Propellant actuated devices, originally developed for use in conventional aircraft, were subjected to special vibration tests in order to qualify them for use in the Dyna-Soar (X20) Escape System. Four initiators were developed for use in the system and the ejection seat catapult was tested under high g loads to determine safety of the defice if initiated during high down-load conditions. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Dyna-Soar Escape System Propellant Actuated Devices


    Contributors:

    Publication date :

    1965


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Dyna-Soar Bioastronautics

    Robert Y Walker | NTRS | 1962


    Dyna soar research objectives

    Anderton, Jr., F.R. | Engineering Index Backfile | 1960


    PERT in dyna-soar

    Senecal, T.L. / Sadow, R.M. | Engineering Index Backfile | 1962



    Dyna-Soar aerodynamic performance

    Lesko, J. S. | NTRS | 1960