Gravity jitter excited cryogenic liquid slosh waves in microgravity environmentThe dynamical behavior of fluids, in particular the effect of surface tension on partially-filled rotating fluids (cryogenic liquid helium and helium vapor) in a full-scale Gravity Probe-B Spacecraft liquid helium container tank without probe imposed by various frequencies of gravity jitter have been investigated. Results disclose the conditions for the excitation of large amplitude slosh waves which should be avoided in the design of cryogenic liquid propellant system.
Document ID
19930064653
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hung, R. J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Lee, C. C. (Alabama Univ. Huntsville, United States)
Leslie, F. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Advances in cryogenic engineering. Vol. 37B - Proceedings of the 1991 Cryogenic Engineering Conference, Univ. of Alabama, Huntsville, June 11-14, 1991 (A93-48578 20-37)
Publisher: Plenum Press
Subject Category
Engineering (General)
Accession Number
93A48650
Funding Number(s)
CONTRACT_GRANT: NAG8-129
Distribution Limits
Public
Copyright
Other
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Related Records
IDRelationTitle19930064581Collected WorksAdvances in cryogenic engineering. Vols. 37A & 37B - Proceedings of the 1991 Cryogenic Engineering Conference, Univ. of Alabama, Huntsville, June 11-14, 1991