Validation of Force Limited Vibration Testing Using Dummy Satellite Structure

Details Validation of Force Limited Vibration Testing Using Dummy Satellite Structure Validation of Force Limited Vibration Testing Using Dummy Satellite Structure

Aug 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.558..209n&link_type=abstract

Proceedings of the 5th International Symposium on Environmental Testing for Space Programmes Noordwijk, The Netherlands (ESA SP-

Computer Science

Scientific paper

The benefit of force limited testing is that it limits the overtesting of flight hardware, by controlling input force and acceleration from the shaker to the test article. The force limited vibration testing is developed to minimize the overtesting associated with enveloping the acceleration spectral density and differences in flight versus test mounting impedance. This paper reports the basic study of the force limited testing method at Japan Aerospace Exploration Agency (JAXA). In this paper, some numerical methods were examined in order to estimate the maximum flight interface force between shaker and test article. This paper discusses results of force limit vibration test using a dummy satellite performed at JAXA Tsukuba Space

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