A reusable high-performance rocket engine intended for putting the Space Shuttle orbiter vehicle into earth orbit is described. Three such engines are clustered in the aft end of the orbiter stage. They burn in parallel with the solid-propellant boosters during the initial ascent phase and continue to burn after booster ejection until just prior to orbit insertion. The nominal burn time is roughly 10 min. Propulsion requirements demand maximum performance from liquid oxygen/hydrogen propellants with a minimum hardware weight. The engine design and the present progress made in the development of the engine are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The Space Shuttle Main Engine


    Beteiligte:

    Kongress:

    International Astronautical Congress ; 1973 ; Baku, Azerbaidzhan SSR


    Erscheinungsdatum :

    01.10.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Shuttle Main Engine

    Thompson, J. R., Jr. | NTRS | 1980


    Space Shuttle Main Engine

    Thompson, J. R., Jr. | NTRS | 1977


    Rocketdyne's space shuttle main engine

    CASTENHOLZ, P. | AIAA | 1971


    Space Shuttle Main Engine. Overview

    E. D. Jackson | NTIS | 1993


    Space Shuttle Main Engine Controller

    R. M. Mattox / J. B. White | NTIS | 1981