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- RS-88 abstract "The RS-88 is a liquid-fueled rocket engine burning Alcohol (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 50,000 lbf (220 kN) 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).".
- RS-88 thumbnail RS-88_test_firing.jpg?width=300.
- RS-88 wikiPageExternalLink 6-11-97.pdf.
- RS-88 wikiPageExternalLink 20050237017_2005207085.pdf.
- RS-88 wikiPageID "35996685".
- RS-88 wikiPageRevisionID "588290982".
- RS-88 countryOfOrigin United_States.
- RS-88 fuel Alcohol.
- RS-88 hasPhotoCollection RS-88.
- RS-88 manufacturer Rocketdyne.
- RS-88 name "RS-88".
- RS-88 oxidiser Liquid_oxygen.
- RS-88 purpose "low cost throttleable booster engine".
- RS-88 type "liquid".
- RS-88 subject Category:Rocket_engines.
- RS-88 comment "The RS-88 is a liquid-fueled rocket engine burning Alcohol (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.".
- RS-88 label "RS-88".
- RS-88 sameAs RS-88.
- RS-88 sameAs m.0j_7pz4.
- RS-88 sameAs Q7277680.
- RS-88 sameAs Q7277680.
- RS-88 wasDerivedFrom RS-88?oldid=588290982.
- RS-88 depiction RS-88_test_firing.jpg.
- RS-88 isPrimaryTopicOf RS-88.
