Compact turbojet engine
XM222NG propulsion class.
Compact turbojet engine class for advanced UAV programs that need increased thrust margin.
Core specifications
- Thrust
- 222 N
- Weight
- On request
- Diameter
- On request
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM222NG 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.