Compact turbojet engine
XM98NG propulsion class.
Compact turbojet engine for small UAV, target drone and experimental aerospace platforms.
Core specifications
- Thrust
- 98 N
- Weight
- 968 g
- Diameter
- 88 mm
- System
- Engine, ECU and telemetry support
Designed for integration work, not catalogue browsing.
The XM98NG 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.