An airlock is described for use in transferring waste objects from a positively pressurized enclosure aboard an operative space vehicle, to a waste receiver attached to the vehicle and maintained at the negative pressure of a celestial space environment. The airlock is characterized by a shell having an internal chamber and hermetically sealed within an opening formed in a bulkhead of the enclosure. The shell is provided with an insertion hatch adjacent to the enclosure, and an ejection hatch hermetically sealed within an opening formed in a bulkhead of the enclosure. The shell is provided with an insertion hatch adjacent to the enclosure, and an ejection hatch adjacent the waste receiver, each hatch being hermetically sealed by a hatch cover. A three-way selector valve is provided for alternately coupling the chamber with the enclosure and the receiver in response to manipulation of the mechanism.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Airlock


    Beteiligte:

    Erscheinungsdatum :

    1972


    Format / Umfang :

    48 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airlock

    Linderfelt, H. R. | NTRS | 1974


    Airlock

    H. R. Linderfelt | NTIS | 1974


    Airlock Entry

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


    PRESSURE AIRLOCK

    RICHEY STEPHEN / COSTLE CAREY / OJEDA GRANT | Europäisches Patentamt | 2020

    Freier Zugriff

    PRESSURE AIRLOCK

    RICHEY STEPHEN E / COSTLE CAREY C / OJEDA GRANT PETER AJ | Europäisches Patentamt | 2023

    Freier Zugriff