Approach for combining spacecraft attitude and thermal control systems

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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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Bibliographic Details
Main Authors:	Varatharajoo, Renuganth, Kahle, Ralph, Fasoulas, Stefanos
Format:	Article
Published:	American Institute of Aeronautics and Astronautics 2003
Online Access:	http://psasir.upm.edu.my/id/eprint/113031/

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