For passive flow rate control of oxidizer and fuel of a liquid propellant engine a cavitating venturi is designed, produced and tested.


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    Title :

    Passive flow rate control of the fuel and the oxidizer in liquid fuelled rocket motors


    Contributors:
    Yazici, B. (author) / Gunduz, D.E. (author) / Puskulcu, G. (author) / Yildirim, C. (author) / Sumer, B. (author) / Orhan, F.E. (author) / Gonc, L.O. (author) / Ak, M.A. (author)


    Publication date :

    2005-01-01


    Size :

    536769 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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