– This study aims to present a method for conceptual design and simulation of hybrid propellant motors.

    Design/Methodology/Approach

    – The design methodology is based on previous studies and thermo-physical governor relations, and also a computational code that was derived to simulate the performance of designed system.

    Findings

    – Conceptual design algorithm for space hybrid propellant systems and method of performance simulation are findings of this study.

    Practical implications

    – Results of this study are applicable for design process of space systems with hybrid propulsion. Also, simulation results can help the users to improve the performance weaknesses.

    Originality/value

    – This study shows the implementation of present algorithm for a specified space mission and also study on variation of performance parameters.


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    Title :

    Conceptual design and performance simulation of a space hybrid motor


    Contributors:


    Publication date :

    2015-01-05


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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