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A Pulsed Detonation Microthruster for Space Applications
- Source :
- 29th International Symposium on Shock Waves 1 ISBN: 9783319168340
- Publication Year :
- 2015
- Publisher :
- Springer International Publishing, 2015.
-
Abstract
- The majority of microsatellites in orbit do not have a propulsion system, which greatly limits their flexibility and their ability to perform complex tasks. Ambitious future missions will need the capability to produce the thrust required for either orbit change, drag makeup, station keeping or attitude control, and this usually requires more than one propulsion system [1].
Details
- ISBN :
- 978-3-319-16834-0
- ISBNs :
- 9783319168340
- Database :
- OpenAIRE
- Journal :
- 29th International Symposium on Shock Waves 1 ISBN: 9783319168340
- Accession number :
- edsair.doi...........e7ea542882a653fa0fee38ffebf3639b