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The influence of structural flexibility on the dynamic response of spinning spacecraft
Home
Publications
The influence of structural flexibility on the dynamic response of spinning spacecraft
The influence of structural flexibility on the dynamic response of spinning spacecraft
CB
C. Bodley
C. Bodley
AP
A. Park
A. Park
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10 April 1972
proceedings article
Published by
American Institute of Aeronautics and Astronautics (AIAA)
https://doi.org/10.2514/6.1972-348
Abstract
No abstract available
Cited
Cited by 12 articles
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