1–20 of 21 hits
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    Numerical study of solid-fuel combustion under supersonic crossflows

    JARYMOWYCZ, T. A. / YANG, V. / KUO, K. K. | AIAA | 1992

    Different modes of crack propagation in burning solid propellants

    KUO, K. K. / MORECI, J. / MANTZARAS, J. | AIAA | 1987

    Importance and Challenges of Hybrid Rocket Propulsion Beyond Year 2000

    Kuo, K. K. / Kenes Tel Aviv | British Library Conference Proceedings | 1997

    Thrust and ignition transients of the Space Shuttle solid rocket motor

    CAVENY, L. H. / KUO, K. K. / SHACKELFORD, B. W. | AIAA | 1980

    Hot fragment conductive ignition of nitramine-based propellants

    Huang, T. H. / Thynell, S. T. / Kuo, K. K. | AIAA | 1995

    feet of Chamber Pressure & Propellant Composition on Erosion Rate of Graphite Rocket Nozzle (AIAA 2006-0363)

    Acharya, R. / Kuo, K. K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    Characteristics of Nitromethane for Propulsion Applications (AIAA 2006-0361)

    Boyer, E. / Kuo, K. K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    Combustion Behavior and Flame Structure of XM46 Liquid Propellant

    Chang, Y.-P. / Boyer, E. / Kuo, K. K. et al. | British Library Conference Proceedings | 2000

    Recession behavior of graphitic nozzles in simulated rocket motors

    KESWANI, S. T. / ANDIROGLU, E. / CAMPBELL, J. D. et al. | AIAA | 1985

    Thrust and ignition transients of the Space Shuttle solid rocket motor

    Caveny, L. H. / Kuo, K. K. / Shackelford, B. W. | NTRS | 1980

    A comprehensive model for AP-based composite propellant ignition

    KUMAR, M. / WILLS, J. E. / KULKARNI, A. K. et al. | AIAA | 1984