Flexible joints have been used to achieve thrust vector control over a wide range of sizes of nozzles and have been demonstrated successfully in bench tests and static firings, and are operational on two motors. From these many joints the problems of flexible joints have been defined as establishment of the movable nozzle envelope, definition of the actuation power requirements, definition of the mechanical properties of joint materials, adhesive bonding, test methods, and quality control. These data and problem solutions are contained in a large number of reports. Data relating to joint configuration, design requirements, materials selection, joint design, structural analysis, manufacture, and testing are summarized.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flexible joints for thrust vector control


    Beteiligte:

    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





    Thrust Vector Control Flex Joints-Commercial Applications

    Reinhardt, Charles M. / Herbert, John T. | SAE Technical Papers | 1974


    Thrust vector control

    SEIFERT JOST | Europäisches Patentamt | 2017

    Freier Zugriff

    Thrust Vector Control

    P. Quevauviller | NTIS | 1967


    Thrust vector control mechanism

    GOLDMAN ELLIOT / GORDON JASON / ROSENBLAD NATHAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff