Advances in Aircraft and Spacecraft Science Volume 5, Number 2, March 2018 , pages 165-175 DOI: https://doi.org/10.12989/aas.2018.5.2.165 |
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Spacecraft vibration testing: Benefits and potential issues |
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Ali R. Kolaini, Walter Tsuha and Juan P. Fernandez
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Abstract | ||
Jet Propulsion Laboratory has traditionally performed system level vibration testing of flight spacecraft. There have been many discussions in the aerospace community for more than a decade about spacecraft vibration testing benefits or lack thereof. The benefits and potential issues of fully assembled flight spacecraft vibration testing are discussed herein. The following specific topics are discussed: spacecraft screening test to uncover workmanship problems for launch dynamics environments, force- and moment-limited vibration testing, potential issues with structural frequency identification using base shake test data, and failures related to vibration shaker testing and ways to prevent them. | ||
Key Words | ||
random vibration and sine test; acoustic; shaker vibration; virtual shaker; force limited RV test | ||
Address | ||
Ali R. Kolaini, Walter Tsuha and Juan P. Fernandez: Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA | ||