Liquid propellant and elastic behavior of boosters exhibit problem areas which should be considered in preliminary design stage; influence of propellant sloshing on stability of vehicle requires knowledge of liquid motion for various container geometries; since stability of vehicle alone is not sufficient for success of mission, magnification function of various generalized coordinates is also presented; these response functions lead way for design of swivel engine system.
Interactions of structural vibrations, propellant sloshing and control frequency in booster rockets
Zum Zusammenwirken struktureller Schwingungen, Treibstoffschwappen und der Regelfrequenz bei Traegerraketen
Raumfahrtforschung ; 9 , n 2
1965
15 pages
Article (Journal)
German
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NTIS | 1968
|NTIS | 1967
|NTRS | 1964
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