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潜射导弹燃气蒸汽式发射装置的内弹道建模
引用本文:肖虎斌.潜射导弹燃气蒸汽式发射装置的内弹道建模[J].舰船科学技术,2010,32(2):36-39.
作者姓名:肖虎斌
作者单位:中国船舶重工集团公司第七一三研究所,河南,郑州,450015
摘    要:发射过程中的内弹道建模是潜射导弹变深度发射的关键技术之一。按冷却水状态将燃气—蒸汽式发射装置发射过程分为4个阶段,本文主要针对各阶段的内弹道进行理论分析和建模,得出了整个发射过程中发射筒内的内弹道模型。将该内弹道模型应用于某实例,计算结果和实验结果吻合较好,这表明该内弹道模型具有一定的准确性和实用性,一定程度上可以预示发射筒内工质气体的状态参数及导弹运行参数。

关 键 词:潜射导弹  燃气—蒸汽式  内弹道  建模

Interior ballistics modeling of submarine-based missile launching unit
XIAO Hu-bin.Interior ballistics modeling of submarine-based missile launching unit[J].Ship Science and Technology,2010,32(2):36-39.
Authors:XIAO Hu-bin
Institution:The 713 Research Institute of CSIC;Zhengzhou 450015;China
Abstract:Interior ballistics predication is a key problem in gas-steam variable depth launching dynamics system.According to the phase change of cooling water,the whole process was divided into four stages,and mathematical models were presented individually,resulting a fully formulated mathematical model.Numerical predication was carried,and results matched well with the experimental data,which says the usefulness and accuracy of the model were validated.
Keywords:submarine-based missile launcher  gas-steam launch power unit  interior ballistics  
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