1–20 von 207 Ergebnissen
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    An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3

    Gloria, H. R. | NTRS | 1958
    Schlagwörter: WINGLESS VEHICLE , LONGITUDINAL STABILITY AND CONTROL , STATIC STABILITY

    Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01

    Foster, G. V. | NTRS | 1959
    Schlagwörter: LONGITUDINAL STABILITY AND CONTROL , HYPERSONIC VEHICLE , LATERAL STABILITY AND CONTROL

    Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01

    G. V. Foster | NTIS | 1959
    Schlagwörter: Hypersonic vehicle , Lateral stability and control , Longitudinal stability and control , Stability , Vehicle

    Full-Scale Wind-Tunnel Investigation of the Low-Speed Static Aerodynamic Characteristics of a Model of a Reentry Capsule

    W. I. Scallion | NTIS | 1959
    Schlagwörter: Reentry vehicle , Stability , Vehicle

    Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

    Foster, G. V. / Robinson, R. B. | NTRS | 1961
    Schlagwörter: STATIC STABILITY AND CONTROL , LONGITUDINAL STABILITY AND CONTROL , HYPERSONIC VEHICLE

    Interaction of structural vibrations. propellant sloshing and control for large space vehicles

    Bauer, H. F. | NTRS | 1961
    Schlagwörter: SPACE VEHICLE CONTROL , STABILITY AND CONTROL

    A WIND-TUNNEL INVESTIGATION aT SUBSONIC aND LOW SUPERSONIC SPEEDS oF a RE-ENTRY VEHICLE WITH RETRACTABLE WINGS

    Smith, W. G. | NTRS | 1961
    Schlagwörter: WIND TUNNEL STABILITY TEST , REENTRY VEHICLE

    THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

    Kenyon, G. C. / Sutton, F. B. | NTRS | 1961
    Schlagwörter: LONGITUDINAL STABILITY AND CONTROL , REENTRY VEHICLE

    Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-Movable Wing and Tail Surfaces

    G. V. Foster / R. B. Robinson | NTIS | 1961
    Schlagwörter: Hypersonic vehicle , Longitudinal stability and control , Static stability and control , Stability

    LAUNCH VEHICLE RECOVERY SYSTEM REQUIREMENTS

    Barraza, R. M. | NTRS | 1962
    Schlagwörter: LAUNCH VEHICLE , SPACECRAFT STABILITY

    INVESTIGATION OF THE LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 0.34 -SCALE FREE-FLYING MODEL OF A MODIFIED HALF-CONE REENTRY VEHICLE

    Hassell, J. L., Jr. / Ware, G. M. | NTRS | 1962
    Schlagwörter: REENTRY VEHICLE , STABILITY AND CONTROL

    Preliminary Investigation of Interference Effects of Multicoplanar Fins on a Two-Stage Rocket Launch Vehicle with Winged Spacecraft at Transonic Speeds

    P. K. Pierpont | NTIS | 1962
    Schlagwörter: Launch vehicle , Stability and control , Winged vehicle , Stability , Vehicle

    Dynamic stability of a uniform free-free beam under a gimbaled thrust of periodically varying magnitude

    Beale, T. R. | NTRS | 1963
    Schlagwörter: ROCKET VEHICLE , DYNAMIC STABILITY