Laboratory test is devised to approximate payload vibration response characteristics of Nike Tomahawk system; test is based upon flight test data and apparent weight (WA) characteristics of rocket motors and payload; intermediate tests gave data on payload's vibration response to motor burning irregularities; test procedure included also static firing, force controlled vibration testing and electric simulation of WA during force controlled test; test results and practical limitations of test procedure are considered.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Progress report on force controlled vibration testing


    Weitere Titelangaben:

    U S Naval Research Laboratory -- Shock Vibration Bul


    Beteiligte:
    Nuckolls, C.E. (Autor:in) / Otts, J.V. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Force limited vibration testing

    Scharton, Terry D. | NTRS | 1991


    Response-Controlled Vibration Testing

    Tustin, W. / Aerospace Corporation | British Library Conference Proceedings | 1999


    Force Limited Vibration Testing Monograph

    Scharton, T. D. | NTRS | 1997


    Force Limited Vibration Testing Monograph

    Scharton, Terry D. | NTRS | 1997


    Force Limited Vibration Testing Monograph

    T. D. Scharton | NTIS | 1997