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《Ordnance Industry Automation》 2009-02
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Simulation Analysis for Launch Dynamics of Multiple Launch Rocket System Based on ADMAS

CAO Guang-qun1,ZHANG Yan-hua2,LIU Shu-hua1(1.College of Weapon Facility & Technology,North University of China,Taiyuan 030051,China;2.Dept.of Information Gathering-Detecting & Authority Control,Hebei Yuandong Communication System Engineering Co.,Ltd.,Shijiazhuang 050081,China)  
Based on virtual prototype technology,the dynamic characteristics of the Multiple Launch Rocket mounting buffer device in fire period was discussed.We established the physical model that is suitable for dynamic simulation according to rocket gun system’s geometric model;developed simulation prototype system based on ADAMS software platform and program composition of launching simulation.Shocked vibration torque of pitch axis and azimuth axis,as well as rocket gun system’s mechanical characteristics of base,which provide reference data for developing and testing multiple launch rocket system,effectively reduced development period of the system,and saved the development funds.
【CateGory Index】: TJ393
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【Citations】
Chinese Journal Full-text Database 2 Hits
1 Zhang Shengsan(Beijing Institute of Aerospace Launch Technology, Beijing, 100076)Guo Weidong(Beijing University of Aeronautics and Astronautics, Beijing, 100083);Outlet Attitude Simulation of Multitube Artillery Rocket[J];Missiles and Space Vehicles;2003-02
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【Co-references】
Chinese Journal Full-text Database 7 Hits
1 WANG Shang-bin1,SUN Yu1,ZHANG Qing-fei2(1.School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China;2.Yangzhou Metal Forming Machine Group Co.,Ltd.,Yangzhou 225127,China);ANSYS analysis of 5000kN press frame[J];Forging & Stamping Technology;2009-02
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【Secondary Citations】
Chinese Journal Full-text Database 2 Hits
1 Zhang Shengsan Wang Xinqian(Beijing Institute of Special Engineering Machinery, Beijing,100076)Guo Weidong(Beijing University of Aeronautics and Astronautics,Beijing,100083)Wang Qian(Beijing Office of American MDI Corporation,Beijing,100031)$$$$;The Simulation on Dynamics of Multi-tube Launcher[J];Missiles and Space Vehicles;2001-06
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