The dynamics of intrachamber processes in a type of solid propellant rocket engine under consideration is investigated in order to optimize its parameters. The conjugate statement of the problem at the level of setting up a computational experiment is formulated. The results of numerical calculations are presented, which revealed an anomalous feature of the rocket engine firing process.


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    Title :

    Anomalous Features of Dynamics of Intrachamber Processes in a Low-Thrust Solid Propellant Rocket Engine with a Multi-Grain Propellant Charge


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 4 ; 711-720


    Publication date :

    2021-10-01


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English