Research Articles

Structural design and mechanical analysis of C/C grids for ion thruster

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  • 1. Shanghai Institute of Applied Mathematics and Mechanics,Shanghai University, Shanghai 200072, China
    2. College of Sciences, Shanghai University, Shanghai 200444, China
    3. Research Center of Composite Materials, Shanghai University, Shanghai 200072, China

Received date: 2017-05-08

  Online published: 2019-05-05

Abstract

To design C/C grids for the ion thruster and estimate lateral stiffness of the C/C grids, the mechanical behavior of C/C composite grids is studied based on the geometry of molybdenum grids. Finite element models of acceleration and screen grids are established using ABAQUS. By introducing a periodic boundary condition, a homogeneous model is established to analyze the stress distribution and mechanical properties of the representative volume element. The effect of mechanical properties of the composite components on global lateral stiffness of the grids is then discussed, and compared with molybdenum grids. The results show that global lateral stiffness of C/C grids is a function of tensile modulus of the carbon fiber and the modulus of matrix. Higher tensile modulus of carbon fiber can be selected to improve lateral stiffness of C/C grids.

Cite this article

CHEN Yue, LI Kai, PENG Yuqing, LI Aijun, ZHANG Dongsheng . Structural design and mechanical analysis of C/C grids for ion thruster[J]. Journal of Shanghai University, 2019 , 25(2) : 235 -244 . DOI: 10.12066/j.issn.1007-2861.1922

References

[1] 郑茂繁, 江豪成, 张天平 , 等. 离子推进器C/C复合材料栅极研究[J]. 航天器环境工程, 2010,27(6):756-759.
[2] 吴建军, 张传胜 . 离子发动机关键技术分析[J]. 国防科技大学学报, 2003,25(1):7-11.
[3] 李娟, 顾佐, 江豪成 , 等. 离子火箭发动机补偿栅极设计[J]. 真空与低温, 2005,11(1):29-33.
[4] 郭德洲, 顾左, 郑茂繁 , 等. 离子推力器碳基材料栅极研究进展[J]. 真空与低温, 2016,22(3):125-131.
[5] Mueller J, Brophy J R, Brown D K, et al. Performance characteristics of 15 cm carboncarbon composite grids [C]// 30th Joint Propulsion Conference and Exhibit. 1994.
[6] Mueller J, Brophy J R, Brown D K. Endurance testing and fabrication of advanced 15 cm and 30 cm carbon-carbon composite grids [C]// 31st Joint Propulsion Conference and Exhibit. 1995.
[7] Mueller J, Brophy J R, Brown D K. Design, fabrication, and testing of 30 cm dia dished carbon-carbon ion engine grids [C]// 32nd Joint Propulsion Conference and Exhibit. 1996.
[8] Rohit S, Daniel A, George C, et al. Status of NASA’s evolutionary xenon thruster (NEXT) long-duration test as of 50,000 h and 900 kg throughput [C]// 33rd International Electric Propulsion Conference and Exhibit. 2013.
[9] 成来飞, 张立同, 梅辉 , 等. 化学气相渗透工艺制备陶瓷基复合材料[J]. 上海大学学报(自然科学版), 2014,20(1):15-32.
[10] 冯志海, 樊桢, 孔清 , 等. 高导热碳/碳复合材料的制备[J]. 上海大学学报(自然科学版), 2014,20(1):51-58.
[11] 房金铭, 许正辉, 张中伟 , 等. 碳布缝合预制体孔隙与热解碳沉积时变相依的多尺度研究[J].宇航材料工艺, 2015(5):36-39.
[12] 严雪, 许希武, 张超 . 二维三轴编织复合材料的弹性性能分析[J]. 固体力学学报, 2013,34(2):140-151.
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