Description
Product Overview
The TJ-80 is an 80 kg thrust turbojet engine designed for model aircraft propulsion. It features a compact design, low weight and one-button electronic start capability. With excellent environmental adaptability, it can operate at high altitudes and withstand a wide temperature range, making it suitable for demanding aviation operating conditions.
Key Features
- 80 kgf thrust output for jet-powered model aircraft and aerial platforms
- Lightweight 9.5 kg engine with compact 207 mm diameter
- Wide speed range of 25,000-65,000 rpm
- One-button electronic start for easy ground operation
- Maximum service ceiling of 12,000 m for high-altitude operation
- Operates from -40°C to 50°C on aviation kerosene
Technical Specifications
| Parameter | Value |
|---|---|
| Thrust | 80 kgf |
| Weight | 9.5 kg |
| Diameter | 207 mm |
| Maximum Service Ceiling | 12,000 m |
| Maximum Flight Altitude | 300 m/s |
| Operating Temperature Range | -40°C ~ 50°C |
| RPM Range | 25,000 – 65,000 |
| Maximum Fuel Consumption | 1,850 ml/min |
| Fuel | Aviation Kerosene |
| Startup Method | One-button electronic start |
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