[F-2] Missions and Future Capabilities 1

[2022-f-07] Development of Osaka Sangyo University 1U Cubesat OSU-1 with 1J/1W Pulsed Plasma Thruster Systems for Powered Flight, and R&D Project Features of Nano-Satellite & Probe OSU-2, 3 and 4

*Kazuki Aoyagi¹, Tomoya Shimada¹, Takuma Unegawa¹, Maika Uedahira¹, Ken-ichiro Oka², Tomonori Kimura², Takayuki Kuri², Kenshin Motoe², Takahiro Itsuki³, Hirokazu Tahara¹, Tomoyuki Ikeda⁴, Yoshiyuki Takao⁵, Takashi Wakizono⁶ (1. Osaka Sangyo University, Department of Mechanical Engineering , 2. Osaka Sangyo University, Solar System Space Development Project, 3. Osaka Sangyo University, Graduate School of Engineering, Division of Mechanical Engineering, 4. Tokai University, 5. Nishinippon Institute of Technology, 6. High Serve, Inc.)

Keywords:Nano-Satellite, Orbital Transfer, Powered Flight, Debris Removal , Electric Propulsion