Compact turbojet engine
XM255NG propulsion class.
High-thrust XM engine class for advanced UAV and target platform propulsion requirements.
Core specifications
- Thrust
- 255 N
- Weight
- 2,080 g
- Diameter
- 132 mm
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM255NG 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.