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
200 N-CLASS COMPACT MICRO TURBOJET
A high-performance compact turbojet engine purpose-built for autonomous aerial vehicle (AAV) propulsion. Delivering 200 N of maximum thrust from a 1.8 kg package, it combines a thermally efficient RQL-optimised combustor with CANBUS-enabled digital diagnostics — an ideal powerplant for next-generation compact AAV platforms.
Compact & Light WeightRQL Optimized CombustorAdaptive ECUReliable Start-upCANBUS Diagnostics
PARAMETER
SPECIFICATION
Engine Type
Single Spool Micro Turbojet
Maximum Thrust (N)
200 (ISA)
Max Speed (RPM)
118000
TSFC (Kg/N-Hr)
< 0.16
Max EGT (°C)
< 750
Engine Diameter (mm)
112
Engine Length (mm)
273
Total Weight (kgs)
< 1.8
PHOTOS
VIDEOS