DescriptionDetails & specsAttachments
Engine Model: TJ-10000 (992 kgf)Configuration: Single-shaft turbojet engine (built-in starter-generator, 2-stage axial compressor + 1-stage centrifugal compressor, annular combustion chamber with oil injector, 1-stage axial turbine)Engine Dimensions (Diameter × Length): 410 × 963 mmMaximum Thrust: 992 kgfSpecific Fuel Consumption (SFC): 1.04 kg/(kgf·h)Operating Altitude: 0–18,000 mMaximum Flight Mach Number: 0–1.8Engine Weight: Main unit: 107 kgAuxiliary Components Weight (including lubrication system & generator module): 28 kgElectrical Generation: 8 kWTotal Engine Life / Time Before Major Overhaul: 600 h / 200 h