Techno Press
You logged in as. Techno Press

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
 

Spacecraft vibration testing: Benefits and potential issues
Ali R. Kolaini, Walter Tsuha and Juan P. Fernandez

 
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
 

Techno-Press: Publishers of international journals and conference proceedings.       Copyright © 2025 Techno Press
P.O. Box 33, Yuseong, Daejeon 305-600 Korea, Tel: +82-42-828-7996, Fax : +82-42-828-7997, Email: admin@techno-press.com