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A transient heat transfer and thermodynamic analysis of the Apollo service module propulsion system. Vol. I, phase I - Transient thermal analysis Final report, 28 Jul. 1964 - 28 Jul. 1965Transient heat transfer and thermodynamic behavior analysis for Apollo service module propulsion system - fuel cell effect on overheating
Document ID
19660013063
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holmes, H. R.
Kazarian, M. A.
Nevelli, B. A.
Schultz, H. D.
Shuldiner, I.
Date Acquired
August 3, 2013
Publication Date
August 10, 1965
Subject Category
Propulsion Systems
Report/Patent Number
LR-18899, VOL. I
NASA-CR-65331
Report Number: LR-18899, VOL. I
Report Number: NASA-CR-65331
Accession Number
66N22352
Funding Number(s)
CONTRACT_GRANT: NAS9-3349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMODYNAMIC PROPERTY
APOLLO SPACECRAFT
TRANSIENT HEATING
FUEL CELL

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