TY - GEN
T1 - Numerical simulation of microwave neutralizer including ion’ s kinetic effects
AU - Kubota, K.
AU - Watanabe, H.
AU - Yamamoto, N.
AU - Nakashima, H.
AU - Miyasaka, T.
AU - Funaki, I.
PY - 2014
Y1 - 2014
N2 - In order to analyze a microwave neutralizer in ion’s time/space scales, a three-dimensional Hybrid-PIC (Particle-In-Cell) solver which treats ions and electrons as particles and fluid was developed. In this analysis, microwave power absorption distribution was estimated by means of another electromagnetic PIC solver. The results show that qualitative agreement on voltage-current characteristics was achieved, whereas a discontinuous current jump between a low current mode and a high current mode was still diffused. It is found that, in the high current mode, the electric potential is gradually increased toward the plume region inside the orifice, which promotes high ion production rate there. It is also shown that the sputtering rate of an antenna is comparable with the measured data, where doubly-ionized ions mainly produced inside the orifice considerably aggravate the sputtering rate.
AB - In order to analyze a microwave neutralizer in ion’s time/space scales, a three-dimensional Hybrid-PIC (Particle-In-Cell) solver which treats ions and electrons as particles and fluid was developed. In this analysis, microwave power absorption distribution was estimated by means of another electromagnetic PIC solver. The results show that qualitative agreement on voltage-current characteristics was achieved, whereas a discontinuous current jump between a low current mode and a high current mode was still diffused. It is found that, in the high current mode, the electric potential is gradually increased toward the plume region inside the orifice, which promotes high ion production rate there. It is also shown that the sputtering rate of an antenna is comparable with the measured data, where doubly-ionized ions mainly produced inside the orifice considerably aggravate the sputtering rate.
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U2 - 10.2514/6.2014-3831
DO - 10.2514/6.2014-3831
M3 - Conference contribution
AN - SCOPUS:84913534513
T3 - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
BT - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
Y2 - 28 July 2014 through 30 July 2014
ER -