1–20 of 23 hits
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    Investigation of a side force due to ablation

    RAGSDALE, W. C. / HORANOFF, E. V. | AIAA | 1978

    An evaluation of automatic control system concepts for general aviation airplanes

    STEWART, E. / RAGSDALE, W. / WUNSCHEL, A. | AIAA | 1988

    Preliminary piloted simulation studies of the HL-20 lifting body

    Rivers, Robert A. / Jackson, E. B. / Ragsdale, W. A. | AIAA | 1994

    Utilization of simulation tools in the HL-20 conceptual design process

    Jackson, E. B. / Powell, Richard W. / Ragsdale, W. A. | NTRS | 1991

    Real-time simulation model of the HL-20 lifting body

    Jackson, E. Bruce / Cruz, Christopher I. / Ragsdale, W. A. | NTRS | 1992

    An evaluation of automatic control system concepts for general aviation airplanes

    Stewart, E. C. / Ragsdale, W. A. / Wunschel, A. J. | NTRS | 1988

    Piloted simulator studies of the HL-20 Lifting Body

    Rivers, Robert A. / Jackson, E. B. / Ragsdale, W. A. | NTRS | 1991

    Atmospheric effects on the Space Shuttle approach and landing

    Ragsdale, W. A. / Osborne, A. R. / Seaman, C. K. | NTRS | 1974

    Investigation of the launch pad abort capabilities of the HL-20 lifting body

    JACKSON, E. / RIVERS, ROBERT / CHOWDHRY, RAJIV et al. | AIAA | 1993

    Initial Investigation of Reaction Control System Design on Spacecraft Handling Qualities for Earth Orbit Docking

    Bailey, Randall E. / Jackson, E. Bruce / Goodrich, Kenneth H. et al. | NTRS | 2008

    Launch pad abort of the HL-20 lifting body

    Jackson, E. B. / Rivers, Robert A. / Chowdhry, Rajiv S. et al. | AIAA | 1994