| Citation: | LI Baoxing, MENG Haolong, XING Pengtao, et al. Numerical simulation and experimental study on lateral gasbag separation of submunition missile[J]. Journal of Aerospace Power, 2023, 38(8):2024-2033 doi: 10.13224/j.cnki.jasp.20230053 |
In order to study the lateral gasbag separation characteristics of the submunition missile, the low burning temperature and high burning rate solid propellant was used as energy source, a mathematical model of gasbag separation was established and solved by fourth-order Runge-Kutta method. The variation laws of separation parameters such as gas generator interior ballistics, gasbag expansion and bullet simulated load separation motion were obtained. A simulation experimental system for lateral gasbag separation of submunition missile was set up for separation test verification simultaneously. The calculation results indicate that during the separation process, the pressure in the gasbag presents a variation trend that it increases first, and then decreases slowly, and then increases slowly. The acceleration of the bullet simulated load increases first and then decreases, with the maximum acceleration peak value of 15.1
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