Circular manifold with tangential orifices at the inner circumference provides for the vapor constituent of a vaporized cryogenic propellant to enter a rocket combustion chamber before the liquid constituent. The vapor is separated from the liquid by centrifugal action and precedes it into the chamber through carefully positioned orifices.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Combustion chamber inlet manifold separates vapor from liquid


    Contributors:

    Publication date :

    1966-02-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Plastic inlet manifold

    Ford,GB | Automotive engineering | 1981


    CSS separates presentation from content

    British Library Online Contents | 2004


    Victor separates the spoils

    Online Contents | 2008



    Inlet-Manifold Design and Fuel Utilization

    PETZE, CHARLES LOUIS | SAE Technical Papers | 1929