[E-3] High-enthalpy and Hypersonic Flow I

[2022-e-11] Development of an evaluation method for Sample return capsule parachute using Numerical analysis and Wind tunnel tests

*Ryota Samo¹, Hiroki Takayanagi², Riku Shinohara¹, Toshiyuki Suzuki², Shinjiro Umezu¹ (1. Waseda Univ. Faculty of Science and Engineering, 2. Japan Aerospace Exploration Agency)

キーワード：Parachute system, Sample return capsule, wind tunnel