[b-13] Pulsed Plasma Thruster

[2023-b-48] Development of Commercially-Available High-Total-Impulse Electrothermal Pulsed Plasma Thruster Systems in Osaka Sangyo University -from Charging Electric Energy/Power: 1J/1W for 1U(1kg) Cubesats to 50J/50W for 50cm Cube (50kg) Nano-Satellites-

*Takuma Unegawa¹, Rika Taniuchi¹, Taiji Yoshimura¹, Ryo Hirata¹, Ren-ichiro Oka¹, Tomonori Kimura¹, Takayuki Kuri¹, Hirokazu Tahara¹, OSU Solar Space Development Project Team², Tomoyuki Ikeda³, Yoshiyuki Takao⁴, Takashi Wakizono⁵ (1. Osaka Sangyo University, Department of Mechanical Engineering , 2. Osaka Sangyo University, 3. Tokai University, 4. Nishinippon Institute of Technology, 5. High Serve, Ltd.)

Keywords:Pulsed Plasma Thruster, Electrothermal Acceleration, Solid Propellant, Small/Nano-Satellites & Cubesat, Powered Flight