This paper summarizes the impacts on the weight, volume and power usage of a manned space station and its 90-day resupply for three integrated, auxiliary propulsion subsystems. The study was performed in coordination with activities of the Space Station Concept Development Group (CDG). The study focused on three space station propulsion high-low thrust options that make use of fluids that will be available on the manned space station. Specific uses of carbon dioxide, water and cryogen boiloff were considered. For each of the options the increase in station hardware mass and volume to accommodate the dual thrust option is offset by the resupply savings, relative to the reference hydrazine system, after one to several resupplies. Over the life of the station the savings in cost of logistics could be substantial. The three options are examples of alternative technology paths that, because of the opportunity they provide for integration with the environmental control life support system (ECLSS) and OTV propellant storage systems, may reduce the scarring which is required on the early station to meet the increasing propulsion requirements of the growth station.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space Station propulsion analysis study


    Contributors:

    Publication date :

    1984-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Space station propulsion analysis study

    Donovan, R. M. / Sovey, J. S. / Hannum, N. B. | NTRS | 1984


    Space Station propulsion analysis study

    DONOVAN, R. / SOVEY, J. / HANNUM, N. | AIAA | 1984


    Space station propulsion requirements study

    Wilkinson, C. L. / Brennan, S. M. | NTRS | 1985


    Space Station Propulsion Requirements Study

    C. L. Wilkinson / S. M. Brennan | NTIS | 1985


    Space Station Propulsion

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