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《Missiles and Space Vehicles》 2017-03
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Research on Calculation and Test of Initiating Explosive Circuit Operating Current for Launch Vehicle

Zhu Yuan;Beijing Aerospace Automatic Control Institute;  
The calculation and verification of the initiating explosive circuit operating current is an important constituent part of launch vehicle control system. Firstly, the paper puts forward the composition of the initiating explosive circuit. Then, three different calculation methods for the initiating explosive circuit operating current based on the equivalent model are provided. Finally, three different test methods are provided, such as little current test, the simulated explosive initiator test, the explosive initiator test. The results calculated with the equivalent model agree with those from test. The above methods can serve as a reference for engineering applications.
【CateGory Index】: V475.1
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【Citations】
Chinese Journal Full-text Database 5 Hits
1 Du Zhi,Zhen Guoyong,Dong Xiaona(National Key Laboratory for Electronic Measurement Technology,North University of China,Taiyuan 030051,China);Safety and Reliability Design of Ignition Controller[J];计算机测量与控制;2013-01
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【Co-citations】
Chinese Journal Full-text Database 9 Hits
1 Zhu Yuan;Beijing Aerospace Automatic Control Institute;;Research on Calculation and Test of Initiating Explosive Circuit Operating Current for Launch Vehicle[J];导弹与航天运载技术;2017-03
2 ZHOU Heng-bao;XIN Gao-bo;DING Xiu-feng;QIN Ying-ming;WANG Meng;Aerospace System Engineering Shanghai;;Design of Sequential Control System for New Generation Launch Vehicle[J];上海航天;2016-S1
3 HU Haifeng;Beijing Aerospace Automatic Control Institute;;Reliability Analysis on Complex and Fault Tolerant GNC System of Launch Vehicle[J];航天控制;2014-05
4 Zhou Tao;Ren Yongfeng;Li Huijing;Wang Shuqin;Ministerial Key Laboratory for Instrument Science and Dynamic Test,Key Laboratory for Electronic Measurement Technology,North University of China;;Reliability Design and Research of Launching Control Device on Catapulting[J];计算机测量与控制;2014-07
5 HE Zhi-hang;NIE Hong;YANG Chun;ZHANG Ming;WANG Xu-gang;College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics;China Academy of Launch Vehicle Technology;;Design and Dynamics Analysis of Separation Guiding Mechanism's Parameters of Payload-Rocket[J];宇航学报;2014-06
6 HU Haifeng;ZHAI Shaolei;SUN Haifeng;Beijing Aerospace Automatic Control Institute;;Study on Reliability Model of Launch Vehicle GNC System Based on Total Probability Formula[J];航天控制;2014-03
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9 Du Zhi,Zhen Guoyong,Dong Xiaona(National Key Laboratory for Electronic Measurement Technology,North University of China,Taiyuan 030051,China);Safety and Reliability Design of Ignition Controller[J];计算机测量与控制;2013-01
【Secondary Citations】
Chinese Journal Full-text Database 4 Hits
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