DescriptionDetails & specsAttachments
Engine Model: TJ-1050 (105 kgf)Maximum Rated Speed: 56,500 rpmMaximum Rated Thrust: 105 kgfMaximum Specific Fuel Consumption (Rated): 1.44 kg/(kgf·h)Maximum Fuel Consumption (Rated): 2,520 g/minMaximum Airflow (Rated): 1.64 kg/sMaximum Pressure Ratio (Rated): 4.35Maximum Exhaust Gas Temperature (EGT): 830 °CIdle Speed: 22,000 rpmThrust at Idle: 8.1 kgfSpecific Fuel Consumption at Idle: 3.56 kg/(kgf·h)Fuel Consumption at Idle: 480.6 g/minEngine Diameter × Overall Length: 215 × 520 mmEngine Weight / System Weight: 12.06 kg / 1.40 kgThrust-to-Weight Ratio (Dry / Total Engine): 9.85 / 8.71Fuel Type: Aviation kerosene with 5% oilLubrication Oil: Mobil Pegasus 2Start Method: Starter motor / fuel-assisted startAcceleration Time: < 6 sDeceleration Time: < 8 sTotal Start Time: < 50 sMaximum Flight Mach Number: 0.9Maximum Launch Altitude: 4,500 mMaximum Operating Altitude: 10,000 mTotal Engine Life / Time Before First Overhaul (TBO): 60 h / 25 hEngine Reference Condition: H = 0 km, Ma = 0, T = 15 °C, P = 101,325 Pa