MICRO GAS TURBINE
Reliable Propulsion Systems
For Unmanned Aerial Systems
Next-generation, fuel-flexible micro turbojets engineered for high-altitude performance, rapid deployment, and mission-critical reliability in autonomous aerial platforms.
DET 200
200N CLASS MICRO TURBOJET
Optimized for compact UAV propulsion, DET 200 delivers reliable thrust with a lightweight, thermally efficient design. Ideal for autonomous compact UAVs.
Compact & Light WeightHQL Optimized CombustorAdaptive ECUReliable Start-up
PARAMETER
SPECIFICATION
Maximum Thrust
200 N / 20 kgf
Idle Thrust
7 N / 0.7 kgf
Exhaust Gas Temperature @ Max Thrust
<750(deg C)
TSFC
< 0.161 kg/N-hr
Fuel Type
Jet A1 / Diesel
Fule Pump
BLDC
Fuel Consumption Full Load
631 ml/min
Fuel Consumption Idle Load
85 ml/min
Lubrication
Aeroshell (5%)
Maximum Speed
123,000 RPM
Idle Speed
38,000 RPM
Pressure Ratio
3.8
Total Engine Weight
1.8 kg
Air Flow Rate
0.38 kg/s
Startup Time to Idle
<35 sec
Engine Thrust Control
PWM (CANBUS)
Engine Operating Mach Number
0-0.6
Engine Operating Temperature
-20 to 55(deg C)
Engine Service Interval
25 Hours
Engine Starter
BLDC Starter Motor with Bendix
Max Flight Endurance
Can be specified based on mission profile
Max Operating Altitude
Up to 5 km
Diameter
111 mm
Length
273 mm
PHOTOS
VIDEOS