An interactive computer code for the preliminary design of solid propellant rocket motors ('SPRMD') was successfully developed and its use was demonstrated through a design example. 'SPRMD' was written in FORTRAN for use on an IBM PC/AT. It combined several existing codes ('MICROPEP', 'GRAINS', 'ROCKET', etc.) and used the performance loss estimation methods suggested by the AGARD Propulsion and Energetics Panel for aluminized propellants. Keywords: Solid propellant rocket motor, Design.


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    Title :

    Interactive Computer Code for Preliminary Design of Solid Propellant Rocket Motors


    Contributors:
    C. I. Yuan (author)

    Publication date :

    1987


    Size :

    94 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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