Fluid-flow components in a liquid propellant rocket engine and the rocket vehicle which it propels are interconnected by lines, bellows, and flexible hoses. Elements involved in the successful design of these components are identified and current technologies pertaining to these elements are reviewed, assessed, and summarized to provide a technology base for a checklist of rules to be followed by project managers in guiding a design or assessing its adequacy. Recommended procedures for satisfying each of the design criteria are included.


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    Title :

    Liquid Rocket Lines, Bellows, Flexible Hoses, and Filters


    Publication date :

    1977


    Size :

    186 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English