500kg Thrust Turbojet Engine CTJ-8
SKU: MD-P00529·Spare Parts & Components·حسب الطلب
نظرة عامة
Compressor: 3-stage axial flow, the supercharging ratio is 3.8, of which the first-stage compressor is a titanium alloy integral blade rotor (IBR). Combustion chamber : DC annular combustion chamber, 12 centrifugal fuel atomizing nozzles. Turbine: 1st stage axial flow. Nozzle : Simple Converging Nozzle. Control system : Electronic fuel control system. Fuel system : Use RP-3 fuel. Lubricating oil system : 4010 lubricating oil is used. Lgnition system : Compressed air blow, electric igniter or high energy igniter ignition. Accessories : comes with a 4kW generator system. Others : The unique oil seal structure makes the engine life longer. Maximum thrust (CTJ-8A, H=0, Ma0): 4.9kN Takeoff thrust (H=0, Ma0.7): 3.2kN Cruising thrust (H=8000m, Ma0.7): 1.5kN Take-off state: 182kg/(kN h)
المواصفات التقنية
Specifications. المواصفات الرئيسية: Combustion chamber DC annular combustion chamber, 12 centrifugal fuel atomizing nozzles.، Turbine 1st stage axial flow.، Nozzle Simple Converging Nozzle.، Control system Electronic fuel control system.، Fuel system Use RP-3 fuel.، Lubricating oil system 4010 lubricating oil is used.، Lgnition system Compressed air blow, electric igniter or high energy igniter ignition.، Accessories comes with a 4kW generator system.، Others The unique oil seal structure makes the engine life longer.، Length 1250mm، Diameter 330mm، Dry mass 67kg، Maximum thrust (CTJ-8A, H=0, Ma0) 4.9kN، Takeoff thrust (H=0, Ma0.7) 3.2kN، Cruising thrust (H=8000m, Ma0.7) 1.5kN، Take-off state 182kg/(kN h)، Life span 80~150h.
المواصفات التقنية — 1 groups
المواصفات الرئيسية: Combustion chamber DC annular combustion chamber, 12 centrifugal fuel atomizing nozzles.، Turbine 1st stage axial flow.، Nozzle Simple Converging Nozzle.، Control system Electronic fuel control system.، Fuel system Use RP-3 fuel.، Lubricating oil system 4010 lubricating oil is used.، Lgnition system Compressed air blow, electric igniter or high energy igniter ignition.، Accessories comes with a 4kW generator system.، Others The unique oil seal structure makes the engine life longer.، Length 1250mm، Diameter 330mm، Dry mass 67kg، Maximum thrust (CTJ-8A, H=0, Ma0) 4.9kN، Takeoff thrust (H=0, Ma0.7) 3.2kN، Cruising thrust (H=8000m, Ma0.7) 1.5kN، Take-off state 182kg/(kN h)، Life span 80~150h.
المواصفات الفنية
Specifications
- Combustion chamber
- DC annular combustion chamber, 12 centrifugal fuel atomizing nozzles.
- Turbine
- 1st stage axial flow.
- Nozzle
- Simple Converging Nozzle.
- Control system
- Electronic fuel control system.
- Fuel system
- Use RP-3 fuel.
- Lubricating oil system
- 4010 lubricating oil is used.
- Lgnition system
- Compressed air blow, electric igniter or high energy igniter ignition.
- Accessories
- comes with a 4kW generator system.
- Others
- The unique oil seal structure makes the engine life longer.
- Length
- 1250mm
- Diameter
- 330mm
- Dry mass
- 67kg
- Maximum thrust (CTJ-8A, H=0, Ma0)
- 4.9kN
- Takeoff thrust (H=0, Ma0.7)
- 3.2kN
- Cruising thrust (H=8000m, Ma0.7)
- 1.5kN
- Take-off state
- 182kg/(kN h)
- Life span
- 80~150h
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