Various means for crewmen to transfer from pressurized vehicle to space vacuum and concept which provides simple, light weight means to effect such transfers; transfer method comparisons under consideration include cabin decompression vs use of airlock, rigid air-lock construction vs flexible, and internal airlock location vs external; system concept presented uses external, inflatable air-lock which, for insignificant weight penalty, affords major improvements in crew safety, mission completion capability, and vehicle payload capacity.


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    Titel :

    Considerations for manned space vehicle airlock design


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Carlyle, L. (Autor:in) / Duskin, F.E. (Autor:in) / Englar, K.G. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Airlock

    H. R. Linderfelt | NTIS | 1972


    Airlock

    Linderfelt, H. R. | NTRS | 1974


    Airlock Entry

    Frickland, P. O. / Cleland, E. L. | NTRS | 1984


    Airlock

    H. R. Linderfelt | NTIS | 1974


    Positive-pressure airlock system between ship and platform airlock

    HUANG JI / GAN FEIFEI / WU LEI et al. | Europäisches Patentamt | 2020

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