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    Importance and Challenges of Hybrid Rocket Propulsion Beyond Year 2000

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

    Hot fragment conductive ignition of nitramine-based propellants

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

    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

    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

    Thrust and ignition transients of the Space Shuttle solid rocket motor

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