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- W2103540781 abstract "Development and testing of a recovery system for the Low Cost Concept Validation (LCCV) phase of the U.S. Air Force Evolved Expendable Launch Vehicle (EELV) program is discussed. This system demonstrated for the first time the recovery of a liquid fueled rocket engine , a Space Shuttle Main Engine (SSME), from altitude to an ocean touchdown with subsequent refurbishment and engine firing. New technology developed and discussed includes the largest three Ringsail parachute cluster of Apollo heritage, in-flight deployable spray shield, and Propulsion Module (PM) testing approaches to validate the integrated concept." @default.
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- W2103540781 date "1997-06-03" @default.
- W2103540781 modified "2023-09-25" @default.
- W2103540781 title "Recovery system for the evolved expendable launch vehicle" @default.
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- W2103540781 doi "https://doi.org/10.2514/6.1997-1513" @default.
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