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- W164564376 abstract "Since 1981, NASA has been supporting an Orbit Transfer Vehicle (OTV) propulsion technology development program which encompasses the efforts of three major engine manufacturers. A thrust variability ratio of 30:1 has been stipulated for the baseline 520 lbf-sec/lbm engines, in order to yield the versatility needed for low acceleration missions, orbit-transfer missions, and aeromaneuvering tasks. These goals may not be reachable either individually or collectively; the program supports generic technology benefitting all three engine concepts, as well as concept-specific technology. Engine/vehicle integration will determine the final configuration. The three engines under study differ as to turbomachinery types and operating speeds." @default.
- W164564376 created "2016-06-24" @default.
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- W164564376 date "1984-08-01" @default.
- W164564376 modified "2023-09-27" @default.
- W164564376 title "Integration becomes the name of the OTV game" @default.
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