[F-6] NSAT&LCPM Joint Session: Lunar and Interplanetary Missions

[2022-f-27] System Design of Interplanetary Microsatellite with High Thrust Propulsion System

*Shintaro Nakajima¹, Yosuke Kawabata², Tomotaka Yamamoto², Kazuma Fujimoto², Akihiro Ishikawa², Ryu Funase^1,2 (1. Institute of Space and Astronautical Science, JAXA, 2. The University of Tokyo)

キーワード：System design, Reliability, Interplanetary microsatellite