A novel non-separation opening scheme of front cover for rocket launch canister
Autor: | Xin Zhao, Zhuo-Yu Guo, Zong-Lai Mo, Ce Zhang, Jun Li |
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Rok vydání: | 2019 |
Předmět: |
0209 industrial biotechnology
Computer science Mechanical Engineering Separation (aeronautics) Metals and Alloys Computational Mechanics Process (computing) Mechanical engineering Thrust Angular velocity 02 engineering and technology Kinematics Spring (mathematics) Rigid body dynamics 01 natural sciences 010305 fluids & plasmas Rocket launch Military Science 020901 industrial engineering & automation 0103 physical sciences Ceramics and Composites |
Zdroj: | Defence Technology, Vol 15, Iss 6, Pp 905-911 (2019) |
ISSN: | 2214-9147 |
DOI: | 10.1016/j.dt.2019.01.005 |
Popis: | 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. Keywords: Canister covers, Spring-driven, Non-separation, Optimized opening scheme, Rocket launch canisters, Launch safety |
Databáze: | OpenAIRE |
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