The 6,500-H Life Test Results of 30 cm Diameter Ion Thruster

IF 0.9 Q3 ENGINEERING, AEROSPACE Journal of Aerospace Technology and Management Pub Date : 2021-02-10 DOI:10.1590/JATM.V13.1202
Sun Mingming, Geng Hai, Zheng Yi
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Abstract

The life test of the 30 cm diameter ion thruster developed by the Lanzhou institute of physics began in Apr. 2018 and ended in Jan. 2020, lasting 6,500 h. This paper introduces the results of the 6,500-h life test of the 30 cm diameter ion thruster completed on the ground, including the ground facility for life test, the variations of the thrusters working performance, the times of the breakdown and power restart, and the erosion of the key components. The results show that the performance parameters, such as thrust, specific impulse and efficiency, do not change obviously during the test and magnetic field of the discharge chamber has no change. With the increase of test time, breakdown times increased significantly, whereas the power restart time decreased correspondingly. The diameter of the cathode orifice decreases gradually and there is a blockage risk of orifice. However, the diameter of the keeper orifice increases and presents an inverted cone erosion pattern. The diameter of the decelerator grid aperture expanded from 1.6 to 1.8 mm from 0 to 1,000 h and slightly enlarged after that. The aperture diameter of the accelerator grid presented linear enlargement but the pits-and-grooves erosion is obvious.
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直径30cm离子推进器6500-H寿命试验结果
兰州物理研究所研制的直径为30cm的离子推进器的寿命试验从2018年4月开始,到2020年1月结束,历时6500小时。本文介绍了在地面完成的直径为30mm的离子推进器6500小时的寿命试验结果,包括用于寿命试验的地面设施、推进器工作性能的变化,故障和电源重启的次数,以及关键部件的侵蚀。结果表明,在试验过程中,推力、比冲和效率等性能参数没有明显变化,放电室的磁场也没有变化。随着测试时间的增加,击穿次数显著增加,而电源重启时间相应减少。阴极孔的直径逐渐减小,存在孔堵塞的风险。然而,保持器孔口的直径增加,并呈现倒锥形侵蚀模式。减速器栅格孔径的直径从0到1000h从1.6到1.8mm扩大,此后略有扩大。加速器格栅孔径呈线性增大,但坑槽侵蚀明显。
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CiteScore
2.00
自引率
0.00%
发文量
16
审稿时长
20 weeks
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