[G-3] Reusable Launch Vehicles (RLVs) 3

[2022-g-17] Application of Multidisciplinary Design Optimization to Preliminary Design of Suborbital Spaceplane

*Takahiro Fujikawa¹, Koichi Yonemoto^1,2 (1. Tokyo University of Science, Department of Mechanical Engineering, 2. SPACE WALKER Inc.)

キーワード：Suborbital spaceplane, Multidisciplinary design optimization, Preliminary design, Space transportation