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Vibration and acoustic testing of spacecraft

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dc.contributor.author Scharton, T. D. en_US
dc.date.accessioned 2004-09-17T06:01:08Z
dc.date.available 2004-09-17T06:01:08Z
dc.date.issued 2002-06 en_US
dc.identifier.citation International Congress of Sound and Vibration en_US
dc.identifier.clearanceno 02-1359 en_US
dc.identifier.uri http://hdl.handle.net/2014/8818
dc.description.abstract Spacecraft are subjected to a variety of dynamics environments, which may include: quasi-static, vibration and acoustic loads at launch: pyrotechnic shocks generated by separation mechanisms; on orbit jitter; and sometimes, planetary landing loads. There is a trend in the aerospace industry to rely more on structural analyses and less on testing to simulate these environments, because dynamics testing of spacecraft is time consuming, risky and expensive. en_US
dc.format.extent 2137195 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other vibration acoustics spacecraft en_US
dc.title Vibration and acoustic testing of spacecraft en_US


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