[a-10] Liquid Rocket 2

[2023-a-44] Flame Response of a Sub- and Supercritical LOX/H2 and LOX/LNG Rocket Combustor with large Optical Access

*Jan Martin¹, Wolfgang Armbruster¹, Michael Börner¹, Justin Hardi¹, Michael Oschwald^1,2 (1. German Aerospace Center (DLR), 2. RWTH Aachen University)

キーワード：rocket engine, optical access, supercritical combustion, subcritical combustion, liquid oxygen / methane