OPTIMIZATION DESIGN OF THE SOLID ROCKET MOTOR

Apr. 1990

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Article Navigation > Journal of Aerospace Power > 1990 > 5(2): 176-178,191

Fang Guoyao, Guo Zhiyong. OPTIMIZATION DESIGN OF THE SOLID ROCKET MOTOR[J]. Journal of Aerospace Power, 1990, 5(2): 176-178,191.

Citation:

Fang Guoyao, Guo Zhiyong. OPTIMIZATION DESIGN OF THE SOLID ROCKET MOTOR[J]. Journal of Aerospace Power, 1990, 5(2): 176-178,191.

Fang Guoyao, Guo Zhiyong. OPTIMIZATION DESIGN OF THE SOLID ROCKET MOTOR[J]. Journal of Aerospace Power, 1990, 5(2): 176-178,191.

Citation:

Fang Guoyao, Guo Zhiyong. OPTIMIZATION DESIGN OF THE SOLID ROCKET MOTOR[J]. Journal of Aerospace Power, 1990, 5(2): 176-178,191.

Abstract

This paper presents the optimization design of a two stage solid rocket motor for a air to air missile.There are eight variables in the optimization process.The mathematical model of the solid rocket motor is formulated.A variable simplex method has been used.Finally,the optimum results for a real solid rocket motor are obtained.