תיאור
Parameter
| Performance : | 4.1HP/8500rpm |
| Idle Speed : | 1500 rmp/min |
| Static Thrust : | 9kg/100 meters Altitude |
| Static Thrust : | 7.8kg/1800 meters Altitude |
| Recommended Propeller : | 18×10 ; 19×8 ; 20×8 ; 20×10 ; |
| Spark Plug Type : | NGK CM6 |
| Displacement : | 34.9cm3 |
| Diameter × Stroke : | 38.5mm×30mm |
| Compression Ratio : | 7.6:1 |
| Lubrication Ratio : | 30:1 |
| Weight of Main Engine : | 930g |
| Weight of Exhaust : | 120g |
| Weight of Ignition : | 140g |
| Ignition voltage : | 4.8V-8.4V |
This engine is not a toy , before staring the engine ,read the operators manual carefully ,if failure to do so may result in personal injuries , DLE refuses any liability;Before each operation, check the engine mount ,propeller and airframe carefully to ensure all engine screws and nuts is tight . Loctite(242,243) is strongly recommended during the installation.
■CAUTION : During the break-in period, it is recommended that the engine be installed on the aircraft or a test stand with an appropriate shock absorber. Otherwise it is probable that vibration could rebound back to the engine and serious damages may occur during the break-in period. For your safety and the safety of others, please do not stand in front or in line with the propeller when the engine is running.


