Reliability Analysis on Solid Rocked Engine Vessel

Liu Chong, S. Torii, C. Yuting
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Abstract

: The solid rocket engine is widely used in missile. In order to expand the scope of attack, both iincrease specific impulse and decrease weight are become the research goal. In this paper, we take the vessel of solid rocket engine as research object, simulate the pressure of hydrostatic test, establish the finite element model of solid rocket engine vessel, solve the stress for any element in solid rocket engine vessel and find the maximum stress point by ANASYS, and then we solve reliability by the method of random analysis. According to this reliability, change the pressure which load on the inside of solid rocket engine vessel while insure reliability higher than the criticality. In this analysis, we can increase the pressure which loads the solid rocket engine vessel and we achieve the sensitivity of all parameters.
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固体振动发动机容器可靠性分析
固体火箭发动机广泛应用于导弹。为了扩大攻击范围,增加比冲和减轻重量成为研究目标。本文以固体火箭发动机容器为研究对象,模拟静水试验压力,建立固体火箭发动机容器的有限元模型,利用ansys求解固体火箭发动机容器内任意元件的应力并求出最大应力点,然后用随机分析法求解可靠性。根据这一可靠性,在保证可靠性高于临界水平的前提下,改变固体火箭发动机容器内部的压力载荷。在此分析中,我们可以增加固体火箭发动机容器的载荷压力,并实现所有参数的灵敏度。
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