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A novel non-separation opening scheme of front cover for rocket launch canister 被引量:1
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作者 Ce Zhang Xin Zhao +2 位作者 Zonglai Mo Zhuoyu Guo Jun Li 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第6期905-911,共7页
In view of that existing opening technologies of front cover for rocket launch canister have disadvantages such as causing damage on the ground equipment,not being reused and easily broken.A novel reusable non-separat... In view of that existing opening technologies of front cover for rocket launch canister have disadvantages such as causing damage on the ground equipment,not being reused and easily broken.A novel reusable non-separation spring-driven opening scheme is proposed to achieve rapid and reliable opening of the front cover.The mathematical model of the opening process of the front cover is established by the rigid body dynamics theory.To establish a response surface model to optimize the opening scheme,three main influencing factors of the opening process are obtained through the designed experiments,including the pre-compression,the stiffness of the thrust spring,and the thrust spring force arm length.In addition,the prescribed kinematic law was taken as constraint,and the smaller thrust spring preliminary pressure and angular velocity was taken as optimization expectations.The results show that the opening scheme meets the design requirements on opening process well.It also shows that the optimized scheme can reduce the kinetic energy of the front cover,and the impact on the canister effectively,achieving a reliable and rapid opening of the front cover. 展开更多
关键词 canister covers Spring-driven Non-separation Optimized opening scheme Rocket launch canisters Launch safety
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