DescriptionDetails & specsAttachments
Engine Model: TJ-3000 (300 kgf)Maximum Thrust: 3,020 NSpecific Fuel Consumption at Maximum Thrust: 0.118 kg/(N·h)Fuel Consumption at Maximum Thrust: 5,993 g/minMaximum Rotational Speed: 36,000 rpmAirflow: 5.18 kg/sExhaust Gas Temperature (EGT): 780 °CEngine Diameter × Length: 251 × 481 mmMain Engine Weight: 35 kgTotal Engine Weight (including auxiliary drive): 42 kgMaximum Launch Altitude: 5,000 mStart Time: 70 sMaximum Operating Altitude: 0–14,000 mMaximum Flight Mach Number: 0–1.3Total Engine Life / First Service Interval (TBO): 100 h / 50 h