At A Glance
Airplane drone turbojet engines is a significant step forward in drone evolution. It provides significant advantages over piston based drone engines. Well designed air frames can deliver 750km/h (460m/h) speeds and ranges far over 1000 km. UAV-AA engines offer larger thrust allowing delivery of heavier payload or expanding fuel capacity.
| Item | 40 KG Model | 100 KG Model | 150 KG Model |
|---|---|---|---|
| Max Speed (r/min) | 80,000 | 65,000 | 46,000 |
| Max Thrust (daN) | 39.2 | 100 | 150 ± 3 |
| Idle Speed (r/min) | 40,000 | 30,000 | 25,000 |
| Idle Thrust (daN) | 1.8 | 11 | 23.5 |
| Dry Weight (kg) | 4.5 | 9.25 | ＜24 |
| Installed Weight (kg) | 4.7 | 11.5 | ＜27 |
| Airflow (kg/s) | 0.87 | 1.8 | — |
| Max EGT | 750 ℃ | 850 ℃ | 890 ℃ |
| Operating Temp. | -40 ℃ ~ +40 ℃ | -25 ℃ ~ +50 ℃ | -30 ℃ ~ +50 ℃ |
| Max Start Altitude (m) | 5000 | 5,000 | 5,000 |
| Max Operating Altitude (m) | 7,000 | 10,000 | 10,000 |
| Max Mach Number | 0.7 | 0.9 | 0.9 |
| Engine size Length / Diameter: | 375 mm ⌀152 mm | 496 mm ⌀265 mm | 533 mm ⌀263 mm |
Fuel consumption figures for the three engine options.
40KG thrust: at 50% throttle, 40,000 RPM, fuel consumption is 0.6 liters/minute; at 100% throttle, 80,000 RPM, fuel consumption is 1.25 liters/minute.
100KG thrust: at 50% power, 48,000 RPM, fuel consumption is 1.3 liters/minute; at 100% thrust, 65,000 RPM, fuel consumption is 3.2 liters/minute.
150KG thrust: at 60% power, 38,000 RPM, fuel consumption is 2.8 liters/minute; at 100%
power, 46000 RPM, fuel consumption is 4.6 liters/minute.
All turbine components are milled, 3D printed or cast to a highest precision. High thermal alloys such as Inconel 718 can be used to optimize endurance. Proper balanced and fine tuned capabilities of UAV-AA allow increased thrust performance. Further more improvements can be made for custom engines built to a client specs.
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