The benefits of the utilization of effluents of the Space Station Environmental Control and Life Support (ECLS) system are examined. Various ECLSS-propulsion system interaction options are evaluated and compared on the basis of weight, volume, and power requirements. Annual propulsive impulse to maintain station altitude during a complete solar cycle of eleven years and the effect on station resupply are considered.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space station propulsion-ECLSS interaction study


    Contributors:

    Publication date :

    1986-02-14


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English