33rd International Symposium on Space Technology and Science, 10th Nano-Satellite Symposium & 14th IAA Low-Cost Planetary Missions Conference

Presentation information

Oral Session

e) Fluid Dynamics and Aerothermodynamics

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

Wed. Mar 2, 2022 4:00 PM - 5:00 PM Meeting Room3 (BF1)

Chair:Kojiro SUZUKI, Yasumasa WATANABE

4:00 PM - 4:20 PM

[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)

Keywords:Parachute system, Sample return capsule, wind tunnel

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