Significant findings of the Highly Maneuverable Aircraft Technology Remotely Piloted Research Vehicle (HiMAT RPRV) flight test program are presented. Among the topics covered are: aerodynamic scaling relationships, the aeroelastic tailoring of wing and canard twist and camber, and laminate graphite/epoxy composite primary structure performance under high-g loading maneuvers. Attention is also given to the set of actuators used in the test and development program, with a view to the minimization of costs through modularity and interchangeability of components and the extensive use of off-the-shelf equipment. The relationship between composite ply geometry and the shape and magnitude of aeroelastic deformations during maneuvering is discussed in detail.


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    Titel :

    HiMAT systems development results and projections


    Beteiligte:
    Brown, L. E., Jr. (Autor:in) / Roe, M. H. (Autor:in) / Quam, R. A. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1980 ; Los Angeles, CA


    Erscheinungsdatum :

    1980-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    HiMAT Systems Development Results and Projections

    Brown, L. E. / Roe, M. H. / Quam, R. A. | SAE Technical Papers | 1980


    The HiMAT RPRV system

    BROWN, JR., L. / ROE, M. / WILER, C. | AIAA | 1978


    Qualification of HiMAT flight systems

    Myers, A. F. / Sheets, S. G. | NTRS | 1980


    RPRV research focus on HiMAT

    Lockenour, J. L. / Layton, G. P. | NTRS | 1976