Product Overview
The 80KGF micro turbojet engine delivers a standard thrust of no less than 80 kgf and is designed as a compact powerplant for small fixed-wing UAVs, target drones and model aircraft. It features one-click electronic starting, a wide operating temperature range of -40°C to 60°C, and runs on RP-3 aviation kerosene with 3%-5% lubricating oil. Supplied as a complete set including engine body with integrated ECU, clamps and mounting joints, it is easy to integrate and maintain with a 50-hour routine maintenance cycle.
Key Features
- Standard thrust ≥80 kgf (approx. 785 N) for small jet-powered aerial platforms
- Compact and lightweight: 202 mm diameter, 479 mm length, total weight ≤10.5 kg including accessories
- Wide speed range of 30,000-60,200 rpm with rated exhaust temperature of 750°C
- One-click electronic start-up powered by a 28V supply for rapid field deployment
- Fuel-efficient SFC of 1.38 kg/kgf/h, running on RP-3 aviation kerosene
- Operates reliably from -40°C to 60°C with a simple 50-hour maintenance cycle
Technical Specifications
| Parameter | Value |
|---|---|
| Standard Thrust | ≥80 kgf |
| Diameter | 202 mm |
| Length | 479 mm |
| Total Weight (incl. accessories) | ≤10.5 kg |
| Operating Temperature | -40°C ~ 60°C |
| Power Supply Voltage | 28 V |
| Startup Method | One-click electronic start-up |
| Speed Range | 30,000 – 60,200 rpm |
| Rated Exhaust Temperature | 750°C |
| Fuel Consumption Rate | 1.38 kg/kgf/h |
| Fuel | RP-3 Aviation Kerosene |
| Lubricating Oil | 3% – 5% |
| Regular Maintenance Cycle | 50 h |
| Accessories (per set) | Engine body (including ECU, clamps, mounting joints) × 1 |
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