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Effect of Anode Structure on the Plasma Jet Characteristics of Arcjet Thruster

机译:阳极结构对电弧喷射推进器等离子喷射特性的影响

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摘要

In order to study the effects of anode geometry on volt-ampere characteristics and plasma jet characteristics of the arcjet thruster, the arcjet thruster flow characteristics were simulated. Through numerical simulation, the velocity field and temperature field of thruster were calculated, and the volt-ampere characteristics were obtained at different anode geometry. The calculation results show that the influence of the anode throat diameter was the most obvious, compared to the influence of the anode throat length and compression angle on volt-ampere characteristics and plasma jet characteristic of the arcjet thruster.Key words: arcjet thruster / anode structure / plasma jet / volt-ampere characteristics / numerical simulation
机译:为了研究阳极几何形状对电弧喷射推进器的伏安特性和等离子体喷射特性的影响,模拟了电弧喷射推进器的流动特性。通过数值模拟,计算了推进器的速度场和温度场,得到了不同阳极几何形状的伏安特性。计算结果表明,与阳极喉长和压缩角对电弧喷射推进器的伏安特性和等离子喷射特性的影响相比,阳极喉直径的影响最为明显。结构/等离子射流/伏安特性/数值模拟

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