The separation characteristics of the space shuttle solid rocket boosters (SRBs) are introduced along with the system level requirements for the booster separation motors (BSMs). These system requirements are then translated into specific motor requirements that control the design of the BSM. Each motor component is discussed including its geometry, material selection, and fabrication process. Also discussed is the propellant selection, grain design, and performance capabilities of the motor. The upcoming test program to develop and qualify the motor is outlined.


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    Title :

    Space shuttle booster separation motor design


    Contributors:
    Smith, G. W. (author) / Chase, C. A. (author)

    Conference:

    Propulsion Conference ; 1976 ; Palo Alto, CA


    Publication date :

    1976-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Space shuttle booster separation motor design

    SMITH, G. / CHASE, C. | AIAA | 1976



    Shuttle booster separation aerodynamics

    Craig, M. K. / Dresser, H. S. | NTRS | 1983