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Propellant tank pressurization analysis programComputer program for the analysis of a single propellant tank pressurization system includes many pertinent physical phenomena previously ignored in other mathematical models. This program can be used for analysis, simulation, and design of propellant pressurization systems.
Document ID
19670000624
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Epstein, M.
Date Acquired
August 3, 2013
Publication Date
December 1, 1967
Subject Category
Mathematics And Information Sciences
Report/Patent Number
Report Number: MFS-1506
MFS-1506
Accession Number
67B10625
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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