500kg Thrust Turbojet Engine CTJ-8
SKU: MD-P00529·Spare Parts & Components·Bajo pedido
Vista general
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)
Especificación técnica
Specifications. Especificaciones clave: 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.
Especificación técnica — 1 groups
Especificaciones clave: 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.
Especificaciones técnicas
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
Aeronaves compatibles
Esta pieza se adapta a las siguientes plataformas.
Datos de compatibilidad pendientes — contáctenos con el modelo de su aeronave.