The International Space Station's primary external heat transport system is a single phase ammonia loop called the Active Thermal Control System (ATCS). ATCS loop heat is acquired from the station modules through interface heat exchangers (Internal Thermal Control System water to ATCS ammonia) and from external truss mounted electronics through cold plates. The heat exchangers are compact plate/fin counterflow type and the cold plates are a brazed and bonded construction using a radiation heat transfer interface to the electronics.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    ISS Active Thermal Control System(ATCS) Heat Exchangers and Cold Plates


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Dellinger, Brent (Autor:in) / Taddey, Ed (Autor:in) / Tongue, Stephen (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1997



    Erscheinungsdatum :

    1997-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    ACCURATE TEMPERATURE CONTROL SYSTEM (ATCS)

    DANG QUOC HUNG | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft engines (without ATCs)

    Engineering Index Backfile | 1941


    Aircraft engines (with ATCs)

    Engineering Index Backfile | 1941


    S.F. Muni Resignals to ATCS

    Moy, B. L. / DeVlieg, P. G. / American Public Transit Association | British Library Conference Proceedings | 1994


    Control Stability Analysis Applied to Columbus ATCS

    Persson, Jan / De Palo, Savino / Klingberg, Tor | SAE Technical Papers | 2009