1–20 von 603 Ergebnissen
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    Vacuum-air missile boost system

    KUMAR, S. / MURRAY, J. J. / RAJAN, J. R. N. | AIAA | 1964

    On the Optimum Stabilization of a Satellite

    Kumar, K. S. P. | IEEE | 1965

    Stabilization of a Satellite via Specific Optimum Control

    Kumar, K. S. P. / Teng, Lincoln | IEEE | 1966

    Attitude Determination Via Nonlinear Filtering

    Kau, S. / P. Kumar, K. S. / Granley, Gerald B. | IEEE | 1969

    Comment on Rates of Change of Flutter Mach Number and Flutter Frequency

    KUMAR G. BHATIA AND CARL S. RUDISILL | AIAA | 1973

    Planetary systems and extraterrestrial life

    Kumar, Shiv S. | Online Contents | 1974

    Thermal Conductivity of Comets

    G. N. Kumar / M. S. Khader / R. I. Vachon | AIAA | 1975

    Inclination correction for geostationary orbits using ion thrusters

    KUMAR, S. P. / KUDVA, P. / GOEL, P. S. | AIAA | 1985

    Effect of shot peening on fatigue of a Ni-based superalloy

    Kumar, D. / Das, S. / Radhakrishnan, V.M. | Tema Archiv | 1987

    Spin rate variations of spin-stabilized apogee motors in thrust phase

    ADIMURTHY, V. / KUMAR, PRADEEP / LAKSHMINARAYANAN, S. | AIAA | 1988

    Frequency estimation techniques for high dynamic trajectories

    Vilnrotter, V.A. / Hinedi, S. / Kumar, R. | IEEE | 1989

    Transient energy transfer by conduction and radiation in nongray gases

    TIWARI, S. N. / SINGH, D. J. / KUMAR, A. | AIAA | 1989

    Effect of nose bluntness on flowfield over slender bodies in hypersonic flows

    SINGH, D. J. / TIWARI, S. N. / KUMAR, A. | AIAA | 1991