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| H-1 (rocket engine) ： ウィキペディア英語版 |
Rocketdyne H-1
The Rocketdyne H-1 is a thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, where it was used in clusters of eight engines. After the Apollo program, surplus H-1 engines were rebranded and reworked as the Rocketdyne RS-27 engine with first usage on the Delta 2000 series in 1974.〔(【引用サイトリンク】publisher=Encyclopedia Astronautica )〕
==History==
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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