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燃气蒸汽式发射系统内弹道若干问题研究
引用本文:赵世平,鲍福廷.燃气蒸汽式发射系统内弹道若干问题研究[J].固体火箭技术,2003,26(3):7-10.
作者姓名:赵世平  鲍福廷
作者单位:西北工业大学航天工程学院,西安,710072
摘    要:通过对燃气蒸汽式发射动力系统的研究,总结出影响内弹道计算精度的若干因素,并就其中几个影响较大的问题进行了详细的分析,开发研制出了一套用于预估内弹道性能的系统化程序。通过实验数据的比较,验证了适用于内弹道计算的数学物理模型,为燃气蒸汽式发射系统设计提供参考依据。

关 键 词:燃气蒸汽式发射系统  内弹道  计算精度  导弹  运动规律  发射筒
文章编号:1006-2793(2003)03-0007-04

Analysis of several coefficients of interior ballistic evaluation for gas and steam launching system
ZHAO Shi-ping,BAO Fu-ting // College of Astronautics,Northwestern Polytechnical University,Xi'an ,China..Analysis of several coefficients of interior ballistic evaluation for gas and steam launching system[J].Journal of Solid Rocket Technology,2003,26(3):7-10.
Authors:ZHAO Shi-ping  BAO Fu-ting // College of Astronautics  Northwestern Polytechnical University  Xi'an  China
Institution:ZHAO Shi-ping,BAO Fu-ting // College of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China.
Abstract:Some important factors that have great effect on the interior ballistic evaluation for gas and steam launching devices are discussed and analyzed. A set of computer program is developed to predict the interior ballistic performance inside the launching tube, and the comparison with the test data is made to demonstrate the applicability of different mathematical and physical models of the system. The results can provide a reference for gas and steam launching system design.
Keywords:missile launcher  gas and steam launching device  in- terior ballistic calculation  
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