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Spacecraft Vibration Testing: Benefits and Potential IssuesJPL has traditionally performed system level vibration testing of flight spacecraft. The benefits and potential issues of fully assembled flight spacecraft vibration testing are discussed herein. The following specific topics, which may be complementary to the special session on “Virtual Vibration Testing,” are discussed: spacecraft workmanship, functional and structural integrity testing to uncover workmanship problems, force- and moment-limited vibration testing, potential issues with structural frequency identification using base shake test data, and several failures related to vibration shaker testing. The information provided in this paper is complementary to the special session on “Virtual Shaker Testing,’ and attention is given to issues that virtual shaker testing may face.
Document ID
20190026838
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Kolaini, Ali R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tsuha, Walter
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Fernandez, Juan P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
July 1, 2019
Publication Date
September 27, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JPL-CL-16-4234
Meeting Information
Meeting: European Conference on Spacecraft Structures, Materials and Environmental Testing
Location: Toulouse
Country: France
Start Date: September 27, 2016
End Date: September 30, 2016
Sponsors: Centre National d'Etudes Spatiales
Distribution Limits
Public
Copyright
Other

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