21–40 von 160 Ergebnissen
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    THERMAL PROTECTION SYSTEMS: HERITAGE - DEVELOPMENT STATUS - PERSPECTIVES

    Pichon, T. / Barreteau, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    THERMAL PROTECTION AND HYDROGEN PRODUCTION ON BOARD OF THE HYPERSONIC VEHICLE

    Kuranov, A.L. / Korabelnikov, A.V. / Mikhailov, A.M. et al. | British Library Conference Proceedings | 2012

    THE AEROTHERMAL, THERMAL AND STRUCTURAL DESIGN PROCESS AND CRITERIA FOR THE HIFIRE-4 FLIGHT TEST VEHICLE

    Lau, K.Y. / Woo, Y. / Tran, J. et al. | British Library Conference Proceedings | 2012

    TECHNOLOGY STATUS OF FUEL COOLED CERAMIC MATRIX COMPOSITES FOR DUAL-MODE RAMJET (DMR) AND LIQUID ROCKET ENGINE (LRE) APPLICATIONS

    Beyer, S. / Schmidt-Wimmer, S. / Quering, K. et al. | British Library Conference Proceedings | 2012

    TECHNICAL MATURATION OF THE SPACELINER CONCEPT

    Sippel, M. / Schwanekamp, T. / Bauer, C. et al. | British Library Conference Proceedings | 2012

    SUPERSONIC COMBUSTION PROCESSES IN A PREMIXED 3D NON-UNIFORM-COMPRESSION SCRAMJET ENGINE

    Bricalli, M.G. / Boyce, R.R. / Brown, L. et al. | British Library Conference Proceedings | 2012

    STUDY ON AERODYNAMIC CHARACTERISTICS OF A HIGH ENTHALPY FLOW AROUND BLUNT-NOSED BODY

    Takahashi, M. / Sato, K. / Itoh, K. et al. | British Library Conference Proceedings | 2012

    STRUCTURAL DESIGN AND OPTIMISATION OF THE LAPCAT A2 MACH 5 VEHICLE BASED ON AERO-ELASTIC DEFORMATIONS

    Sharifzadeh, S. / Hendrick, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    STATIC STABILITY OF THE SCRAMSPACE I MACH 8 HYPERSONIC FLIGHT EXPERIMENT

    Brown, L.M. / Tirtey, S.C. / Van Staden, P.A. et al. | British Library Conference Proceedings | 2012

    STAGE SEPARATION FROM SHUTTLE CARRIER AIRCRAFT FOR SPACE ACCESS

    Mehta, U. / Bowles, J. / Pandya, S. et al. | British Library Conference Proceedings | 2012

    SINGLE PULSE LASER ENERGY DEPOSITION IN QUIESCENT AIR AND HYPERSONIC FLOWS

    Yang, L. / Erdem, E. / Zare-Behtash, H. et al. | British Library Conference Proceedings | 2012

    SIMULATION OF HIGH MACH NUMBER SCRAMJET FLOW CONDITIONS USING THE X2 EXPANSION TUBE

    Gildfinder, D.E. / Morgan, R.G. / McGilvray, M. et al. | British Library Conference Proceedings | 2012

    SHOCK TUNNEL AND NUMERICAL STUDIES OF A LARGE INLET-FUELLED INWARD TURNING AXISYMMETRIC SCRAMJET

    Boyce, R.R. / Schramm, J.M. / Oberg, D. et al. | British Library Conference Proceedings | 2012

    SHOCK TUBE TESTING OF THE TRANSPIRATION-COOLED HEAT SHIELD EXPERIMENT AKTIV

    Bohrk, H. / Wartemann, V. / Eggers, T. et al. | British Library Conference Proceedings | 2012

    SENSITIVITY OF FLIGHT DYNAMICS OF HYPERSONIC VEHICLES TO DESIGN PARAMETERS

    Dalle, D.J. / Torrez, S.M. / Driscoll, J.F. et al. | British Library Conference Proceedings | 2012

    RESEARCH ON THE COMBINED HEATING METHOD USING DUAL SUBSONIC GAS FLOW OF HIGH AND MIDDLE TEMPERATURE FOR THERMAL TEST OF TIP WEDGE STRUCTURE

    Dong, S. / Li, Z. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    RESEARCH ON HOT GAS JET IGNITION PROCESS OF SCRAMJET COMBUSTOR FUELED WITH KEROSENE

    Li, Q. / Wenxiong, X. / Lin, L. et al. | British Library Conference Proceedings | 2012