500kg Thrust Turbojet Engine CTJ-8
SKU: MD-P00529·Spare Parts & Components·受注生産
概要
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)
技術仕様
Specifications. 主な仕様： 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。
技術仕様 — 1 groups
主な仕様： 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。
技術仕様
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
対応機体
この部品は以下のプラットフォームに対応します。
適合データの準備中です。機体の型番をお知らせください。