippet view article find links to article
Cutlass evolved into a low cost expendable upper stage engine using a gas generator cycle. A Phase 2 SBIR grant was not awarded so development was put on hold
Tianlong-3 (898 words) [view diff] no match in snippet view article find links to article
40%~110%, and a thrust-to-weight ratio of 163. The engines utilize a gas generator cycle and feature pump-fed gimbaling. The first stage propellant tanks
Turbofan (11,175 words) [view diff] no match in snippet view article find links to article
turbofan which allows specific thrust to be chosen independently of the gas generator cycle. The working substance of the thermodynamic cycle is the only mass