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Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 2Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limits
Document ID
19700025294
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-109944
D2-118246-1-VOL-2
Report Number: NASA-CR-109944
Report Number: D2-118246-1-VOL-2
Accession Number
70N34610
Funding Number(s)
CONTRACT_GRANT: NASW-1650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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