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介绍并评价了固体火箭发动机初步设计中沿用的八种优化准则。分析了固体弹道式导弹和有翼战术导弹中影响推进系统目标的主要特征参量。概要说明了组织固体火箭发动机初步设计优化过程的要点。
The eight optimization criteria used in the preliminary design of solid rocket motors are introduced and evaluated. The main characteristic parameters that affect the propulsion system of solid ballistic missiles and winged tactical missiles are analyzed. This section outlines the key points in the initial design optimization of solid rocket motors.