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Find link is a tool written by Edward Betts .
searching for Gas-generator cycle 11 found (165 total)
alternate case: gas-generator cycle
Viking (rocket engine)
(529 words)
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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)
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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)
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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)
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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 AR2
(507 words)
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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
Rocketdyne E-1
(1,238 words)
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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
Pistonless pump
(929 words)
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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
(2,689 words)
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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)
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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)
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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
(11,156 words)
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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