Compact turbojet engine
XM166NG propulsion class.
Mid-range compact turbojet platform for demanding unmanned aircraft integration and validation work.
Core specifications
- Thrust
- 166 N
- Weight
- 1,420 g
- Diameter
- 112 mm
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM166NG is positioned for teams evaluating compact turbojet propulsion around aircraft envelope, control architecture, installation constraints and validation route.
- UAV and target platform propulsion studies.
- ECU, sensor and telemetry integration planning.
- Bench validation and flight-test preparation support.