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| Launch Stability Analysis of a Missile Electromagnetic Ejection Device |
| KONG Chao, WANG Jun, CHEN Jianping, SHA Zhaoming |
1. Shanghai ElectroMechanical Engineering Institute, Shanghai 201109, China;
2. School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu，China |
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Abstract In order to accurately acquire the motion characteristics of the launch process of a vehicle borne missile electromagnetic ejection device, a multibody dynamics model is established by using ADAMS, and launch stability of the ejection device under the effect of recoil force and braking counterforce is analyzed. The results show that: in the process of missile firing, the rear part of the electromagnetic ejection device has a certain upward and backward movements, but there are within the acceptable range. The electromagnetic ejection device has good launch stability and its technology application to a missile firing is feasible.
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Received: 10 October 2018
Published: 08 January 2020
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| [1] |
JIA Mizhi, XU Liming, LIN Nan, NAN Bohua, WANG Kun, CAI Deng’an, ZHOU Guangming. Structural Design and Mechanical Properties of Fissile Cover with Rebound and Reset Functions[J]. Air & Space Defense, 2022, 5(2): 8-16. |
| [2] |
AN Qingsheng, SUN Lidong, WU Qiusheng. Design of Carbon Fiber Reinforced Composite Launch Tube[J]. Air & Space Defense, 2021, 4(2): 13-. |
| [3] |
LIU Weipeng, YUAN Jiebo, QIN Feng, WU Zhen, ZHAO Wenlong. Study on Obtainment of High Accuracy Initial Attitude for Vertical Launching of Ground-to-air Missile[J]. Air & Space Defense, 2018, 1(4): 24-28. |
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2019, Vol. 2 
