Total impulse improvement of coaxial pulsed plasma thruster for small satellite

Author:

Aoyagi Junichiro,Mukai Masayuki,Kamishima Yukiya,Sasaki Tsubasa,Shintani Kouhei,Takegahara Haruki,Wakizono Takashi,Sugiki Mitsuteru

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference9 articles.

1. Kumagai N, Sato K, Kawahara K, Koide T, Takegahara H. Research and development status of low power pulsed plasma thruster system for μ-Lab Sat II. In: 28th International electric propulsion conference; 2003. IEPC-03-0202.

2. Fukushima T, Kawahara K, Koide T, Uezu J, Iio J, Takegahara H. R&D on pulsed plasma thruster for μ-Lab Sat II – development status of EM. In: International symposium on space technology and science; 2004. 2004-b-05.

3. Kamishima Y, Fukushima T, Uezu J, Iio J, Takegahara H. Study on impulse bit increase by modification of PPT configuration. In: 56th International astronautical congress; 2005. IAC-050C4.P02.

4. Uezu J, Iio J, Fukushima T, Kamishima Y, Takegahara H. Study on pulsed plasma thruster configuration to expand impulse bit range. In: 29th International electric propulsion conference; 2005. IEPC-05–234.

5. Edamitsu T, Tahara H. Performance measurement and flowfield calculation of electrothermal pulsed plasma thruster with a propellant feeding mechanism. 29th International electric propulsion conference; 2005. IEPC-05-105.

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