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Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster | |
Pan WX(潘文霞); Huang HJ(黄河激); Wu CK(吴承康) | |
发表期刊 | Plasma Science and Technology |
2010 | |
卷号 | 12期号:4页码:473-477 |
ISSN | 1009-0630 |
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. |
关键词 | Arcjet Thruster Nozzle Temperature Energy Conversion Experimental Measurement |
学科领域 | 交叉与边缘领域的力学 |
DOI | 10.1088/1009-0630/12/4/17 |
URL | 查看原文 |
收录类别 | SCI |
语种 | 英语 |
WOS记录号 | WOS:000281989500017 |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/43281 |
专题 | 等离子体与燃烧中心(2009-2011) |
通讯作者 | Pan WX(潘文霞) |
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. |
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