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Combined Loads, Vibration, and Modal Testing of QuickSCAT Spacecraft

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dc.contributor.author Scharton, T. en_US
dc.contributor.author Vujcich, M. en_US
dc.date.accessioned 2004-09-23T22:54:20Z
dc.date.available 2004-09-23T22:54:20Z
dc.date.issued 1999-03-10 en_US
dc.identifier.citation Aerospace Testing Seminar en_US
dc.identifier.citation Los Angeles, California, USA en_US
dc.identifier.clearanceno 99-0138 en_US
dc.identifier.uri http://hdl.handle.net/2014/16742
dc.description.abstract Combining the quasi-static loads, workmanship verification, and model validation tests of aerospace hardware into a single vibration test sequence can considerably reduce schedule and cost. en_US
dc.format.extent 764242 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other QuickScat Spacecraft vibration testing force en_US
dc.title Combined Loads, Vibration, and Modal Testing of QuickSCAT Spacecraft en_US


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