[A-3] Air-breathing Engine 2

[2022-a-13] A Streamline-traced Air Inlet for the Reusable Sounding Rocket with Airbreathing Engines

*Yusuke Maru¹, Haruaki Seta², Kazuma Matsumoto², Tetsuya Sato² (1. Japan Aerospace Exploration Agency, 2. Department of Applied Mechanics and Aerospace Engineering, Waseda University)

キーワード：Air inlet, Airbreather, Busemann inlet, Boundary layer ingestion, Reusable sounding rocket