Lunar excursion module (LEM) environmental control system (ECS) is comprised of atmosphere revitalization, oxygen supply, cabin pressure control, heat transport, water management, and cold plates; description of LEM system sections, checkout phases before and during orbit, and operational sequences with regard to in-flight mission; ECS in-flight instrumentation, compatible with operational procedures, is restricted to spacecraft performance and management, crew safety functions to assist in making abort decision, status of expendable items, and indications of switch to back-up equipment.


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    Titel :

    In-flight checkout of LEM environmental control system


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Cytryn, E.P. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Life support systems



    Erscheinungsdatum :

    1964


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    In Flight Checkout of the LEM Environmental Control System

    Cytryn, E. P. | SAE Technical Papers | 1964



    Transceiver In-Flight Checkout System

    Halm, R. / Spallicci, A. / Hahne, A. | SPIE | 1987



    On-Board In-Flight Checkout

    J. L. Johnson / D. P. Blowney / E. W. Methlie et al. | NTIS | 1967