Abstract This chapter discusses the time-dependent thrust modulation process of the fluidic throat for engineering applications. It is necessary to learn the thrust modulation of the fluidic throat and the unsteady process of the mainstream flux. It is directly related to the thrust modulation characteristic of the fluidic-throat nozzle and its proper operating mode. Typical internal ballistic results under different operating conditions are introduced in the following sections, including calculation method of internal ballistics, modulation process at fixed mass flow rates, unsteady process for the axial-gap fluidic throat, and thrust modulation for the hole-type fluidic throat in hot test conditions.


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    Title :

    Thrust Modulation Process of Fluidic Throat for Solid Rocket Motors


    Contributors:
    Xie, Kan (author) / Chen, Xinmin (author) / Li, Junwei (author) / Liu, Yu (author)


    Publication date :

    2019-01-01


    Size :

    12 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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