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EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESSEffect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid-vapor interface during weightlessness
Document ID
19630013804
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Nussle, R. C. (NASA Lewis Research Center Cleveland, OH, United States)
Otto, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Petrash, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2075
Accession Number
63N23684
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WEIGHTLESSNESS
PROPELLANT
LIQUID-VAPOR INTERFACE
TANK GEOMETRY

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