* two cylinders horizontally opposed; (ENGINE TESTED AND APPROVED BY APOLLO-45G 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: Plus +$5899USD
Model number :B2H170
Displacement :170ccm
Maximum power :15HP
The rotational speed ranges from 1800 to 8000rpm
Applicable fuel: jet coal RP-3
Minimum specific fuel consumption: 388g/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 :5337 g
ECU: 169 g Fuel pump :213 g
CDI :175 g
Wiring harness :200 g
Exterior dimension Length x width x height: 265 x 371.1 x 273.4
Other configurations are optional Damping system Inspired integrated configuration/generator configuration
Recommended propeller specification
Two-bladed propeller: 26x18, 28x16, 28x14, 30x12, 30x10 Three-bladed propeller: 24x18, 24x16, 25x12, 25x14
Audited Supplier 
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