[f-4] Missions 4: Lunar and Interplanetary Missions

[2023-f-19] System Design of 50kg-class Microsatellite with High Thrust Propulsion System

*Shintaro Nakajima¹, Ralf Boden¹, Yosuke Kawabata², Ryota Fuse², Kazuma Fujimoto², Akihiro Ishikawa², Ryu Funase^1,2 (1. Japan Aerospace Exploration Agency, 2. The University of Tokyo)

キーワード：System design, High thrust propulsion system, Reliability, Interplanetary microsatellite