The U25-P Mechanical Engine is engineered to deliver high-performance propulsion and reliable power output for advanced UAV operations, it provides stable performance and responsive operation across demanding environments.
| Idle Speed | 31000 RPM |
| Idle Torque | 0,85 kg |
| Idle Fuel Consumption | 100 ml/min |
| Max Speed | 117000 RPM |
| Max Thrust | 25 kg |
| Fuel Consumption at Max Speed | 640 g/min |
| Exhaust Gas Temperature | 550°C - 750°C |
| Pressure Ratio | 3.7 |
| Maximum Airflow Rate | 0,47 kg/s |
| SFC Max Speed | 1.6 kg/daN.h |
| Machine Weight | 2.05 kg |
| Diameter | 117 mm |
| Length | 297 mm |
| Max Initial Height | 4600 m |
| Max Operating Height | 10000 m |
| Fuel Mixture | Kerosene or Aviation Diesel |
| Supply Voltage | Battery 3SLi-Po/12V |
| Operational Flow | <3A |
The U55-P Mechanical Engine is engineered to deliver high-thrust propulsion and reliable power output for demanding UAV operations, it provides dependable support for heavy-duty and mission-critical aerial applications.
| Idle Speed | 26000 RPM |
| Idle Torque | 3.0 kg |
| Idle Fuel Consumption | 230 ml/min |
| Max Speed | 83000 RPM |
| Max Thrust | 56 kg |
| Fuel Consumption at Max Speed | 1300 g/min |
| Exhaust Gas Temperature | 550°C-850°C |
| Pressure Ratio | 4 |
| SFC Max Speed | 1.4 kg/daN.h |
| Machine Weight | 4.9 kg |
| Diameter | 175 mm |
| Length | 456 mm |
| Max Initial Height | 4000 m |
| Max Operating Height | 10000 m |
| Fuel Mixture | Kerosene or Aviation Diesel |
| Power Supply Voltage | 12V |
| Initial Flow | <20A |
| Operational Flow | <5A |
The U42-P Mechanical Engine is engineered to deliver reliable propulsion performance and efficient power output for advanced UAV operations, it provides dependable support for long-endurance and mission-critical aerial applications.
| Idle Speed | 35000 RPM |
| Idle Torque | 3.5 kg |
| Idle Fuel Consumption | 240 ml/min |
| Max Speed | 98000 RPM |
| Max Thrust | 42 kg |
| Fuel Consumption at Max Speed | 1300 g/min |
| Exhaust Gas Temperature | 550°C-850°C |
| Pressure Ratio | 4 |
| SFC Max Speed | 1.65 kg/daN.h |
| Machine Weight | 3.95 kg |
| Diameter | 148 mm |
| Length | 390 mm |
| Max Initial Height | 4000 m |
| Max Operating Height | 10000 m |
| Fuel Mixture | Kerosene or Aviation Diesel |
| Power Supply Voltage | 12V |
| Initial Flow | <20A |
| Operational Flow | <5A |
The U85-P Mechanical Engine is engineered to deliver high-thrust propulsion and dependable power output for heavy-duty UAV operations, it provides stable performance and efficient operation across demanding mission environments.
| Idle Speed | 20000 RPM |
| Idle Torque | 4.0 kg |
| Idle Fuel Consumption | 450 ml/min |
| Max Speed | 62000 RPM |
| Max Thrust | 86 kg |
| Fuel Consumption at Max Speed | 1960 g/min |
| Exhaust Gas Temperature | 550°C-850°C |
| Pressure Ratio | 4 |
| Maximum Airflow Rate | 1.35 kg/s |
| SFC Max Speed | 1.35 kg/daN.h |
| Machine Weight | 9.3 kg |
| Diameter | 205 mm |
| Length | 536 mm |
| Max Initial Height | 4000 m |
| Max Operating Height | 10000 m |
| Fuel Mixture | Kerosene or Aviation Diesel |
| Power Supply Voltage | 12V |
| Initial Flow | <20A |
| Operational Flow | <5A |
The T120 Mechanical Engine is engineered to deliver reliable propulsion performance and efficient power output for professional UAV operations, it provides dependable support for long-endurance and mission-critical aerial applications.
| Power | 11.22hp/8.25kW |
| Static Thrust | 26.5kg/Altitude 100m | 23.5kg/Altitude 1800m |
| Max take-off weight | 60kg |
| Recommended Propeller | 26*10;26*12;27*10;28*10 |
| Diameter X Stroke | 45mm X 35mm |
| Displacemet | 120cc |
| Weight | 3.05kg |
| Crankshaft | 3 Ball Bearings |
| Speed Range | 1300 – 7500 RPM |
| Lubricantion Ratio | 25:1 – 30:1 |
| Ignition Voltage | 6.0 – 8.4VDC |
| Fuel | 4.5L/h |
| Dimension | 285*220*222mm |
The T170 Mechanical Engine is engineered to deliver powerful propulsion performance and reliable power output for advanced UAV operations, it provides stable performance and responsive operation across demanding flight environments.
| Power | 18.1hp/13.3kW |
| Static Thrust | 35kg/Altitude 100m | 31.5kg/Altitude 1800m |
| Max take-off weight | 80kg |
| Recommended Propeller | 30*12 ; 32*10 |
| Diameter X Stroke | 51mm X 41mm |
| Displacemet | 170cc |
| Weight | 3.93kg |
| Crankshaft | 3 Bearings crankshaft |
| Speed Range | 1100 – 7500 RPM |
| Lubricantion Ratio | 50:1 |
| Ignition Voltage | 6 – 8.4V DC |
| Fuel | 6L/h |
| Dimension | 340*232*190mm |
The T350 Mechanical Engine is engineered to deliver high-power propulsion and reliable performance for heavy-duty UAV operations, provides stable performance and efficient operation across demanding flight environments.
| Power | 29.37hp/21.6kW |
| Static Thrust | 47.5kg/Altitude 100m | 45.5kg/Altitude 1800m |
| Max take-off weight | 150kg |
| Recommended Propeller | D750*H760 ; 30*20 |
| Diameter X Stroke | 65mm X 50mm |
| Displacemet | 350cc |
| Weight | 11.46kg |
| Crankshaft | High Strength Alloy Steel |
| Speed Range | 2200 – 5600 RPM |
| Lubricantion Ratio | 20:1 |
| Ignition | DC CDI Electronic Ignition |
| Carburetor | All-round carburetor with choke |
| Generator | 36V three-phase AC (Optional 500w/1000w) |
| Fuel | 10L/h |
| Option | Starter 24V/optional electric start |
| Dimension | 360*310*330mm |
The T500 Mechanical Engine is engineered to deliver high-power propulsion and dependable performance for heavy-duty UAV operations, provides dependable support for long-endurance and mission-critical aerial applications.
| Power | 44.88hp/33kW |
| Static Thrust | 60g/Altitude 100m | 55.5kg/Altitude 1800m |
| Max take-off weight | 220kg |
| Recommended Propeller | 30*26 |
| Diameter X Stroke | 75mm X 56mm |
| Displacemet | 500cc |
| Weight | 17kg |
| Crankshaft | High Strength Alloy Steel |
| Speed Range | 2500 – 6000 RPM |
| Lubricantion Ratio | 20:1 |
| Ignition | Solid-state magneto igniton |
| Carburetor | All-round carburetor with choke |
| Generator | Standard 350w, optional 500w 1000w generator |
| Fuel | 13.5L/h |
| Option | Starter 24V |
| Dimension | 440*290*310mm |
The T550 Mechanical Engine is engineered to deliver high-power propulsion and dependable performance for heavy-duty UAV operations, provides stable performance and efficient operation across demanding flight environments.
| Power | 49.62hp/37kW |
| Static Thrust | 70g/Altitude 100m | 61.8kg/Altitude 1800m |
| Max take-off weight | 220kg |
| Recommended Propeller | 32*20 ; 30*23 ; 30*25 |
| Diameter X Stroke | 66mm X 40mm |
| Displacemet | 550cc |
| Weight | 18.3kg |
| Crankshaft | Forging, seven-piece set |
| Speed Range | 1300 – 7500 RPM |
| Lubricantion Ratio | 50:1 |
| Ignition | Solid-state magneto igniton |
| Firing order | 2 Cylinders are ignited synchronously , 180° apart |
| Carburetor | 2 membrane type full range carburetors, without choke |
| Generator | None |
| Piston | Oval grinding, aluminium alloy casting |
| Cylinder | Aluminium alloy casting, inner wall nickell silicon hardening coating |
| Engine Stroke | Two-stroke |
| Layout form | Horizontally opposed, 4 cylinders |
| Starter | Optional |
| Fuel | 14L/h |
| Option | Exhaust pipe Starter Generator |
| Dimension | 430*340*400mm |
The T630 Mechanical Engine is engineered to deliver high-power propulsion and reliable performance for heavy-duty UAV operations, provides dependable support for long-endurance and mission-critical aerial applications.
| Power | 55hp/41kW |
| Speed Range | 2000 – 75000 RPM |
| Max take-off weight | 252kg |
| Recommended Propeller | 40*20 ; 45*20 |
| Spark Plug Type | BM6A |
| Diameter X Stroke | 60mm X 50mm |
| Compression ratio | 10.5 : 1 |
| Displacemet | 630cc |
| Lubrication ratio | 30 : 1 |
| Weight | 18.3kg |
| Ignition Voltage | 6V – 14.4V |
| Starting Power Supply Voltage | 12V – 24V |
| Fuel | 15L/h |
| Option | Electric starter, generator, EFI |
| Dimension | 420*410*370mm |
The T730 Mechanical Engine is engineered to deliver high-power propulsion and dependable performance for heavy-duty UAV operations, provides dependable support for long-endurance and mission-critical aerial applications.
| Power | 63.5hp/47.3kW |
| Speed Range | 2000 – 75000 RPM |
| Max take-off weight | 270kg |
| Recommended Propeller | 40*20 ; 45*20 |
| Spark Plug Type | BM6A |
| Diameter X Stroke | 66mm X 54mm |
| Compression ratio | 10.5 : 1 |
| Displacemet | 730cc |
| Lubrication ratio | 30 : 1 |
| Weight | 18.3kg |
| Ignition Voltage | 6V – 14.4V |
| Starting Power Supply Voltage | 12V – 24V |
| Fuel | 17L/h |
| Option | Electric starter, generator, EFI |
| Dimension | 420*410*370mm |