Knowledge Management System of Institue of Mechanics, CAS
| 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)
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| Source Publication | Plasma Science and Technology (IF:1.193[JCR-2018],1.009[5-Year]) |
| 2010 | |
| Volume | 12Issue:4Pages:473-477 |
| ISSN | 1009-0630 |
| Abstract | 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. |
| Keyword | Arcjet Thruster Nozzle Temperature Energy Conversion Experimental Measurement |
| Subject Area | 交叉与边缘领域的力学 |
| DOI | 10.1088/1009-0630/12/4/17 |
| URL | 查看原文 |
| Indexed By | SCI |
| Language | 英语 |
| WOS ID | WOS:000281989500017 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/43281 |
| Collection | 等离子体与燃烧中心(2009-2011) |
| Corresponding Author | Pan WX(潘文霞) |
| Recommended Citation 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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| 1009-0630_12_4_17.pd（2666KB） | 开放获取 | License | View Download | |||
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