Evolution of the space shuttle from previous spacecraft systems dictated growth and innovative design of previously standard ordnance devices. Initially, one bolt design was programmed for both 747 and external tank application. However, during development and subsequent analyses, two distinct designs evolved. The unique requirements of both bolts include: high combined loading, redundant initiation, flush separation plane, self-righting and shank attenuation. Of particular interest are the test methods, problem areas, and use of subscale models which demonstrated feasibility at an early phase in the program. The techniques incorporated in the shuttle orbiter bolts are applicable to other mechanisms.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space Shuttle orbiter separation bolts


    Contributors:


    Publication date :

    1979-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Space Shuttle Orbiter Barricade

    P. R. Digiovanniantonio | NTIS | 1974



    Space Shuttle Orbiter ECLSS.

    Stoll, O. T. / Laubach, G. E. / Gibb, J. W. | NTRS | 1973



    Space shuttle orbiter avionics

    Carrier, L.M. / Minor, R.G. | Tema Archive | 1977