Performance Validation of the Six-Degree-of-Freedom Thrust Stand Using a Cold Gas Jet Thruster
Author:
Affiliation:
1. 連絡先著者（Corresponding author）：i.moriai@al.t.u-tokyo. ac.jp
2. 東京大学大学院
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/72/2/72_72_59/_pdf
Reference7 articles.
1. 1) Polk, J. E., Pancotti, A., Haag, T., King, S., Walker, M., Blakely, J. and Ziemer, J.: Recommended Practice for Thrust Measurement in Electric Propulsion Testing, J. Propul. Power, 33, 3 (2017), pp. 539-555.
2. 2) Asakawa, J., Nishii, K., Nakagawa, Y., Koizumi, H. and Komurasaki, K.: Direct Measurement of 1-mN-class Thrust and 100-s-class Specific Impulse for a CubeSat Propulsion System, Rev. Sci. Instrum., 91, 3 (2020), 035116.
3. 3) Zhang, H., Duan, B., Wu, L., Hua, Z., Bao, Z., Guo, N., Ye, Y., DeLuca, L. T. and Shen, R.: Development of a Steady-state Microthrust Measurement Stand for Microspacecrafts, Measurement, 178 (2021), 109357.
4. 4) Nagao, N., Yokota, S., Komurasaki, K. and Arakawa, Y.: Development of a Two-dimensional Dual Pendulum Thrust Stand for Hall Thrusters, Rev. Sci. Instrum., 78, 11 (2007), 115108.
5. 5) Yamashita, Y., Tsukizaki, R., Yamamoto, Y., Koda, D., Nishiyama, K. and Kuninaka, H.: Azimuthal Ion Drift of a Gridded Ion Thruster, Plasma Sources Sci. Technol., 27, 10 (2018), 105006.
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