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 compactness, DET 200 delivers reliable thrust with a lightweight, thermally efficient design. Ideal for autonomous aerial platforms.
Compact & Light WeightRQL Optimized CombustorAdaptive ECUReliable Start-up
PARAMETER
SPECIFICATION
Engine Type
MICROTURBOJET, single spool
Maximum Thrust (N)
200
Maximum Speed (RPM)
118,000
Idle Speed (RPM)
38,000
TSFC (kg/N-hr)
< 0.161
Pressure Ratio
3.6
Total Weight of Engine (Kg)
1.8
Engine Diameter (mm)
111
Engine Length (mm)
273
Fuel
Jet A1, Diesel
Maximun EGT (°C)
<750
Maximum Altitude (m)
5000
PHOTOS
VIDEOS