Compact turbojet engine
XM250NG propulsion class.
250 N compact turbojet propulsion class for demanding UAV and special mission platform requirements.
Core specifications
- Thrust
- 250 N
- Weight
- On request
- Diameter
- On request
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM250NG 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.