TY - GEN
T1 - Inflow angular dependency on cryopump and beam target in hall thruster test facility
AU - Ito, Gen
AU - Kawashima, Rei
AU - Komurasaki, Kimiya
AU - Koizumi, Hiroyuki
N1 - Publisher Copyright:
© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018
Y1 - 2018
N2 - A role of a beam target installed in ground tests facilities for electric propulsion devices were investigated in terms of induced flow to cryopumps. Cryopumps are widely used for producing high vacuum environments in electric propulsion ground test facilities and their pumping speed depend on an angle where particle flow comes from due to their structure. Particle trajectory from a beam target inside a vacuum chamber for electric propulsion test was calculated by direct simulation Monte Carlo method in a three-dimensional simulation model. Inflow angle of particle flow to pumps varies with a cone angle of a conical beam target, and the peak of inflow angular distribution is 45 degrees on the pump installed at the position where the flux density from the target takes a peak. This result shows that the optimization of the pumping speed of cryopumps is able to be achieved by designing locations of cryopumps with respect to the flux distribution from a beam target..
AB - A role of a beam target installed in ground tests facilities for electric propulsion devices were investigated in terms of induced flow to cryopumps. Cryopumps are widely used for producing high vacuum environments in electric propulsion ground test facilities and their pumping speed depend on an angle where particle flow comes from due to their structure. Particle trajectory from a beam target inside a vacuum chamber for electric propulsion test was calculated by direct simulation Monte Carlo method in a three-dimensional simulation model. Inflow angle of particle flow to pumps varies with a cone angle of a conical beam target, and the peak of inflow angular distribution is 45 degrees on the pump installed at the position where the flux density from the target takes a peak. This result shows that the optimization of the pumping speed of cryopumps is able to be achieved by designing locations of cryopumps with respect to the flux distribution from a beam target..
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U2 - 10.2514/6.2018-4515
DO - 10.2514/6.2018-4515
M3 - Conference contribution
AN - SCOPUS:85066499777
SN - 9781624105708
T3 - 2018 Joint Propulsion Conference
BT - 2018 Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
Y2 - 9 July 2018 through 11 July 2018
ER -