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Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster 期刊论文
Plasma Science and Technology, 2010, 卷号: 12, 期号: 4, 页码: 473-477
Authors:  Pan WX(潘文霞);  Huang HJ(黄河激);  Wu CK(吴承康)
Adobe PDF(2666Kb)  |  Favorite  |  View/Download:939/245  |  Submit date:2011/01/06
Arcjet Thruster  Nozzle Temperature  Energy Conversion  Experimental Measurement