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Force limited vibration testing of Cassini spacecraft cosmic dust analyserThe testing of the cosmic dust analyzer for the Cassini mission using the force limited method in order to avoid overtesting and to verify the ability of the specimen design to withstand the loads during launch and cruise, is reported on. In order to implement the method, force gages, fixtures and a test controller are required and the test specimen is subjected to sine vibration, random vibration and half sine shock. The practical aspects of the use of the force limited method are described. Due to the high loads and the weak design of the structural element, a notching method is used which provides the possibility of limiting the excitation to flight expected levels.
Document ID
19970007447
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Jahn, Heiko
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Berlin, Germany)
Ritzmann, Swen
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Berlin, Germany)
Chang, Kurng
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Scharton, Terry
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 17, 2013
Publication Date
June 1, 1996
Publication Information
Publication: Proceedings of an International Conference on Spacecraft Structures, Materials and Mechanical Testing
Volume: 3
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
97N14183
Distribution Limits
Public
Copyright
Other
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