This report describes the test firing of a thrust vector control system (TVC) on the AFRPL 40-inch-diameter Char Motor. The TVC system consisted of a movable exit cone (Flex-X) nozzle and support hardware, which was designed to combine the advantages of the elastomeric seal with those of the supersonic split-line nozzle. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flexible Exit Cone Nozzle Demonstration Firing Results


    Beteiligte:
    J. R. Ellison (Autor:in) / S. J. Ojala (Autor:in)

    Erscheinungsdatum :

    1969


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flexible Exit Cone Nozzle Firing

    S. J. Ojala / J. R. Ellison | NTIS | 1970



    Flexible Exit Cone Nozzle Development Program

    J. W. Wilson / C. W. Wright | NTIS | 1968



    IUS nozzle and extendible exit cone development

    HALL, R. / MORROW, O. / CROWE, G. et al. | AIAA | 1980