Thrust: 550 NEngine Diameter × Length: 175 × 456 mmEngine Casing Weight: 4.7 kgMaximum Operating Altitude: 9,000 mMaximum Launch Altitude: 4,500 mStart Time: 40 sOperating Temperature: −25 °C to +50 °CFlight Speed Range: Mach 0–0.85Start Speed Range: Mach 0–0.5Maximum Rotational Speed: 83,000 rpmMaximum Runtime at Full Speed: 12 minIdle Speed: 35,000 rpmExhaust Gas Temperature (EGT): ≤ 830 °CFuel Consumption at Maximum Thrust: 1,300–1,330 g/minFuel Type: Aviation Kerosene #3Lubrication Oil: 3%–5% Mobil Pegasus #2Total Engine Life / Time Before First Overhaul (TBO): 60 h / 25 h