Plasma-Assisted N2O/CH4 Combustion in a Rotating Gliding Arc Thruster Under Ultra-Lean Conditions (Oxidizer-to-Fuel Ratio 5–1000) | DocHero AI - 专业免费润色翻译工具，助您快速准确翻译英文学术论文
Plasma-Assisted N2O/CH4 Combustion in a Rotating Gliding Arc Thruster Under Ultra-Lean Conditions (Oxidizer-to-Fuel Ratio 5–1000)