Combined Loads, Vibration, and Modal Testing of QuickSCAT Spacecraft

Scharton, T.; Vujcich, M.

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