The report is concerned with stability and control of the helicopter when used as a weapons platform for aerodynamically stabilized rockets. Analysis and simulation are used to ascertain problem areas that exist when engagement techniques similar to those used for fixed wing aircraft are used for helicopters. It is shown that significant improvements in helicopter controllability and rocket accuracy can be achieved by utilizing an impact prediction calculation which accounts for the relative wind on the rocket launching tubes. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stability and Control of the Helicopter When Used as a Weapons Platform for Aerodynamically Stabilized Rockets


    Beteiligte:
    R. W. Campagna (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    115 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design of aerodynamically stabilized free rockets

    USA, Army Materiel Command | TIBKAT | 1968


    Aerodynamically stabilized instrument platform

    Bland, Geoffrey L. / Miles, Ted K. | NTRS | 2012


    Modeling aerodynamically generated sound of helicopter rotors

    Brentner, Kenneth S. | Online Contents | 2003



    Aerodynamically Efficient Rotor Design for Hovering Agricultural Unmanned Helicopter

    B. A. Haider / C. H. Sohn / Y. S. Won et al. | DOAJ | 2017

    Freier Zugriff