SCHEDULE OF STATIC THRUST
Engine MINI 2 PLUS matriculation M2210
Poly-V belt reduction, ratio 1:230
Double blade pushing propeller wood made 126 GT
TESTING CONDITIONS
T 2°C - P 1048 Mb - UR 46%
Locality Torre Maina 18/02/2001
Altitude (S.L.M.) 300 m
RPM Consumption
l/hr Kg
of thrust
7200 5,8 86
7000 5,6 82
6800 5,4 78
6600 5,2 72
6400 4 66
6000 3,5 58
5500 2,5 48
5000 2,2 44
4500 2 31
4000 1,5 28

FLY PRODUCTS
1° PREMIO MIGLIORE
PARAMOTORE 2002-2004

TECHNICAL DATA
Displacement cc 202
Bore mm 66,4
Stroke mm 58
Compression Ratio 10,5/1
Power Hp 26 kW 19
RPM 7.500
Weight of the engine ready to fly Kg 18.3
Lamellar intake with Walbro WB 37 carburetor
Alluminium cylinder with Nikasil coating
Air-cooling
Exhaust resonance system. Poly-V belt reduction
Electronic ignition with alternator to recharge battery in fly
Electric starter
Flying consumption at 5000 RPM, 2,2 liters/hour
Premix two stroke oil gasoline, 2,5% oil by volume to leaded fuel, 3% oil by volume to unleaded fuel

REDUCTION RATIO AVAIABLE
1:226 Crown gear 129 mm / Pinion 57 mm
1:230 Crown gear 129 mm / Pinion 56 mm
1:234 Crown gear 129 mm / Pinion 55 mm
1:242 Crown gear 129 mm / Pinion 53,3 mm