Approach for combining spacecraft attitude and thermal control systems
Coupling of existing spacecraft subsystems could be an alternative to reduce the emerging cost, decrease the system volume/mass and complexity, increase the reliability, and enhance the overall performance of future spacecraft. Therefore, a new concept to combine the attitude and thermal control sys...
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| Main Authors: | , , |
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| Format: | Article |
| Published: |
American Institute of Aeronautics and Astronautics
2003
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| Online Access: | http://psasir.upm.edu.my/id/eprint/113031/ https://arc.aiaa.org/doi/10.2514/2.6914 |
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