A road map of milestones toward the goal of a full scale Redesigned Solid Rocket Motor/Flight Support Motor (RSRM/FSM) hot fire test is discussed. These milestones include: component feasibility, full power system demonstration, SSME hot fire tests, and RSRM hot fire tests. The participation of the Marshall Space Flight Center is emphasized.


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    Titel :

    Development and test of electromechanical actuators for thrust vector control


    Beteiligte:
    Weir, Rae A. (Autor:in) / Cowan, John R. (Autor:in)

    Kongress:

    AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States


    Erscheinungsdatum :

    1993-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Design and Test of Electromechanical Actuators for Thrust Vector Control

    Cowan, J. R. / Weir, R. A. / United States et al. | British Library Conference Proceedings | 1993



    Transient Force Reduction in Electromechanical Actuators for Thrust-Vector Control

    Dale E. Schinstock / Douglas A. Scott / Tim A. Haskew | AIAA | 2001