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作 者:周成[1] 袁渊[2,3] 于存贵 王燕[1] 甘霖 Zhou Cheng;Yuan Yuan;Yu Cungui;Wang Yan;Gan Lin(School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China;Shanghai Institute of Satellite Engineering,Shanghai 201109,China;Shanghai Key Laboratory of Deep Space Exploration Technology,Shanghai 201109,China)
机构地区:[1]南京理工大学机械工程学院,江苏南京210094 [2]上海卫星工程研究所,上海201109 [3]上海市深空探测技术重点实验室,上海201109
出 处:《南京理工大学学报》2020年第3期354-358,378,共6页Journal of Nanjing University of Science and Technology
摘 要:通过地面试验模拟了某深空撞击器侵彻天体过程,并得到侵彻过程有关数据。试验采用125 mm口径滑膛炮作为撞击器发射平台,浇筑C20圆柱形素混凝土靶标,发射撞击器撞击靶标,得到了撞击器在不同速度下的侵彻深度、受损情况及过载数据。试验结果表明:以125 mm口径滑膛炮作为发射平台合理有效;撞击器在着靶速度662 m/s以上时能达到1 m以上侵彻深度,同时满足强度要求。The penetration process of a deep space impactor into celestial bodies is simulated through ground tests,and the relevant data of the penetration process are obtained.A 125 mm sliding gun is used as the launching platform of the impactor,a C20 cylindrical plain concrete target is poured,and the impactor is launched against the target.The penetration depth,damage and overload data of the impactor at different velocities are obtained.The test results show that it is reasonable and effective to use the 125 mm sliding gun as launching platform.The penetration depth of the impactor reaches more than 1 m when the impact velocity is 662 m/s,and meets the strength requirements.
分 类 号:V553.2[航空宇航科学与技术—人机与环境工程]
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