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Parallel-burn options for dual-fuel single-stage orbital transportsA parallel-burn version of a single-stage vehicle for transport from the earth to low-earth orbit using two fuels and rocket propulsion is considered. New engine results were incorporated in vehicle performance and design studies. The results indicate that a hydrogen-cooled gas generator cycle engine provides attractive vehicle performance and that there is little incentive for increasing the chamber pressure beyond 27 MPa.
Document ID
19780038292
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Martin, J. A.
(NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1978
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 15
Subject Category
Spacecraft Propulsion And Power
Accession Number
78A22201
Distribution Limits
Public
Copyright
Other

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