A spacecraft module, to be integrated with the FLTSATCOM spacecraft, was tested in a simulated orbit environment separate from the host spacecraft. Thermal vacuum testing of the module was accomplished using internal IR heating rather than conventional external heat sources. For this configuration, the technique produced boundary conditions expected for flight to enable verification of system performance and thermal design details.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thermal testing by internal IR heating of the FEP module


    Beteiligte:
    Nathanson, D. M. (Autor:in) / Efromson, R. A. (Autor:in) / Lee, E. I. (Autor:in)


    Erscheinungsdatum :

    1986-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    HEATING MODULE HEATING SYSTEM AND VEHICLE INCLUDING HEATING MODULE AND HEATING SYSTEM

    JI JOON DONG / AN JIN HYOK | Europäisches Patentamt | 2018

    Freier Zugriff

    Impact of Internal Heating on Spacecraft Thermal Signature

    Carnahan, Scott / Schaub, Hanspeter / Lane, Benjamin | TIBKAT | 2019


    BATTERY MODULE THERMAL MANAGEMENT FEATURES FOR INTERNAL FLOW

    OBASIH KEM M / DEKEUSTER RICHARD M | Europäisches Patentamt | 2023

    Freier Zugriff

    HEATING MODULE

    JI JUN DONG / AN JIN HYOK | Europäisches Patentamt | 2018

    Freier Zugriff

    Battery module thermal management features for internal flow

    OBASIH KEM M / DEKEUSTER RICHARD M | Europäisches Patentamt | 2020

    Freier Zugriff