This specification covers the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison. This Aerospace Recommended Practice is intended to provide general guidelines for the design, development, and qualification of aircraft, tank mounted fuel booster pumps. This revision adds references to SAE documents ARP594 and ARP6385 which provide additional details on proper methods for thermal, mechanical, and electrical safety design of pump components.


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    Title :

    Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard


    Publication date :

    2018-05-16



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English








    DESIGN, TESTING OF CENTRIFUGAL FUEL PUMP FOR LIQUID PROPELLANT ROCKET ENGINE L75

    Reis, Ronaldo C. / Silva, Lucas D. / Pagliuco, Cristiane M. et al. | TIBKAT | 2019