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Advanced pressurization systems for cryogenic propellants Final report, 20 Nov. 1963 - 25 Jun. 1965Optimized pressurization system for Apollo-type service module using cryogenic propellants
Document ID
19670007276
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, J. E. (Martin Co. Denver, CO, United States)
Brady, H. F. (Martin Co. Denver, CO, United States)
Scott, O. L. (Martin Co. Denver, CO, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
CR-65-75
NASA-CR-54467
Report Number: CR-65-75
Report Number: NASA-CR-54467
Accession Number
67N16605
Funding Number(s)
CONTRACT_GRANT: NAS3-2574
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
APOLLO SPACECRAFT
FUEL TANK PRESSURIZATION SYSTEM
CRYOGENIC PROPELLANT

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