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Design of coast-phase propellant management system for two-burn Atlas-Centaur flight AC-8Coast-phase propellant management system for two- burn Atlas-Centaur flight AC-8
Document ID
19670001460
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Groesbeck, W. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-1318
Report Number: NASA-TM-X-1318
Accession Number
67N10783
Funding Number(s)
CONTRACT_GRANT: 891-01-00-06-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATLAS CENTAUR LAUNCH VEHICLE
CRYOGENIC PROPELLANT
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