[G-1] Reusable Launch Vehicles (RLVs) 1

[2022-g-01] Numerical Analysis on Axial Force Characteristics of Reusable Launch Vehicle during Return Phase

*Tomohiro Mamashita¹, Tomotaro Muto², Keiichi Kitamura¹, Satoshi Nonaka³ (1. Yokohama National University, 2. The University of Tokyo, 3. JAXA (Japan Aerospace Exploration Agency))

キーワード：Reusable Launch Vehicle, Numerical Analysis, Flight Scale, Axial Force