This report describes the steps involved in the design and evaluation of the FMU-90/B point-detonating delay fuze for the 2.75-inch folding-fin aircraft rocket (FFAR). Beginning with a summary of the performance requirements of this fuze, it discusses various phases of the development of the fuze. Formal laboratory evaluation and results of high-speed track and ground-launch tests of the fuze are summarized. The design, development, and qualification testing of a stab-initiated 50-millisecond delay primer is included. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and Evaluation of the FMU-90/B Point-Detonating Delay Fuze for the 2.75-Inch Folding-Fin Aircraft Rocket


    Beteiligte:
    F. W. Schwarz (Autor:in)

    Erscheinungsdatum :

    1970


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    2.75-In. Folding Fin Aircraft Rocket. Volume 1

    G. Dolgonas / H. A. Krayenbuhl | NTIS | 1969



    An Improved Canadian 2.75-Inch Rocket Motor

    F. Jackson / F. A. Christie / M. N. Clark et al. | NTIS | 1976