Compact turbojet engine
XM210NG propulsion class.
Higher-thrust XM propulsion class for compact unmanned aircraft and target platform integration studies.
Core specifications
- Thrust
- 210 N
- Weight
- On request
- Diameter
- On request
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM210NG 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.