The benefits which would be gained by providing commonality and integration of propulsion and fluid systems associated with various elements of the Space Station are discussed and the results of the integrated propulsion system assessment are presented. The O2/H2 propulsion system with and without resistojets, the integration of O2/H2 systems across the Space Station elements, and an approach for handling waste fluids available for resistojet venting are evaluated. It is shown that major benefits can be gained through commonality and integration. Several systems are recommended, including a gaseous O2/H2 propulsion system with resistojets, a Bosch CO2 reduction process, and pumping electrolysis units.


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    Titel :

    Integration of Space Station propulsion and fluid systems


    Beteiligte:
    Bicknell, B. A. (Autor:in) / Fester, D. A. (Autor:in) / Wilson, S. C. (Autor:in)

    Erscheinungsdatum :

    01.07.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Integration of Space Station propulsion and fluid systems

    BICKNELL, B. / FESTER, D. / WILSON, S. | AIAA | 1988




    Space station integrated propulsion and fluid systems study

    Bicknell, B. / Wilson, S. / Dennis, M. et al. | NTRS | 1988


    Space Station Integrated Propulsion and Fluid Systems Study

    B. Bicknell / S. Wilson / M. Dennis et al. | NTIS | 1988