LID B2H170cc HF UAV Engine TBO 300H w/cooling & mounting system Optional One Key Starter/Generator 24V/400W

Manual Video Spare Parts * 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: 26×18, 28×16, 28×14, 30×12, 30×10 Three-blade paddle: 24×18, 24×16, 25×12, 25×14