The Micro Turbojet Engine 160 kg is a powerful compact jet engine delivering 158 kgf thrust at 46,000 RPM, designed for large high-speed UAV applications.
Key Capabilities
- 158 kgf maximum thrust at maximum RPM
- 46,000 RPM maximum speed with 16,000 RPM idle
- ≥1,000 km/h maximum flight speed capability
- 8,000 m maximum working altitude
- Integrated ECU and solenoid valve inside the engine
- <55 second start time, <4 second acceleration, <6 second deceleration
- JP4 fuel with Aeroshell Turbine Oil 90 lubrication
Technical Specifications
| Thrust @ max RPM | 158 kgf (under standard conditions) |
|---|---|
| Idle thrust | 13 kg |
| Max speed | 46,000 RPM |
| Idle speed | 16,000 RPM |
| Max state thrust | 0.148 kg/N·h |
| Max EGT | 780°C |
| Max working altitude | 8,000 m |
| Max flight speed | ≥1,000 km/h |
| Diameter | 260 mm |
| Length | 690 mm |
| Total weight | 17,000 ± 200 g |
| Fuel | JP4 |
| Lube | Aeroshell Turbine Oil 90 (recommended) |
| ECU, solenoid valve | Integrated inside the engine |
| Start time | <55 s |
| Acceleration time | <4 s |
| Deceleration time | <6 s |
Applications
Large high-speed UAV propulsion, heavy-lift jet-powered platforms, loitering munition systems, and extended-range reconnaissance aircraft.
Deployment note: Final configuration, operator training, airspace approval, and local regulatory compliance are required before deployment.
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