[D-15] Trajectory Design and Optimization 2

[2022-d-62] Study of an Orbital Transition Scenario for Medium-sized Lunar Cargo Lander Mission

*Yuki Matsumoto¹, Satoshi Ueda¹, Junji Kikuchi¹, Masaru Koga¹, Kota Tanabe¹, Naoki Satoh¹ (1. Japan Aerospace Exploration Agency)

キーワード：Medium-sized Lunar Cargo Lander Mission, Trajectory Design, Weak Stability Boundary