N-TET

FC-FDJ-430 UAV Engine

Product Overview
Power
42HP at 6800 RPM
Static thrust
110kg
Main applications
aviation propulsion platforms including UAVs, powered parachutes, and ultralight experimental aircraft.
FC-FDJ-430 UAV engine with displacement 430.8cc, power/performance 42HP at 6800 RPM, static thrust 110kg.

Product Introduction

FC-FDJ-430 is a two-cylinder inline two-stroke engine for UAVs, powered parachutes, ultralight experimental aircraft, and similar aviation platforms. Its structure emphasizes light weight, long service life, high horsepower, and low vibration.

Technical Specifications

ParameterDescription
Bore70mm
Stroke56mm
Displacement430.8cc
Compression ratiotheoretical 11:1 effective 6.5:1
Reduction ratio2.55
Power42HP at 6800 RPM
Static thrust110kg
Maximum RPM7000 RPM
Idle speed1000 RPM
Spark plug14mm DLE-8
Spark plug gap0.6MM
CarburetorDLE self-priming
Fuelgasoline 93# 97#
Fuel mixed oil2T FD grade fully synthetic
Oil mixture ratio50:1
Gearbox lubricantgear oil,85W-140EP API-GL5
Ignition systemdual DC capacitive discharge ignition 12V power supply 5W/个
Generated powerpermanent-magnet generator 14.5V 90W
Starting motor current35A
Rotation directionclockwise (facing the propeller)
Coolingfan cooling
Weightmain engine:27kg;exhaust pipe:4.1kg;total weight:32.25kg
Recommended propeller1.5M variable-pitch carbon-fiber propeller

Get Solution & Quotation

Please fill out the form below, and we can satisfy any of your needs including equipment selection, custom solution design, technical support, or after-sales service. We will contact you as soon as possible.

Home/Drone Accessories/FC-FDJ-430 UAV Engine
FC-FDJ-430 UAV Engine
Power: 42HP at 6800 RPM
Static thrust: 110kg
Main applications: aviation propulsion platforms including UAVs, powered parachutes, and ultralight experimental aircraft.
Get quotation
FC-FDJ-430 UAV engine with displacement 430.8cc, power/performance 42HP at 6800 RPM, static thrust 110kg.

Overview

Product Introduction

FC-FDJ-430 is a two-cylinder inline two-stroke engine for UAVs, powered parachutes, ultralight experimental aircraft, and similar aviation platforms. Its structure emphasizes light weight, long service life, high horsepower, and low vibration.

Technical Specifications

Bore70mm
Stroke56mm
Displacement430.8cc
Compression ratiotheoretical 11:1 effective 6.5:1
Reduction ratio2.55
Power42HP at 6800 RPM
Static thrust110kg
Maximum RPM7000 RPM
Idle speed1000 RPM
Spark plug14mm DLE-8
Spark plug gap0.6MM
CarburetorDLE self-priming
Fuelgasoline 93# 97#
Fuel mixed oil2T FD grade fully synthetic
Oil mixture ratio50:1
Gearbox lubricantgear oil,85W-140EP API-GL5
Ignition systemdual DC capacitive discharge ignition 12V power supply 5W/个
Generated powerpermanent-magnet generator 14.5V 90W
Starting motor current35A
Rotation directionclockwise (facing the propeller)
Coolingfan cooling
Weightmain engine:27kg;exhaust pipe:4.1kg;total weight:32.25kg
Recommended propeller1.5M variable-pitch carbon-fiber propeller

Get Solution & Quotation

Please fill out the form below, and we can satisfy any of your needs including equipment selection, custom solution design, technical support, or after-sales service. We will contact you as soon as possible.

📝 Get Solution & Quotation💬 WhatsApp