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.


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    Title :

    Spacecraft Two-Phase Thermal Control System Simulation


    Additional title:

    Sae Technical Papers



    Conference:

    International Conference On Environmental Systems ; 1997



    Publication date :

    1997-07-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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