The design, analysis, fabrication and testing of a Kevlar-49/HBRF-55A filament wound chamber is reported. The chamber was fabricated and successfully tested to 80% of the design burst pressure. Results of the data reduction and analysis from the hydrotest indicate that the chamber design and fabrication techniques used for the chamber were adequate and the chamber should perform adequately in a static test.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Filament wound rocket motor chambers


    Erscheinungsdatum :

    01.09.1976


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    In-House Research on Filament Wound Rocket Motor Cases

    Namiki, F. / Miyagawa, K. / Yamamoto, Y. | British Library Conference Proceedings | 1996




    Development of boron epoxy rocket motor chambers.

    Jensen, W. M. / Knoell, A. C. / Zweben, C. | NTRS | 1972


    Development of Filament Wound M-34 Rocket Motor Casing for M-V Satellite Launcher

    Onoda, J. / Minesugi, K. / Nakamura, M. et al. | British Library Conference Proceedings | 1994