LX30 Turbojet engine

Core Specifications​ Dimensions & Weight:​ Body diameter 132mm, length 330mm, weight 2800g; compact structure with multi-scenario deployment capability. High Thrust Output:​ Maximum thrust 290N, thrust-to-weight ratio up to 10.5; efficient power delivery. Fuel Economy:​ Specific fuel consumption 1.59 kg/(daN·h), balancing power and energy efficiency. Extreme Performance:​ Maximum speed 106,000 RPM, operational altitude 0–8000m, speed range 0–0.8 Mach, starting altitude adaptable for complex environments from 0 to 4000m.