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Propellant selection for spacecraft propulsion systems. Volume 3 - Thermodynamics and propulsion Final reportThermodynamic analysis of spacecraft thermal control and pressurization requirements for Mars Orbiter and Mars Excursion Module missions
Document ID
19680024607
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 4, 2013
Publication Date
August 30, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-96740
K-19-68-6, V. 3
Report Number: NASA-CR-96740
Report Number: K-19-68-6, V. 3
Accession Number
68N34079
Funding Number(s)
CONTRACT_GRANT: NASW-1644
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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