Designing with solid propellants is simpler than with liquid propellants; most of design parameters are set by knowing thrust and operating time; this information determines amount of propellant to be burned and, with given propellant formulation, suggests most other design criteria; relative importance of various design parameters; motor construction.


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    Titel :

    Factors in solid missile booster design


    Weitere Titelangaben:

    Aero Digest


    Beteiligte:

    Erschienen in:

    Aero Digest ; 71 , n 2


    Erscheinungsdatum :

    1955


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Missile and booster directory

    Engineering Index Backfile | 1962



    SOLID ROCKET BOOSTER INTEGRATION WITH THE AQM-37C MISSILE TARGET

    Cumbo, F. M. / United States | British Library Conference Proceedings | 1990


    Missile Booster Device and Attachments Therefor

    E. D. Legg / H. W. Kupetzky | NTIS | 1965