41–60 von 71 Ergebnissen
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    Heat pipe avionic thermal control

    TOKEN, K. / GARNER, E. / COOK, R. et al. | AIAA | 1980

    Viscous shock-layer analysis of hypersonic flows over long slender bodies

    GUPTA, R. / LEE, K. / MOSS, J. et al. | AIAA | 1987

    Design and performance evaluation of a two-position variable geometry turbofan combustor

    SANBORN, J. / SCHEIHING, P. / COLEMAN, E. et al. | AIAA | 1984

    Return to the Flight of M-V Rocket

    Onoda, J. / Sato, E. / Inatani, Y. et al. | AIAA | 2004

    Orbital parameters for objects observed by the Mic...

    Abercromby, K. J. / Seitzer, P. / Parr-Thumm, T. L. et al. | AIAA | 2005

    Laser and radiofrequency production of seeded air plasmas

    Scharer, J. / Ding, G. / Gui, H. et al. | AIAA | 1999

    Testing of an advanced liquid hydrogen turbopump

    Grabowski, R. / Chapman, L. / Crease, G. et al. | AIAA | 2000

    Introducing the ESA DRAMA Tool

    Martin, C. E. / Cheese, J. E. / Sánchez-Ortiz, N. et al. | AIAA | 2004

    Numerical simulations of flow modification of supersonic rectangular jets

    Kolbe, R / Kailasanath, K / Young, T et al. | AIAA | 1995

    Oblique detonation wave studies in the Caltech T-5 Shock Tunnel Facility

    Sterling, J. / Cummings, E. / Ghorbanian, K. et al. | AIAA | 1998

    The development of a Planetary Aerobot Testbed

    Nock, K. / Anderson, J. / Bachelder, A. et al. | AIAA | 1997

    Smart fuels - 'Controlled' chemically reacting

    Maurice, L. / Corporan, E. / Minus, D. et al. | AIAA | 1999

    Prediction of unstart phenomena in hypersonic aircraft

    Cox, C / Lewis, C / Pap, R et al. | AIAA | 1995

    V/STOL demonstrator vehicle for ejector thrust augmentation technology

    BYRNES, J. / MURPHY, R. / BALL, R. et al. | AIAA | 1974

    Best Practices for Reliable and Robust Spacecraft Structures

    Raju, I / Murthy, Pappu / Patel, N et al. | AIAA | 2007