1. Aarnio, A.J., Hinkey, J.B., and Bussing, T.R.A., 1996. "Multiple Cycle Detonation Experiments During the Development of a Pulse Detonation Engine,"AIAA 96-3263. Bratkovich, T.E. and Bussing, T.R.A., 1995. "A Pulse Detonation Engine Performance Model," AIAA 95-3155. Bussing, T.R.A., 1995. "A Rotary Valve Multiple Pulse Detonation Engine,"AIAA 95-2577. Bussing, T.R.A. and Pappas, G., 1994. "An Introduction to Pulse Detonation Engines," AIAA 94-0263. Eidelman, S., Grossman, W., Gunners, N.E., and Lottati, I., 1994. "Progress in Pulsed Detonation Engine Development,"AIAA94-2721. Eidelman, S., 1997. "PulseDetonation Engine: A Status Review and Technology Development Roadmap,"AIAA 97-2740. Helman, D., Shreeve, R.P., and Eidelman,S., 1986. "Detonation PulseEngine,"AIAA 86-1683. Hinkey, J.B., Williams, J.T., Henderson, S.E., and Bussing, T.R.A., 1997. "Rotary-Valved, Multiplecycle Pulse Detonation Engine Experimental Demonstration,"AIAA 97-2746. Hinkey, J.B., Bussing, T.R.A., and Kaye, L., 1995. "Shock Tube Experiments for the Development of a Hydrogen-Fueled Pulse Detonation Engine," AIAA 95-2578. Hoffman, H., 1941. "Reaction Propulsion by Intermittent Detonative Combustion," Ministry of Supply, Volkenrode translation. Krzycki, L. J., 1962. "Performance Characteristics of an Intermittent-Detonation Device,"NAVWEPS Report 7655. Nicholls, J.A., Wilkinson, H.R., and Morrison, R. B., 1957. "Intermittent Detonation as a Thrust-Producing Mechanism," Jet Propulsion, 27, pp.534-541. Ting, J.M., Bussing, T.R.A., and Hinkey, J.B., 1995. "Experimental Characterization of the Detonation Properties of Hydrocarbon Fuelsforthe Development of a Pulse Detonation Engine", AIAA 95-3154. Sterling, J., Ghorbanian, K., and Sobota, T., 1997. "Enhanced Combustion Pulsejet Engines for Mach 0 to 3Applications,"AIAA 96-2687.
2. Eidelman, 1997). Figure 8: Photograph of the flight-scale RVMPDE apparatus operating in a detonative mode at
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