Erectable/deployable space structure concepts particularly relating to the development of a science and applications space platform are presented. Design and operating features for an automatic coupler clevis joint, a side latching detent joint, and a module-to-module auto lock coupler are given. An analysis of the packaging characteristics of stacked subassembly, single fold, hybrid, and double fold concepts is given for various platform structure configurations. Payload carrier systems and assembly techniques are also discussed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Erectable/deployable concepts for large space system technology


    Contributors:
    Agan, W. E. (author)


    Publication date :

    1980-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Deployable and erectable concepts for large spacecraft

    Bush, H. G. / Heard, W. L., Jr. / Walz, J. E. et al. | NTRS | 1980




    Space erectable radiator system development

    OREN, J. / HOLMES, H. | AIAA | 1988


    Structural and assembly concepts for large erectable space systems

    Katz, E. / Kruszewski, E. T. / Naumann, E. C. | NTRS | 1978