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Structural response loads in force-limited vibration testing
Flight equipment is exposed to random vibration excitations during launch and is functionally designed to survive a shaker random vibration test.
Document ID
20060031155
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/12312
Authors
Chang, K. Y.
Date Acquired
August 23, 2013
Publication Date
April 22, 2001
Distribution Limits
Public
Copyright
Other
Keywords
vibration testing random vibration force limiting
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