DescriptionDetails & specsAttachments
Maximum Rated Speed: 61,500 rpmMaximum Rated Thrust: 80 kgfMaximum Specific Fuel Consumption (Rated): 1.35 kg/(kgf·h)Maximum Fuel Consumption (Rated): 1,800 g/minMaximum Airflow (Rated): 1.25 kg/sMaximum Pressure Ratio (Rated): 4.05Maximum Exhaust Gas Temperature (EGT): 830 °CIdle Speed: 30,000 rpmThrust at Idle: 9.6 kgfSpecific Fuel Consumption at Idle: 3.26 kg/(kgf·h)Fuel Consumption at Idle: 521.6 g/minEngine Diameter × Overall Length: 202 × 465 / 480 mmEngine Weight / System Weight: 9.85 kg / 0.68 kg (A), 10.8 kg / 1.21 kg (B)Thrust-to-Weight Ratio (Dry / Total Engine): 8.72 / 8.12 (A), 8.34 / 7.41 (B)Fuel Type: Aviation kerosene with 5% oilLubrication Oil: Mobil Pegasus 2Start Method: Starter motor / fuel-assisted startAcceleration Time: < 8 sDeceleration Time: < 10 sTotal Start Time: < 55 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 hPower Supply (Generator Version): DC 28 V ±1.2 V, max 1,200 WEngine Reference Condition: H = 0 km, Ma = 0, T = 15 °C, P = 101,325 Pa