[A-4] Combustion

[2022-a-14] Ground Test Evaluation of a Supersonic Combustor Model for JAXA Flight Experiment in Mach 6 Flight Condition

*Masahiro Takahashi¹, Sadatake Tomioka¹, Masao Takegoshi¹, Kan Kobayashi¹, Takuo Onodera¹, Toshihito Saito¹ (1. Japan Aerospace Exploration Agency, Kakuda Space Center)

キーワード：Supersonic combustion, Ground test, Flight test, CFD