Compact turbojet engine

XM262NG propulsion class.

Highest thrust compact turbojet propulsion package for advanced and high-payload unmanned aircraft.

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XM262NG propulsion class.

Core specifications

Thrust
262 N
Weight
2.095 g
Diameter
122 mm
System
Engine, ECU and telemetry support

Designed for integration work, not catalogue browsing.

The XM262NG 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.
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XM262NG engine hardware