Current NASA space suits use porous metal plate sublimators to reject the metabolic heat generated by the astronaut into space vacuum during EVA. Relying on tubular membranes instead of the flat plate of the sublimator, a proposed alternate unit has the potential to be smaller and lighter. This work outlines the operation of the proposed tubular membrane evaporator and the evaluation of possible membrane materials for the unit.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Tubular Membrane Evaporator Development for the Plss


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Webbon, Bruce W. (Autor:in) / Lomax, Curtis (Autor:in) / Miles, John B. (Autor:in) / Stone, Patrick L. (Autor:in) / Nair, Satish S. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1996



    Erscheinungsdatum :

    1996-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    PLSS Packaging Design

    Rouen, Michael | SAE Technical Papers | 1999



    PLSS Transient Thermal Modeling for Control

    Campbell, Anthony B. / Webbon, Bruce W. / Miles, John B. et al. | SAE Technical Papers | 1996


    Lessons Learned Briefing PLSS 2.0

    McMann, Joe | NTRS | 2012


    Emergency Oxygen System Evaluation for Exploration PLSS Applications

    Conger, Bruce / Paul, Heather / Vonau, Walt | SAE Technical Papers | 2006