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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    Titel :

    Development of HTPB Propellant for Ballistic Missiles


    Beteiligte:
    G. Thompson (Autor:in) / E. E. Day (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    47 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Development of HTPB Propellant for Ballistic Missiles

    G. Thompson / E. E. Day | NTIS | 1974


    HTPB Propellant Aging

    A.G. Christiansen / L.H. Layton / R.L. Carpenter | AIAA | 1981


    Aging of HTPB Propellant

    Kivity, Moshe / Hartman, Gadi / Achlama, Abraham | AIAA | 2005


    Development of HTPB binder for solid propellant

    KOSAKA, KATSUAKI / SUZUKI, SHIGERU / FUKUMA, DAIZO et al. | AIAA | 1988


    Ballistic Missiles

    L. N. Pronin | NTIS | 1970