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Study on propellant dynamics during dockingThe marker-and-cell numerical technique was applied to the study of axisymmetric and two-dimensional flow of liquid in containers under low gravity conditions. The purpose of the study was to provide the capability for numerically simulating liquid propellant motion in partially filled containers during a docking maneuver in orbit. A computer program to provide this capability for axisymmetric and two-dimensional flow was completed and computations were made for a number of hypothetical flow conditions.
Document ID
19730009541
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Feng, G. C.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Robertson, S. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
HREC-5712-2
NASA-CR-124055
LMSC/HREC-D225632
Report Number: HREC-5712-2
Report Number: NASA-CR-124055
Report Number: LMSC/HREC-D225632
Accession Number
73N18268
Funding Number(s)
CONTRACT_GRANT: NAS8-25712
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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