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.


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    Title :

    Space Station Propulsion-Eclss Interaction Study


    Contributors:

    Publication date :

    1986


    Size :

    92 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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