The paper considers an electric pump unit of the spacecraft thermal control system. The aim of the work is to create a simulation model, which allows analyzing the distribution of temperature fields and the stress-strain state in the electric pump structure. The influence of structural materials on the transient behavior is also investigated for the changing the heat transfer agent temperature in the system.


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    Title :

    Interdisciplinary Analysis of Transient Processes in the Electric Pump Unit of the Liquid Thermal Control System of the Spacecraft


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 4 ; 598-605


    Publication date :

    2021-10-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English