DescriptionDetails & specsAttachments
Engine Model: TJ-2000 (200 kgf)Maximum Rated Speed: 41,500 rpmMaximum Rated Thrust: 200 kgfMaximum Specific Fuel Consumption (Rated): 1.30 kg/(kgf·h)Maximum Fuel Consumption (Rated): 4,333.3 g/minMaximum Airflow (Rated): 3.13 kg/sMaximum Pressure Ratio (Rated): 4.6Maximum Exhaust Gas Temperature (EGT): 830 °CIdle Speed: 14,000 rpmThrust at Idle: 11.6 kgfSpecific Fuel Consumption at Idle: 4.10 kg/(kgf·h)Fuel Consumption at Idle: 792.7 g/minEngine Diameter × Overall Length: 295 × 690 mmEngine Weight / System Weight: 29.24 kg / 2.79 kgThrust-to-Weight Ratio (Dry / Total Engine): 7.56 / 6.84Fuel Type: Aviation kerosene with 5% oilLubrication Oil: Mobil Pegasus 2Start Method: Starter motor / fuel-assisted startAcceleration Time: < 10 sDeceleration Time: < 14 sTotal Start Time: < 70 sMaximum Flight Mach Number: 0.95Maximum Launch Altitude: 4,500 mMaximum Operating Altitude: 14,000 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