dc.contributor.author |
Lou, M. C. |
en_US |
dc.contributor.author |
Brent, D. N. |
en_US |
dc.date.accessioned |
2004-10-06T01:25:31Z |
|
dc.date.available |
2004-10-06T01:25:31Z |
|
dc.date.issued |
1993-08 |
en_US |
dc.identifier.citation |
Innsbruck, Austria |
en_US |
dc.identifier.clearanceno |
93-0333 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/34906 |
|
dc.description.abstract |
For a flight hardware system to be launched and/or retrieved by the Space Shuttle, the development of its structures must address both personnel safety and safety of the mission. Safety of personnel and the Shuttle has been a paramount concern for the National Space Transportation System (NSTS) since the first Shuttle flight in 1980. |
en_US |
dc.format.extent |
283229 bytes |
|
dc.format.mimetype |
application/pdf |
|
dc.language.iso |
en_US |
|
dc.subject.other |
shuttle payloads uniform safety policies strength design vibro-acoustic loads fracture control Wide-Field/Planetary Camera (WF/PC 1)optical bench structure |
en_US |
dc.title |
Structural Safety of a Hubble Space Telescope Science |
en_US |