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Orbital Transfer Vehicle (OTV) advanced expander cycle engine point design studyProgress in the development of a performance optimized engine system design for an advanced LOX/hydrogen expander cycle engine is reported. Analysis of the components and engine and the resulting drawings is discussed. The status of the orbit transfer vehicle liquid engine transient simulation computer model is given.
Document ID
19800010902
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mellish, J. A. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 15, 1980
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161389
REPT-33574-M2
BMR-2
Report Number: NASA-CR-161389
Report Number: REPT-33574-M2
Report Number: BMR-2
Accession Number
80N19179
Funding Number(s)
CONTRACT_GRANT: NAS8-33574
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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