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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space shuttle booster separation motor design


    Beteiligte:
    Smith, G. W. (Autor:in) / Chase, C. A. (Autor:in)

    Kongress:

    Propulsion Conference ; 1976 ; Palo Alto, CA


    Erscheinungsdatum :

    01.07.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space shuttle booster separation motor design

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




    Shuttle booster separation aerodynamics

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