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Prediction of propellant tank pressurization requirements by dimensional analysisDimensional analysis used to derive general equation for predicting gas pressurization requirements in cylindrical and spherical liquid propellant tanks
Document ID
19660019780
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Nein, M. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Thompson, J. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3451
Report Number: NASA-TN-D-3451
Accession Number
66N29070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL TANK
LIQUID PROPELLANT
DIMENSIONAL ANALYSIS
SPHERICAL TANK
PROPELLANT TANK
PRESSURIZATION

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