Propellant Flow Analysis within Electric Propulsion Test Facility

Author:

NAKAYAMA Yoshinori1

Affiliation:

1. Department of Aerospace Engineering, National Defense Academy

Publisher

Japan Society for Aeronautical and Space Sciences

Reference15 articles.

1. 1) Randolph, T., Kim, V., Kaufman, H., Kozubsky, K., Zhurin, V. and Day, M.: Facility Effects on Stationary Plasma Thruster Testing, Proceedings of 23rd International Electric Propulsion Conference, Seattle, 1993, IEPC-93-93.

2. 2) Hofer, R., Peterson, P. and Gallimore, A.: Characterizing Vacuum Facility Backpressure Effects on the Performance of a Hall Thruster, Proceedings of 27th International Electric Propulsion Conference, Pasadena, 2001, IEPC-2001-045.

3. 3) Boyd, I., Cai, C., Walker, M. and Gallimore, A.: Computation of Neutral Gas Flow from a Hall Thruster into a Vacuum Chamber, AIP Conference Proceedings, 663(2003), pp.541-548.

4. 4) Walker, M. and Gallimore, A.: Neutral density map of Hall thruster plume expansion in a vacuum chamber, Review of Scientific Instruments, 76(2005), pp. 1-10.

5. 5) Byers, D., and Dankanich, J.: A Review of Facility Effects on Hall Effect Thrusters, Proceedings of 31st International Electric Propulsion Conference, Ann Arbor, 2009, IEPC-2009-076.

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1. Method of Suppressing Ingestion Particles Flowing Back to a Hall Thruster using a Beam Target during Ground Testing;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022

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