[D-8] Mission Design 1

[2022-d-34] Trajectory and Attitude Planning during Deep Space Insertion from GTO for Microsatellite having High Thrust Propulsion System

*Tomotaka Yamamoto¹, Yosuke Kawabata¹, Ryu Funase¹, Shinichi Nakasuka¹ (1. The University of Tokyo)

キーワード：Deep space escape trajectory, Piggyback mission, Spin stabilization