LX22 Turbojet engine

Core Parameters​ Compact Design:​ Body diameter 120 mm, length 295 mm, weight only 1900 g. Lightweight structure compatible with integration into compact devices. Extreme Thrust:​ Maximum thrust 220 N, thrust-to-weight ratio as high as 11.8, delivering robust power output. High Efficiency:​ Specific fuel consumption as low as 1.64 kg/(daN·h), leading in fuel economy among comparable models. Peak Performance:​ Supports a maximum speed of 117,000 RPM, operational altitude up to 8000 meters, speed range covers 0–0.8 Mach, and starting altitude adaptable to complex environments from 0 to 4000 meters.