A thermoelectric liquid cooling system recently developed at the Johnson Space Center was evaluated in manned and unmanned ground tests as an alternative to the Space Shuttle launch and entry suit personal fan. The liquid cooling system provided superior cooling in environments simulating flight deck conditions during launch and postlanding.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Shuttle Launch Entry Suit Liquid Cooling System Thermal Performance


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Sauser, Bruce (Autor:in) / Conger, Bruce C. (Autor:in) / Chang, Chi-Min (Autor:in) / Bue, Grant C. (Autor:in) / Hooper, Philip E. (Autor:in)

    Kongress:

    International Conference on Environmental Systems ; 1995



    Erscheinungsdatum :

    1995-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Space Shuttle Launch Entry Suit Thermal Performance Evaluation

    Conger, Bruce C. / Sauser, Bruce W. / Chang, Chi-Min et al. | SAE Technical Papers | 1993




    Reach performance while wearing the Space Shuttle launch and entry suit during exposure to launch accelerations

    Bagian, James P. / Greenisen, Michael C. / Schafer, Lauren E. et al. | NTRS | 1993


    Reach Performance While Wearing the Space Shuttle Launch and Entry Suit During Exposure to Launch Accelerations

    Probe, J. D. / Bagian, J. P. / Schafer, L. E. et al. | SAE Technical Papers | 1990