A solid rocket motor includes a propellant grain structure defining an axial bore and a vortex inducing feature.


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    Title :

    Solid rocket motor with vortex inducing feature


    Contributors:

    Publication date :

    2021-01-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS



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