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 |