A liquid injection thrust vector control (LITVC) system for the shuttle solid rocket booster (SRB) was analyzed. The LITVC was compared with the SRB baseline flexible seal. A table of LITVC advantages and disadvantages is presented. It is concluded that the LITVC performs well at low to moderate duty cycles, but not for high duty cycle requirements.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Feasibility study of LITVC for shuttle SRB


    Beteiligte:
    Martin, C. L. (Autor:in) / Powers, L. B. (Autor:in)

    Erscheinungsdatum :

    1981-09-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Shuttle seated extraction feasibility study

    Onagel, Steven R. / Bement, Laurence J. | NTRS | 1989


    Feasibility Study of LITVC for Shuttle SRB

    C. L. Martin / L. B. Powers | NTIS | 1981



    Flight feasibility assessment of shuttle/LANDSAT-D missions

    Kincade, R. E. / Wortham, M. B. | NTRS | 1980