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    Depressurization induced extinction of burning solid propellant.

    BRUNO, P. S. / GRAESSER, E. C. | AIAA | 1968

    The Orbiting Astronomical Observatory thermal test program

    CARUSO, JR., P. / DAN, JR., C. / MENGERS, D. et al. | AIAA | 1969

    QUERIES

    COSTE, J. H. / GLETE, JAN / YOUNG, FRANK L. et al. | Taylor & Francis Verlag | 1971

    Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

    F. R. DeJarnette / C. P. Ford / D. E. Young | AIAA | 1980

    Gain Optimization And Saturation Of The Xe III 109 Nm Auger Laser

    Macklin, J J. / Sher, M H. / B arty, C P. et al. | SPIE | 1988

    Using a full potential solver for propulsion system exhaust simulation

    MELVIN, ROBIN G. / JOHNSON, FORRESTER T. / YOUNG, DAVID P. et al. | AIAA | 1993

    Predictions of counterfire impact results obtained at 12 kilometers per second

    Young, Raymond P. / Smith, Mark E. | AIAA | 1996

    Successful Application of New Technologies to the Rosetta and Mars Express Simulations

    Martin, J. E. / Lowe, R. / Osborne, J. J. et al. | AIAA | 2002

    Venus stratospheric sounder: first in situ measurements in upper cloud region

    Kerzhanovich, Viktor V. / Crisp, Dave / Preston, R.A.Robert A. et al. | Elsevier | 2002

    DYNAMO: a Mars upper atmosphere package for investigating solar wind interaction and escape processes, and mapping Martian fields

    Chassefière, E. / Nagy, A. / Mandea, M. et al. | Elsevier | 2003

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