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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    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





    Interdisciplinary Analysis from the Spacecraft Thermal Analyst's Viewpoint

    Humphries, W. Randolph | SAE Technical Papers | 1992



    ELECTRIC VACUUM PUMP CONTROL UNIT

    SEKIYA YOSHIHIDE / OZAKI SHOJI | European Patent Office | 2016

    Free access

    Electrochemically-driven Fluid Pump for Spacecraft Thermal Control

    Reeh, Jonathan / van Boeyen, Roger | SAE Technical Papers | 2008