The program objective is to develop a family of solid propellants based on HTPB (hydroxyl terminated polybutadiene) binder, and demonstrate one optimized propellant formulation by large scale motor testing. Phase I data on DL-H271, an analog of TP-H1136, showed exceptionally fine structural properties after 27 months of aging at 75 and 135F. Additional data is presented for Phase II aging. The TU775/03 structural test vehicle was instrumented and cast with TP-H1139 propellant. (Author)


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    Title :

    Development of HTPB Propellant for Ballistic Missiles


    Contributors:
    G. Thompson (author) / E. E. Day (author)

    Publication date :

    1974


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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