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Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limits
Document ID
19700025293
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Foley, M. G. (Boeing Co. Houston, TX, United States)
Kerkam, B. F. (Boeing Co. Houston, TX, United States)
Smith, D. W. (Boeing Co. Houston, TX, United States)
Wood, A. A. (Boeing Co. Houston, TX, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-109945
D2-118246-1-VOL-1
Report Number: NASA-CR-109945
Report Number: D2-118246-1-VOL-1
Accession Number
70N34609
Funding Number(s)
CONTRACT_GRANT: NASW-1650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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