Research on Design Simulation and Experiment of Separation Mechanism for Micro-Nano Satellites
文献类型：期刊论文
| 作者 | X. Y. Zhao; C. J. Zhao; J. L. Li; Y. L. Guan; S. B. Chen and L. Zhang |
| 刊名 | Applied Sciences-Basel
 |
| 出版日期 | 2022 |
| 卷号 | 12期号:12页码:21 |
| DOI | 10.3390/app12125997 |
| 英文摘要 | The separation mechanism is a critical device that transports and releases satellites during launch and on-orbit. However, as satellites become smaller and more compact, the traditional belt-locking device or pyrotechnic release and separation device cannot meet the micro-nano satellite's separation requirements. A novel separation mechanism kinematic system was designed, analyzed, and experimentally verified to achieve non-interference and non-pyrotechnic separation of the satellites from the launch vehicle while maintaining the initial separation attitude. First, an overall structural strategy for the kinematics system was proposed based on the MF (product code of the satellite) satellite's structural properties. The structural characteristics of the separation mechanism were also confirmed by the principle of energy conservation. Then, a finite element model and a dynamic model of the kinematic coupling system between the MF satellite and the separation mechanism during launch and deployment were constructed, along with an analysis of the mechanical characteristics and a kinematic simulation. Finally, the mechanical characteristics and dependability of the separation mechanism were verified using a ground vibration test and a separation test. The prototype test results demonstrate that the separation process is essentially identical to the numerical simulation results and that the MF satellite can be deployed successfully without interference, with the MF satellite's initial separation attitude fully satisfying the designed technical indexes. |
| URL标识 | 查看原文 |
| 语种 | 英语 |
| 源URL | [http://ir.ciomp.ac.cn/handle/181722/67313]  |
| 专题 | 中国科学院长春光学精密机械与物理研究所 |
| 推荐引用方式 GB/T 7714 | X. Y. Zhao,C. J. Zhao,J. L. Li,et al. Research on Design Simulation and Experiment of Separation Mechanism for Micro-Nano Satellites[J]. Applied Sciences-Basel,2022,12(12):21. |
| APA | X. Y. Zhao,C. J. Zhao,J. L. Li,Y. L. Guan,&S. B. Chen and L. Zhang.(2022).Research on Design Simulation and Experiment of Separation Mechanism for Micro-Nano Satellites.Applied Sciences-Basel,12(12),21. |
| MLA | X. Y. Zhao,et al."Research on Design Simulation and Experiment of Separation Mechanism for Micro-Nano Satellites".Applied Sciences-Basel 12.12(2022):21. |
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