Compact turbojet engine
XM122NG propulsion class.
Lightweight propulsion class for UAV programs that need a compact thrust step with controlled installation mass.
Core specifications
- Thrust
- 122 N
- Weight
- 978 g
- Diameter
- 88 mm
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM122NG 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.