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Composite engines for application to a single-stage-to-orbit vehicleSeven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine. The resulting performance, weight, and drawings of each engine form a data base for establishing a potential of this class of composite engine to various missions, including the single-stage-to-orbit application. The impact of advanced technology in the design of the critical fan turbine was established.
Document ID
19760006115
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bendot, J. G. (Marquardt Corp. Van Nuys, CA, United States)
Brown, P. N. (Marquardt Corp. Van Nuys, CA, United States)
Piercy, T. G. (Marquardt Corp. Van Nuys, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Publication Information
Publisher: NASA
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-2613
S-1325
Accession Number
76N13203
Funding Number(s)
CONTRACT_GRANT: NAS1-13304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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