The Micro Turbojet Engine 80 kg is a compact jet engine delivering 80 kgf thrust at 63,000 RPM, designed for high-speed UAV applications with integrated ECU and solenoid valve.
Key Capabilities
- 80 kgf maximum thrust at maximum RPM
- 63,000 RPM maximum speed with 22,000 RPM idle
- ≥1,000 km/h maximum flight speed capability
- 10,000 m maximum working altitude
- Integrated ECU and solenoid valve inside the engine
- <40 second start time, <4 second acceleration, <6 second deceleration
- JP4 fuel with Aeroshell Turbine Oil 90 lubrication
Technical Specifications
| Thrust @ max RPM | 80 kgf (under standard conditions) |
|---|---|
| Idle thrust | 6 kg |
| Max speed | 63,000 RPM |
| Idle speed | 22,000 RPM |
| Max state thrust | 0.143 kg/N·h |
| Max EGT | 780°C |
| Max working altitude | 10,000 m |
| Max flight speed | ≥1,000 km/h |
| Diameter | 201 mm |
| Length | 465 mm |
| Total weight | 9,000 ± 200 g |
| Fuel | JP4 |
| Lube | Aeroshell Turbine Oil 90 (recommended) |
| ECU, solenoid valve | Integrated inside the engine |
| Start time | <40 s |
| Acceleration time | <4 s |
| Deceleration time | <6 s |
Applications
High-speed UAV propulsion, target drone applications, loitering munition power systems, and jet-powered reconnaissance platforms.
Deployment note: Final configuration, operator training, airspace approval, and local regulatory compliance are required before deployment.
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