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STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHING

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Publication:5729787
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DOI10.2514/3.1861zbMath0118.40506OpenAlexW2060195773WikidataQ113703986 ScholiaQ113703986MaRDI QIDQ5729787

Helmut F. Bauer

Publication date: 1963

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.1861


zbMATH Keywords

mechanics



Related Items (2)

Analytical method for the attitude stability of partially liquid filled spacecraft with flexible appendage ⋮ Dynamic interaction of a liquid with the elastic structure of a circular cylindrical container







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