The results of computer simulation of a typical spacecraft pumped two-phase thermal control system are presented. The two-phase thermal control system transients under effect of the typical disturbances are obtained. The system dynamic characteristics are analyzed and influence of design parameters on the quality of system dynamic processes are discussed.
Spacecraft Two-Phase Thermal Control System Simulation
Sae Technical Papers
International Conference On Environmental Systems ; 1997
1997-07-01
Conference paper
English
TIBKAT | 2012
|SLUB | 2012
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