This paper deal with the thermal design features of the Tethered Satellite Module, according to the project development status of the advanced Phase B. A description of TSM typical mission characteristics, thermal requirements and constraints and the proposed thermal control design will be given. The thermal analytical models, the subsystem performances and the more representative temperature predictions will be presented with emphasis to special features which may occur.
Thermal Control of the Tethered Satellite Module
Sae Technical Papers
Intersociety Conference on Environmental Systems ; 1983
1983-07-11
Conference paper
English
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