40kg Thrust Turbojet CTJ-16
SKU: MD-P00530·Spare Parts & Components·Auf Bestellung
Übersicht
This is a micro turbojet engine specially developed for target drones and small tactical missiles. Compressor: 1-stage centrifugal type with a boost ratio of 3.9. Combustion chamber: annular baffle combustion chamber. Turbine: 1-stage centripetal. Nozzle: Simple Converging Nozzle. Control system: digital electronic control system. Fuel system: Use RP-3 fuel. Lubricating oil system: 4010 lubricating oil is used. Ignition system: motor start or compressed air start, spark plug or electric igniter ignition. Accessories: starter motor, brushless electric fuel pump. Cruising thrust ( H =0, Ma 0.3): 0.28kN Take-off state: 156kg/(kN h)
Technische Daten
Specifications. Wichtige technische Daten: Compressor 1-stage centrifugal type with a boost ratio of 3.9., Combustion chamber annular baffle combustion chamber., Turbine 1-stage centripetal., Nozzle Simple Converging Nozzle., Control system digital electronic control system., Fuel system Use RP-3 fuel., Lubricating oil system 4010 lubricating oil is used., Ignition system motor start or compressed air start, spark plug or electric igniter ignition., Accessories starter motor, brushless electric fuel pump., Length 345mm, Diameter 158mm, Dry mass 23kg, Takeoff thrust 0.42kN, Cruising thrust ( H =0, Ma 0.3) 0.28kN, Take-off state 156kg/(kN h), Life 20h.
Technische Daten — 1 groups
Wichtige technische Daten: Compressor 1-stage centrifugal type with a boost ratio of 3.9., Combustion chamber annular baffle combustion chamber., Turbine 1-stage centripetal., Nozzle Simple Converging Nozzle., Control system digital electronic control system., Fuel system Use RP-3 fuel., Lubricating oil system 4010 lubricating oil is used., Ignition system motor start or compressed air start, spark plug or electric igniter ignition., Accessories starter motor, brushless electric fuel pump., Length 345mm, Diameter 158mm, Dry mass 23kg, Takeoff thrust 0.42kN, Cruising thrust ( H =0, Ma 0.3) 0.28kN, Take-off state 156kg/(kN h), Life 20h.
Technische Daten
Specifications
- Compressor
- 1-stage centrifugal type with a boost ratio of 3.9.
- Combustion chamber
- annular baffle combustion chamber.
- Turbine
- 1-stage centripetal.
- Nozzle
- Simple Converging Nozzle.
- Control system
- digital electronic control system.
- Fuel system
- Use RP-3 fuel.
- Lubricating oil system
- 4010 lubricating oil is used.
- Ignition system
- motor start or compressed air start, spark plug or electric igniter ignition.
- Accessories
- starter motor, brushless electric fuel pump.
- Length
- 345mm
- Diameter
- 158mm
- Dry mass
- 23kg
- Takeoff thrust
- 0.42kN
- Cruising thrust ( H =0, Ma 0.3)
- 0.28kN
- Take-off state
- 156kg/(kN h)
- Life
- 20h
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