41–60 von 998 Ergebnissen
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    Trajectory Optimization for a Generic Hypersonic Vehicle

    Keshmiri, Shahriar / Colgren, Richard / Mirmirani, Maj | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Trajectory Optimization and Guidance of an Air Breathing Hypersonic Vehicle

    Brinda, V / Dasgupta, S / Lal, Madan | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Trajectory and Aeroheating Environment Development and Sensitivity Analysis for Capsule-Shaped Vehicles

    Robinson, Jeffrey / Wurster, Kathryn | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Trailing edge cavity afterbodies for linear plug nozzle engines

    Wisse, Menko / Bannink, Willem | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Tradeoffs for Hypersonic Delivery Systems

    Porter, John / Shaw, William | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Towards an Integrated Design Environment for Hypersonic Vehicle Design and Synthesis

    Zweber, Jeffrey / Kabis, Hanee / Follett, William et al. | AIAA | 2002
    Verlag: The American Institute of Aeronautics and Astronautics

    Towards a low risk airbreathing SSTO program - A continuous robust PREPHA based TSTO

    Serre, L. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Toward a Continuous Detonation Wave Rocket Engine Demonstrator

    Falempin, Francois / Daniau, Emeric / Getin, N. et al. | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Thrust Matching Requirements for the Conceptual Design of Hypersonic Waverider Vehicles

    Javaid, Kashif / Serghides, Varnavas | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Thrust and Drag of a Scramjet Model with Different Combustor Geometries

    Chang, Xinyu / Gu, Hongbin / Chen, Lihong | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Three-Dimensional Shock-Cylinder Interactions in Hypersonic Flow

    Bird, Graeme | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Three-dimensional DSMC simulation of hypersonic rarefied gas flow around a sharp flat plate

    Tsuboi, Nobuyuki / Yamaguchi, Hiroki / Matsumoto, Yoichiro | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    The X-43A Hyper-X Mach 7 Flight 2 Guidance, Navigation, and Control Overview and Flight Test Results

    Bahm, Catherine / Baumann, Ethan / Martin, John et al. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    The X-15 as an analog to expected experimental vehicle operations and costs

    Springer, Anthony / Abe, Takashi / Fujita, Kazuhisa et al. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    The University of Maryland Hypersonics Center - Status report

    Lewis, Mark / Pines, Darryll / Gupta, Ashwani | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    The Themis launch vehicle - The definitive demonstration prior to future European RLV

    Delattre, Nathalie / Clar, Philippe / Deneu, Francois et al. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    The Sustained Hypersonic Flight Experiment

    Cain, Terrence / Walton, Craig | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    The sub-orbital hopper - One of FESTIP's preferred concepts

    Spies, J. / Kuczera, H. | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    The SSTO combined propulsion system on a basis of LACE and DmSCRJ

    Smolyarov, V. / Dulepov, N. / Lanshin, A. et al. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    The Socrates Vehicle - ESTEC CDF Design

    Santovincenzo, Andrea / Innocenti, Luisa / van Pelt, Michel | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics