dc.contributor.author |
Kordon, M. |
en_US |
dc.contributor.author |
Wood, E. |
en_US |
dc.date.accessioned |
2004-09-17T18:59:51Z |
|
dc.date.available |
2004-09-17T18:59:51Z |
|
dc.date.issued |
2003-03-08 |
en_US |
dc.identifier.citation |
2003 IEEE Aerospace Conference |
en_US |
dc.identifier.citation |
Big Sky, MT, USA |
en_US |
dc.identifier.clearanceno |
02-2667 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/10600 |
|
dc.description.abstract |
Spacecraft engineers often rely on specialized simulation tools to facilitate the analysis, design and operation of space systems. Unfortunately these tools are often designed for one phase of a single mission and cannot be easily adapted to other phases or other misions. The Multi-Mission Pace Vehicle Susbsystem Analysis Tools are designed to provide a solution to this problem. |
en_US |
dc.format.extent |
3304994 bytes |
|
dc.format.mimetype |
application/pdf |
|
dc.language.iso |
en_US |
|
dc.subject.other |
multi-mission spacecraft subsystem |
en_US |
dc.title |
Multi-mission space vehicle subsystem analysis tools |
en_US |