Compact turbojet engine
XM182NG propulsion class.
Compact XM turbojet class for UAV programs requiring a thrust step above the XM166NG range.
Core specifications
- Thrust
- 182 N
- Weight
- On request
- Diameter
- On request
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM182NG 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.