The Space Shuttle RCS (reaction control system) is required to provide propulsion thrust for precise attitude control and three-axis translation. This capability must be provided for external tank separation, on-orbit operation, deorbit, and reentry. In order to meet these requirements a bipropellant, pressure-fed system utilizing monomethylhydrazine as fuel, and nitrogen tetroxide as oxidizer has been selected. The RCS engines include 38 primary thrusters rated at 870 lbf thrust and 6 vernier thrusters rated at 25 lbf thrust. The system is divided into three removable modules (one forward and two aft) to achieve maintenance and turnaround requirements. In order to provide additional mission flexibility, the aft modules can be connected together or interconnected with the OMS (orbital maneuvering system).


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    Titel :

    Description of the Space Shuttle Reaction Control System


    Beteiligte:
    Blevins, D. R. (Autor:in) / Hohmann, C. W. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics and Society of Automotive Engineers, Propulsion Conference ; 1975 ; Anaheim, CA


    Erscheinungsdatum :

    01.09.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Description of the Space Shuttle Reaction Control System

    BLEVINS, D. / HOHMANN, C. | AIAA | 1975


    Space Shuttle Reaction Control System

    Vaughan, Chester A. / Kendrick, Darrell / Pohl, Henry O. | SAE Technical Papers | 1970


    Space shuttle reaction control system

    Kendrick, D. / Pohl, H. O. / Vaughan, C. A. | NTRS | 1970