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person:(Jackson, C.)

    Closed-loop simulation of inertial platform accelerometer inputs

    JACKSON, C. T. / SCHLOETZER, F. F. | AIAA | 1965

    An operational electrothermal propulsion system for spacecraft reaction control

    HAGELBERG, C. / JACKSON, F. / JORTNER, D. | AIAA | 1966

    One-mlb Colloid Thruster System Development

    SIDNEY ZAFRAN / JOHN C. BEYNON / PHILIP W. KIDD et al. | AIAA | 1973

    A ram-air-spoiler roll stabilization device for forward control cruciform missiles

    BLAIR, JR., A. / SAWYER, W. / JACKSON, JR., C. | AIAA | 1978

    Integrated avionics for future general aviation aircraft

    DENERY, D. / JACKSON, JR., C. / CALLAS, G. et al. | AIAA | 1978

    Ram-Air-Spoiler Roll Stabilization Device for Forward-Control Cruciform Missiles

    A.B. Blair Wallace C. Sawyer / Charlie M. Jackson | AIAA | 1979

    A pioneer-class Mars aeronomy mission

    JACKSON, R. / MUNOZ, R. / LEIDICH, C. et al. | AIAA | 1983

    Design study of a slant-nose-cylinder aeroassisted orbital transfer vehicle

    BLOSSER, M. / POWELL, R. / JACKSON, L. et al. | AIAA | 1985

    Structural concepts for future space transportation system orbiters

    TAYLOR, A. H. / JACKSON, L. R. / DAVIS, R. C. et al. | AIAA | 1985

    Mechanisms for thermally enhanced target coupling by repetitively pulsed lasers

    JUMPER, E. J. / COUICK, J. R. / MCKEE, L. L. et al. | AIAA | 1987

    Integrated Cryogenic Satellite Communications Cross-link Receiver Experiment

    Romanofsky, R. / Bhasin, K. / Downey, A. et al. | AIAA | 1996