Impacts of mission-related requirements on design of the J402-CA-400 missile propulsion turbojet engine are reviewed. Small-engine cost scaling rationale is presented in relation to engine thrust and functional requirements. The application of current casting technology toward achieving low cost is reviewed.


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    Title :

    Turbine Powerplants for Missiles - Cost Improvement Requirements


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Air Transportation Meeting ; 1973



    Publication date :

    1973-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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