Spacecraft on-orbit deployment anomalies: What can be done?
- 1 April 1993
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Aerospace and Electronic Systems Magazine
- Vol. 8 (4) , 3-15
- https://doi.org/10.1109/62.210636
Abstract
On-orbit anomalies related to the deployment of spacecraft appendage and possible causes of such failures are considered. The discussion covers mechanical launch loading, on-orbit thermal and solar concerns, reliability of spacecraft pyrotechnics, and practical limitations of ground-based deployment testing. Lessons learned from the successful recovery of the Telesat Canada Anik-E2 satellite in 1991 are examined.Keywords
This publication has 3 references indexed in Scilit:
- Tribological design-The spacecraft industryPublished by Elsevier ,1989
- Some experiences of thermal vacuum testing of spacecraft mechanismsVacuum, 1987
- Abatement of gaseous and particulate contamination in a space instrumentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983