24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-6.3.4

CONCEPTUAL DESIGN FOR A SUAV PROPULSION SYSTEM SIZING

Y. Jun, Y. Jung, S. Yang
Korea Aerospace Research Institute, Korea

Keywords: Tipjet rotor, UAV, Propulsion, CRW (canard rotor wing)

In this paper, key design parameters were revealed by analyzing the characteristics of the engine and the tipjet rotor system regarding the various configurations of the internal duct system. The direction for the next design step was shown by the results of the parametric study and the sensitivity analysis.

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