Audited Supplier
* two cylinders horizontally opposed; (ENGINE TESTED AND APPROVED BY APOLLO-15G VTOL drone to achieve over 20 Hours endurance)
* Two strokes;
* Air cooling;
* Dual redunDant speed sensor;
* electronic closed-loop control;
* Optional One Key Starter/generator;
* Own IP development of engine, ECU and fuel pump; (not select the after market one)
* Better environmental adaptability;
* Lower specific fuel consumption to meet the needs of long endurance;
* Engine thermal management technology to ensure engine stability and long TBOH
* The engine body is always in an appropriate temperature range with integrated cooling mounting ;
* Easier to use;
* Higher durability reliability;
24/7 Technical support by our team for protocol integration and support
Optional One Key Starter/Generator 24V/400W:+$4899USD
Model number :B2H120
Displacement :120ccm
Maximum power :10HP
Speed range :1800 to 8000rpm
Applicable fuel :RP-3
Minimum specific fuel consumption: 390g/kwh
Fuel system: Electronic control
Ignition system: Electronic control
Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:50
Cooling method: Air cooling
Throttle control mode: throttle electronic control
Applicable temperature :-30 Celsius ~+55 Celsius
Starting altitude 4000 meters
Output axis rotation: counterclockwise (from the end of the output axis)
Weight composition
Engine body :3620 g
ECU: 169 g
Fuel pump :213 g
CDI :175 g
Wiring harness :166 g
Exterior dimension
Length x width x height: 243 x 330.2 x 242.3mm
Other configurations are optional
Damping system
Inspired integrated configuration/generator configuration
Recommended propeller specification
Two-bladed paddle: 24x18, 26x14, 26x12, 28x12
Three-bladed paddle: /
