The Rotor Systems Research Aircraft (RSRA) was flown in the airplane configuration. Eleven successful flights were made from May 8 to October 3, 1984. The takeoff and landing method was demonstrated and the resultant parameters were obtained. Control power data were obtained. In addition, main rotor hub drag, airplane configuration acoustics data, and aircraft stability data were obtained. Hub drag, acoustics, and stability will be separately reported in more detail. The tail rotor was installed for all tests.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    RSRA flight development test in the airplane configuration


    Beteiligte:
    Erickson, R. E. (Autor:in) / Kufeld, R. M. (Autor:in) / Cross, J. L. (Autor:in) / Acree, C. W. (Autor:in)

    Erscheinungsdatum :

    01.01.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    RSRA flight control and stabilization

    Linden, A. W. | NTRS | 1976


    RSRA/X-Wing flight control system development - Lessons learned

    Corliss, Lloyd D. / Dunn, William R. / Morrison, Michael A. | NTRS | 1989


    RSRA Vertical Drag Test Report

    R. J. Flemming | NTIS | 1981


    Flight Testing the Rotor Systems Research Aircraft (RSRA)

    G. W. Hall / R. K. Merrill | NTIS | 1983


    RSRA vertical drag test report

    Flemming, R. J. | NTRS | 1981