41–60 von 69 Ergebnissen
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    Titan Turtle: NIAC Phase II Design for a Submersible Vehicle for Titan Exploration

    Steven R. Oleson / Jason W. Hartwig / Geoffrey A. Landis et al. | NTRS

    Apparatus for making a metal slurry product Patent

    Prok, G. M. / Walsh, T. J. / Witzke, W. R. | NTRS | 1960

    New design and operating techniques for improved terminal area compatibility

    Reeder, J. P. / Taylor, R. T. / Walsh, T. M. | NTRS | 1974

    Characterization evaluation of the attitude control propulsion system Interim report

    Hoyle, R. S. / Thompson, P. F. / Walsh, T. J. | NTRS | 1970

    Synthetic Flight Training System (Sfts) Concept Formulation Report

    R. E. Flexman / W. P. Jameson / J. M. Walsh | NTIS | 1968

    F/A-18 Performance Benefits Measured During the Autonomous Formation Flight Project

    Vachon, M. Jake / Ray, Ronald J. / Walsh, Kevin R. et al. | NTRS | 2003

    Hybrid Propulsion for Air Force Applications Study

    K. E. Mahaffy / G. C. Harting / R. Bates et al. | NTIS | 1996

    Flight evaluation results for a digital electronic engine control in an F-15 airplane

    Burcham, F. W., Jr. / Myers, L. P. / Walsh, K. R. | NTRS | 1983

    Propulsion Flight Research at NASA Dryden From 1967 to 1997

    Burcham, Frank W., Jr. / Ray, Ronald J. / Conners, Timothy R. et al. | NTRS | 1997

    Development of a Standardized U.S. Flag Dry-Bulk Carrier. Appendix E. Design Selection

    A. Baki / R. T. Walsh / R. H. M. Levite et al. | NTIS | 1979

    F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack

    Yuhas, Andrew J. / Steenken, William G. / Williams, John G. et al. | NTRS | 1997

    Inlet Distortion for an F/A-18A Aircraft During Steady Aerodynamic Conditions up to 60 deg Angle of Attack

    Walsh, Kevin R. / Yuhas, Andrew J. / Williams, John G. et al. | NTRS | 1997

    F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack

    A. J. Yuhas / W. G. Steenken / J. G. Williams et al. | NTIS | 1997