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Peacekeeper tank slosh modelInformation on a tank slosh model for Peacekeeper missiles is given in viewgraph form. Allowable vehicle errors for nose cone ejection clearance, vehicle maneuver sloshing problems, slosh/moment prediction, slosh surface specification, code validation, experimental model-computational model comparison and the propellant storage assembly are covered.
Document ID
19880006560
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schwartz, Sidney H. (Rockwell International Corp. Canoga Park, CA, 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
Fluid Mechanics And Heat Transfer
Accession Number
88N15942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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