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| 离子推进器热特性测试与分析 | |
| 引用本文： | 郑茂繁,江豪成,张天平,顾左. 离子推进器热特性测试与分析[J]. 真空与低温, 2011, 17(2): 96-100. DOI: 10.3969/j.issn.1006-7086.2011.02.007 |
| 作者姓名： | 郑茂繁 江豪成 张天平 顾左 |
| 作者单位： | 兰州空间技术物理研究所,甘肃兰州,730000 |
| 摘 要： | 对离子推进器工作状态的热特性进行了测试与分析。测试分析结果表明：离子推进器工作时产生的热量主要以热传导和热辐射向周围环境传递,通过安装环传导到航天器的热量较少,不会对航天器产生影响。热辐射主要向空间辐射,不会对航天器造成热影响。 |
| 关 键 词： | 电推进 离子推进器 热特性 测试与分析 |
TEST AND ANALYSIS OF THE THERMAL CHARACTERISTIC FOR ION THRUSTER ZHENG Mao-fan |
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| ZHENG Mao-sen,JIANG Hao-cheng,ZHANG Tin-ping,GU Zuo. TEST AND ANALYSIS OF THE THERMAL CHARACTERISTIC FOR ION THRUSTER ZHENG Mao-fan[J]. Vacuum and Cryogenics, 2011, 17(2): 96-100. DOI: 10.3969/j.issn.1006-7086.2011.02.007 | |
| Authors: | ZHENG Mao-sen JIANG Hao-cheng ZHANG Tin-ping GU Zuo |
| Affiliation: | ZHENG Mao-fan,JIANG Hao-cheng,ZHANG Tian-ping,GU Zuo(Lanzhou institute of physics,Lanzhou 730000,China) |
| Abstract: | The thermal characteristic was tested and analyzed for the operating ion thruster.The result indicating: Heat was mostly transferred to ambience through conduction and radiation in the operating ion thruster.Less heat was transferred to spacecraft by fix flange,so it did not influence spacecraft.Radiant heat was mostly transferred to space,and did not influence spacecraft too. |
| Keywords: | electric propulsion ion thruster thermal characteristic test and analysis |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |