The recent fusion of decades of advancements in mathematical models, numerical algorithms and curve fitting techniques marked the beginning of a new era in the science of simulation. It is becoming indispensable to the study of rockets and aerospace analysis. In pneumatic system, which is the main focus of this paper, particular emphasis will be placed on the efforts of compressible flow in Attitude Control System of sounding rocket.


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    Titel :

    Dynamic Analysis of Sounding Rocket Pneumatic System Revision


    Beteiligte:
    Armen, Jerald (Autor:in)

    Erscheinungsdatum :

    08.06.2010


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch