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Undeveloped rocket cycle applications to advanced earth-to-orbit transportationThe application of undeveloped rocket engine cycles to advanced manned launch vehicles is assessed. Two undeveloped rocket cycles are selected, the split expander cycle and the full flow staged-combustion cycle, for detailed engine description and comparison with more mainstream advanced vehicle engine candidates. In the formulation of the Next Manned Transportation System, propulsion is a key area for cost reduction because of the high cost elements associated with the current Space Transportation Syystem.
Document ID
19900053577
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kramer, R. D.
(SRS Technologies Huntsville, AL, United States)
Martin, J. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2438
Report Number: AIAA PAPER 90-2438
Accession Number
90A40632
Funding Number(s)
CONTRACT_GRANT: NAS8-37350
CONTRACT_GRANT: NAS8-36643
Distribution Limits
Public
Copyright
Other

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