Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster
文献类型：期刊论文
| 作者 | Pan WX(潘文霞) ; Huang HJ(黄河激); Wu CK(吴承康)
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| 刊名 | Plasma Science and Technology
 |
| 出版日期 | 2010 |
| 卷号 | 12期号:4页码:473-477 |
| 通讯作者邮箱 | wxpan@imech.ac.cn |
| 关键词 | arcjet thruster, nozzle temperature, energy conversion, experimental measurement |
| ISSN号 | 1009-0630 |
| 通讯作者 | 潘文霞 |
| 合作状况 | 其它 |
| 中文摘要 | A 1 kW-class arcjet thruster was ¯red in a vacuum chamber at a pressure of 18 Pa. A gas mixture of H2 : N2 = 2.8 : 1.5 in volume at a total °ow rate of 4.3 slm was used as the propellant with an input power ¯xed at 860 W. The time-dependent thrust, nozzle temperature and inlet pressure of the propellant were measured simultaneously. Results showed that with the increase in nozzle temperature the thrust decreased and various losses increased. The physical mechanisms involved in these effects are discussed. |
| 学科主题 | 交叉与边缘领域的力学 |
| 收录类别 | SCI |
| 原文出处 | http://iopscience.iop.org/1009-0630/12/4/17/ |
| 语种 | 英语 |
| WOS记录号 | WOS:000281989500017 |
| 公开日期 | 2011-01-06 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/43281]  |
| 专题 | 力学研究所_等离子体与燃烧中心(2009-2011) |
| 推荐引用方式 GB/T 7714 | Pan WX,Huang HJ,Wu CK. Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster[J]. Plasma Science and Technology,2010,12(4):473-477. |
| APA | 潘文霞,黄河激,&吴承康.(2010).Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster.Plasma Science and Technology,12(4),473-477. |
| MLA | 潘文霞,et al."Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster".Plasma Science and Technology 12.4(2010):473-477. |
入库方式： OAI收割
来源：力学研究所
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