Element-wound materials are useful from viewpoint of weight saving when used for aerospace vehicles; application of filament-wound rocket motor chamber is considered; it is necessary that chamber must be proof-tested up to high internal pressure, close to burst pressure; experimental verification concerning low-cycle fatigue is described.


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    Titel :

    Low cycle fatigue of filament wound composites


    Weitere Titelangaben:

    Tokyo. Univ -- Inst Space Aeronautical Science -- Bul


    Beteiligte:
    Kobayashi, A. (Autor:in) / Otani, N. (Autor:in) / Kawata, K. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Preliminary experimental study on low cycle fatigue of filament-wound composites

    Kobayashi, A. / Otani, N. / Kawata, K. | Engineering Index Backfile | 1968


    Cycle testing of boron filament wound tanks

    Alfring, R. J. / Morris, E. E. / Landes, R. E. | NTRS | 1971


    Cycle Testing of Boron Filament Wound Tanks

    R. J. Alfring / E. E. Morris / R. E. Landes | NTIS | 1971


    High Temperature Matrices for Filament Wound Composites

    Rushing, R. A. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 2005