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- W2321604943 abstract "This paper describes Rocketdyne's successful analysis and demonstration of the Space Shuttle Main Engine (SSME) operation at off-nominal power levels during Reusable Launch Vehicle (RLV) evaluation tests. The nominal power level range for the SSME is from 65% rated power level (RPL) to 109% RPL. Off-nominal power levels incrementally demonstrated were: 17% RPL, 22% RPL, 27% RPL, 40% RPL, 45% RPL, and 50% RPL. Additional achievements during low power operation included: use of a hydrostatic bearing High Pressure Oxidizer Turbopump (HPOTP), nominal High Pressure Fuel Turbopump (HPFTP) first rotor critical speed operation, combustion stability at low power levels, and refined definition of nozzle flow separation heat loads." @default.
- W2321604943 created "2016-06-24" @default.
- W2321604943 creator A5042150208 @default.
- W2321604943 date "1997-07-06" @default.
- W2321604943 modified "2023-09-23" @default.
- W2321604943 title "SSME off-nominal low power level operation" @default.
- W2321604943 doi "https://doi.org/10.2514/6.1997-2685" @default.
- W2321604943 hasPublicationYear "1997" @default.
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