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Medium-frequency impulsive-thrust-activated liquid hydrogen reorientation with GeyserEfficient technique are studied for accomplishing propellant resettling through the minimization of propellant usage through impulsive thrust. A comparison between the use of constant-thrust and impulsive-thrust accelerations for the activation of propellant resettlement shows that impulsive thrust is superior to constant thrust for liquid reorientation in a reduced-gravity environment. This study shows that when impulsive thrust with 0.1-1.0-, and 10-Hz frequencies for liquid-fill levels in the range between 30-80 percent is considered, the selection of 1.0-Hz-frequency impulsive thrust over the other frequency ranges of impulsive thrust is the optimum. Characteristics of the slosh waves excited during the course of 1.0-Hz-frequency impulsive-thrust liquid reorientation were also analyzed.
Document ID
19920067637
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hung, R. J.
(NASA Headquarters Washington, DC United States)
Shyu, K. L.
(Alabama, University Huntsville, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1992
Publication Information
Publication: Journal of Propulsion and Power
Volume: 8
Issue: 5 Se
ISSN: 0748-4658
Subject Category
Spacecraft Propulsion And Power
Accession Number
92A50261
Funding Number(s)
CONTRACT_GRANT: NAGW-812
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Other

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