* 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 teamaustars for protocol integration and support

Model number :B2H170

Displacement :170cc

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 blades: 26x18, 28x16, 28x14, 30x12, 30x10

Three-blade paddle: 24x18, 24x16, 25x12, 25x14