NASA NTRS · 19880006560
Peacekeeper tank slosh model
Abstract
Information 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.
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Schwartz, Sidney H.. 1987-09-01. Peacekeeper tank slosh model. https://ntrs.nasa.gov/citations/19880006560
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