Parametric Kinetic Simulation of an IHI High Specific Impulse SPT-Type Hall Thruster
Parametric Kinetic Simulation of an IHI High Specific Impulse SPT-Type Hall Thruster
复制标题
IHI 高比冲 SPT 型霍尔推进器的参数动力学仿真
DOI:
10.2514/6.2014-3426
复制
发表时间:
2014
期刊:
影响因子:
--
通讯作者:
I. Funaki
中科院分区:
文献类型:
--
作者:
Shinatora Cho;Hiroki Watanabe;K. Kubota;Shigeyasu Iihara;K. Honda;K. Fuchigami;K. Uematsu;I. Funaki
A 1 kW class magnetic layer type Hall thruster designed for high specific impulse operation by IHI Corporation, Japan was modeled by a fully kinetic particle code. The measured maximum performance of the thruster was 64% in anode efficiency and 3,200s (3.1kW, 800V) in anode specific impulse. The thruster performance, wall heat loss and erosion, and the plasma property distributions were numerically investigated for the operation conditions ranged from 300V to 700V in discharge voltage, and 2mg/s to 4mg/s in xenon mass flow rate. Simulations with two numerical models: with and without the Bohm diffusion assumption were performed for each thruster operation conditions to characterize the uncertainty caused by the Bohm diffusion model. The simulation results were compared with the measured results, and exhibited excellent agreement with the maximum performance error of 20% for both models. It is suggested that as engineering tools, with and without Bohm simulations can be respectively used as the worst and best case analysis for the performance, heat load, and erosion.
DOI:
10.2514/6.2010-6862
发表时间:
2010-07
期刊:
--
影响因子:
--
作者:
K. Nishiyama;S. Hosoda;H. Koizumi;Y. Shimizu;I. Funaki;H. Kuninaka;M. Bodendorfer;J. Kawaguchi;D. Nakata
通讯作者:
K. Nishiyama;S. Hosoda;H. Koizumi;Y. Shimizu;I. Funaki;H. Kuninaka;M. Bodendorfer;J. Kawaguchi;D. Nakata
DOI:
--
发表时间:
2008
期刊:
Frontier of Applied Plasma Technology 1
影响因子:
--
作者:
S. Yokota;Y. Fukushima;R. Tsukizaki;K. Komurasaki;Y. Arakawa;A. Kobayashi
通讯作者:
A. Kobayashi