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・ RS-232
・ RS-24 Yars
・ RS-26 Rubezh
・ RS-27
・ RS-27A
・ RS-28 Sarmat
・ RS-422
・ RS-423
・ RS-449
・ RS-485
・ RS-56812
・ RS-67,333
・ RS-68
・ RS-82 (rocket family)
・ RS-83
RS-88
・ RS/6000
・ RS100
・ Rs1799913
・ Rs1800532
・ Rs1800955
・ Rs1801133
・ Rs1805054
・ Rs1954787
・ RS2
・ RS200
・ RS200 (dinghy)
・ RS280
・ Rs28363170
・ RS3


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RS-88 : ウィキペディア英語版
RS-88

The RS-88 is a liquid-fueled rocket engine burning ethanol as fuel, and using liquid oxygen (LOX) as the oxidizer. It was designed and built by Rocketdyne, originally for the NASA Bantam System Technology program (1997). In 2003, it was designated by Lockheed for their Pad Abort Demonstration (PAD) vehicle. NASA tested the RS-88 in a series of 14 hot-fire tests, resulting in 55 seconds of successful engine operation in November and December 2003. The RS-88 engine proved to be capable of of thrust at sea level. The ''RS-88'' engine has been selected for usage as the CST-100 Launch Escape System and is being tested by Boeing (2011).〔(【引用サイトリンク】url=http://www.youtube.com/watch?v=mOv1ew1GPKc )
== Bantam Launch System ==
The Bantam System Technology Project, which is part of the Low Cost Technologies effort, teams NASA and its business partners to research and demonstrate technologies for a new low-cost launch system. A technology demonstration flight was targeted for late 1999.
The ''RS-88'' engine was designed by Rocketdyne under NASA's Bantam program which was the propulsion element of the Low Cost Technologies of the larger Advanced Space Transportation Program.

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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