Description

Performance: 5.5HP/***0rpm (DLE*5 =5.5HP/***0rpm) Idle Speed: ***0 rpm/min.ï&frac*4;ˆDLE*5 ***0 rpm/minï&frac*4;‰ *5.2Kg Pulling Force / **0 meters Altitude(*4.2kg for DLE*5) *3.5Kg Pulling Force / ***0 meters Altitude(*2.5kg for DLE*5) The specification of the aircraft propeller: *2*8, *2**0, *3*8, *3**0 The type of the sparking plug :NGK CM6ï&frac*4;ˆmade in Japanï&frac*4;‰(NGKCM6 made in China for DLE*5) Parameter: Exhaust Amount : *6cm3 (DLE*5 =*5.6cm3 ) Diameter*stroke : *5mm**5mm Ratio of compression: 7.8:1 (7.6:1 for DLE*5) Ratio of lubricating capacity: *0:1 飞起来是*0ï&frac*4;š1 Weight: Less *5g than current DLE*5. Material of Muffer and crank case: aluminium magnesium alloy (Aluminum Alloy for DLE*5) Exhaust Amount : *5.6cm3 Diameter*stroke : *5mmX*5mm Ratio of compression: 7.6:1 Ratio of lubricating capacity: *0:1 Weight: Main engine :***0g Exhaust pipe :**0g Ignition apparatus :**0g