EN-P85 85kgf Thrust Small Turbojet Engine for UAV and RC Jet Aircraft

Thrust: 85 kgf nominal thrust output
الوقود: نفاثة A-1 / كيروسين
Max RPM: 61,500 rpm
Exhaust Temp: 770°C (circumferential average value under standard sea-level static conditions)
Control: Integrated ECU system with intelligent engine management, precise throttle control and real-time operating monitoring
Fuel System: Integrated fuel pump and fuel valve design for simplified installation and reliable operation
Weight & Size: 11 kg total system weight, Ø202 × 479 mm compact structure
Fuel Consumption: 1.38 kg/kgf/h under standard sea-level static conditions
Applications: UAV propulsion systems, RC jet aircraft, experimental aviation platforms, aerospace research and custom turbine projects
Service: OEM/ODM customization, factory-direct manufacturing and global supply by Energy RCJetEngine