The technology effort required for the development of a propellant scavenging system is identified. For a cryogenic propellant system, the development tests identified are for a cryogenic capillary acquisition system for zero-g feedout capability and for definition of existing Space Transformation System (STS) performance capabilities. For a storable propellant system, the development tests identified are for three major components required in the system: a propellant pump, a helium compressor, and a zero leakage fluid disconnect.


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    Title :

    Space Transportation System (STS) propellant scavenging system study. Volume 2: Supporting research and technology report


    Publication date :

    1985-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English