Rarefied dynamic pressure distribution measurement near a vacuum pump

Author:

NAKAYAMA Yoshinori1

Affiliation:

1. National Defense Academy of Japan

Publisher

Japan Society of Mechanical Engineers

Reference15 articles.

1. Arakawa, Y., Kuninaka, H., Nakayama, Y. and Nishiyama, K., Ion engines for powered flight in space (2006), pp.99-103, Corona Publishing (in Japanese).

2. Byers, D. and Dankanich, J., A review of facility effects on hall effect thrusters, 31st International Electric Propulsion Conference (2009), Paper No. IEPC-2009-076.

3. Cho, S., Burak, K., Watanabe, H., Kubota, K. and Funaki, I., Feasibility study on facility pressure effect on hall thruster with a numerical simulation, Proceedings of Space Transportation Symposium FY2014 (2015), Paper No. STEP-2014-031 (in Japanese).

4. Dankanich, J., Walker, M., Swiatek, M. and Yim, J., Recommended practice for pressure measurements and calculation of effective pumping speeds during electric propulsion testing, 33rd International Electric Propulsion Conference (2013), Paper No. IEPC-2013-358.

5. Fabris, A. L., Knoll, A., Dannenmayer, K., Schonherr, T., Potterton, T. and Bianco, P., Vacuum facility effects on quad confinement thruster testing, 35th International Electric Propulsion Conference (2017), Paper No. IEPC-2017-250.

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