Property measurements and fabrication characteristics were determined and the performance in subscale (Minuteman Wing 2 second stage) motors was evaluated. It was demonstrated that the incorporation of low cost fabrication techniques in a full scale 260 in. nozzle could result in savings of $149,000 when compared with an identical design using tape-wrapped components throughout.


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    Title :

    Development of low cost fabrication techniques for large solid rocket nozzles


    Contributors:

    Publication date :

    1971-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English