Oxygen/hydrogen propulsion system options for space station orbit maintenance and attitude control were developed and evaluated relative to monopropellant and storable bipropellant propulsion systems. Space station propulsion requirements were analyzed with reference to such considerations as station size, altitude, power, crew size, and orbit transfer vehicle and orbital maneuvering vehicle servicing requirements. The evolutionary growth of oxygen/hydrogen bipropellant propulsion as an integral part of several interrelated space station functions, e.g., life support, power, and thermal management was considered. Propellant resupply evolves from resupply based on transport of liquid oxygen and liquid hydrogen to water. The advantages of the operation of the space station based on an oxygen/hydrogen economy are presented and discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Integratable propulsion systems for the Space Station


    Beteiligte:
    Rosenberg, S. D. (Autor:in) / Judd, D. C. (Autor:in) / Garrison, P. W. (Autor:in)


    Erscheinungsdatum :

    01.02.1985



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Integratable propulsion systems for the Space Station

    ROSENBERG, S. D. / JUDD, D. C. / GARRISON, P. W. | AIAA | 1985


    Integratable ILS interlock system

    CASTELLANOS KEN J / DAVIS LARRY K | Europäisches Patentamt | 2017

    Freier Zugriff

    Multi-gauge pod integratable within motorcycle windscreen

    PEREZ CARLOS ARIEL | Europäisches Patentamt | 2016

    Freier Zugriff

    Space station propulsion

    Jones, Robert E. / Morren, W. Earl / Sovey, James S. et al. | NTRS | 1987


    Space Station Propulsion

    R. E. Jones / W. E. Morren / J. S. Sovey et al. | NTIS | 1987