MICRO GAS TURBINE
Reliable Propulsion Systems
For Unmanned Aerial Systems
Optimized for compact UAV propulsion with reliable thrust and thermally efficient design. Ideal for autonomous compact UAVs.
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
TSFC
< 0.161 kg/N-hr
Fuel Type
Jet A1 / Diesel
Maximum Speed
123,000 RPM
Idle Speed
37,000 RPM
Pressure Ratio
3.8 ± 0.2
EGT @ Max Thrust
< 750 °C
Total Engine Weight
< 1.8 kg
Max Flight Endurance
Up to 45 min
Max Operating Altitude
Up to 5 km
Diameter
111 mm
Length
288 mm
PHOTOS
DET 200 — IMAGE 1
VIDEOS
DET 200 — VIDEO 1
DET 200 — Technical Specification Sheet
PDF · DATASHEET · REPLACE HREF WITH ACTUAL FILE URL