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Computational prediction of propellant reorientationViewgraphs from a presentation on computational prediction of propellant reorientation are given. Information is given on code verification, test conditions, predictions for a one-quarter scale cryogenic tank, pulsed settling, and preliminary results.
Document ID
19880006558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hochstein, John I. (Washington Univ. Saint Louis, MO, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Publication Information
Publication: NASA. Lewis Research Center, Cleveland, Ohio. Cryogenic Fluid Management Technology Workshop. Volume 1: Presentation Material and Discussion
Subject Category
Propellants And Fuels
Accession Number
88N15940
Funding Number(s)
CONTRACT_GRANT: NAG3-578
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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