Development of a two-dimensional dual pendulum thrust stand for Hall thrusters

被引:20
作者
Nagao, N.
Yokota, S.
Komurasaki, K.
Arakawa, Y.
机构
[1] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, Tokyo 1138656, Japan
[2] Univ Tokyo, Dept Adv Energy, Bunkyo Ku, Tokyo 1138656, Japan
基金
日本学术振兴会;
关键词
D O I
10.1063/1.2815336
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
A two-dimensional dual pendulum thrust stand was developed to measure thrust vectors [axial and horizontal (transverse) direction thrusts] of a Hall thruster. A thruster with a steering mechanism is mounted on the inner pendulum, and thrust is measured from the displacement between inner and outer pendulums, by which a thermal drift effect is canceled out. Two crossover knife-edges support each pendulum arm: one is set on the other at a right angle. They enable the pendulums to swing in two directions. Thrust calibration using a pulley and weight system showed that the measurement errors were less than 0.25 mN (1.4%) in the main thrust direction and 0.09 mN (1.4%) in its transverse direction. The thrust angle of the thrust vector was measured with the stand using the thruster. Consequently, a vector deviation from the main thrust direction of +/- 2.3 degrees was measured with the error of +/- 0.2 degrees under the typical operating conditions for the thruster. (c) 2007 American Institute of Physics.
引用
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页数:4
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