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Pintle injector : ウィキペディア英語版 | Pintle injector A pintle injector is a type of propellant injection device for a rocket engine that was first used on a flight vehicle during the Apollo Program in the Lunar Excursion Module's Descent Propulsion System. Pintle injectors are currently used in SpaceX's Merlin engines. ==History== The origins of the pintle injector were early laboratory experimental apparatus, used by Caltech and JPL in the mid-1950s, to study propellant mixing and combustion reaction times of hypergolic liquid propellants. The pintle injector was reduced to practice and developed by Space Technology Laboratories (STL), then a division of Ramo-Wooldridge Corp., later TRW starting in 1960; however, it was not until October 1972 that for invention of the pintle injector was granted to Gerry Elverum, of TRW and made public.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Pintle injector」の詳細全文を読む
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