A flight rated liquid cooled garment system for use inside a full pressure suit has been designed, fabricated, and tested. High temperature tests with this system have indicated that heat is absorbed at a rate decreasing from 224 kg-cal/hr to 143 kg-cal/hr over a 40-min period. The first 30 min are very comfortable; thereafter a gradual heat load builds that results in mild sweating at the end of the 40-min period. In flight tests during hot weather when this cooling system was worn under a regulation flight suit, the pilot reported that temperatures were comfortable and that the garment prevented sweating.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A flight-rated liquid-cooled garment for use within a full-pressure suit


    Beteiligte:
    Carpenter, R. (Autor:in) / Winter, W. R. (Autor:in)


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Water-cooled space suit

    Jennings, D.C. | Engineering Index Backfile | 1966


    Water-cooled space suit.

    JENNINGS, D. C. | AIAA | 1966



    FLIGHT SUIT

    SAVOIE NICOLE / HUOT STEPHAN | Europäisches Patentamt | 2020

    Freier Zugriff