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确定微型固体火箭发动机燃烧时间的CAA与CAD技术
引用本文:李逢春 徐向东. 确定微型固体火箭发动机燃烧时间的CAA与CAD技术[J]. 固体火箭技术, 1993, 0(1): 16-19
作者姓名:李逢春 徐向东
作者单位:西北工业大学 西安710072(李逢春,鲍福廷,徐东来),四院四○一所 西安710000(徐向东),四院四○一所·西安 710000(潘永德)
基金项目:高科技863-409研究课题
摘    要:
应用计算机辅助分析(CAA)与计算机辅助绘图(CAD)方法,确定微型固体火箭发动机燃烧时间t_b。该方法自动化程度高、精度好,有可靠的理论依据。用它替代传统的没有任何理论根据的手工画角分线法,以提高小型固体火箭发动机内弹道数据处理的精度和速度是十分必要的。实践证明这是一种科学的可行的方法,值得推广。

关 键 词:火箭发动机 计算机 辅助分析

CAA and CAD Technique for Determining Burning Time of a Micro Solid Rocket Motor
Li Fengchun,Bao Futing,Xu Dong lai Northwestern Polytechnical University,Xi'an,Xu Xiang dong,Pan Yongde Institute No. of Research Academy No.,Xi'an. CAA and CAD Technique for Determining Burning Time of a Micro Solid Rocket Motor[J]. Journal of Solid Rocket Technology, 1993, 0(1): 16-19
Authors:Li Fengchun  Bao Futing  Xu Dong lai Northwestern Polytechnical University  Xi'an  Xu Xiang dong  Pan Yongde Institute No. of Research Academy No.  Xi'an
Affiliation:Li Fengchun,Bao Futing,Xu Dong lai Northwestern Polytechnical University,Xi'an,710072Xu Xiang dong,Pan Yongde Institute No.401 of Research Academy No.4,Xi'an,710000
Abstract:
The computer aided analysis(CAA)and computer aided drawing(CAD)tech- nique is applied to determine the burning time t_b of a micro solid rocket motor.The tech- nique on the basis of theory features a high automatic degree and a high accuracy.It is nec- essary for it to take the place of the classical angle bisector drawn by hand in order to in- crease the accuracy and speed of the internal ballistic data processing of the micro solid rocket motor.The practice has proven that it is a scientific and feasible technique and wor- thy to be spread.
Keywords:Solid rocket engine  Computer aided analysis  Burning time  Computert aided draughting  
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