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VICTOR 1
VICTOR 1 PLUS
VICTOR 1 SUPER
VICTOR 2
VICTOR 2 PLUS
VICTOR 2 SUPER
MINI 2 PLUS
MINI 2 EVO
MINI 3
MINI 4
ENGINE TOOLS
ENGINE PROPELLERS
SUBARU SYSTEM REDUCTION
The most performant engine

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
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FLY PRODUCTS
1° PREMIO MIGLIORE
PARAMOTORE 2002-2004
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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

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POWER AND TORQUE
RPM Hp kW Kgm
3000 9 6,62 2,15
3500 11,2 8,24 2,29
4000 12,8 9,42 2,29
4500 14,4 10,6 2,29
5000 16,5 12,14 2,36
5500 18,7 13,76 2,36
6000 21 15,46 2,51
6500 22,75 16,74 2,51
7000 24,5 18,03 2,51
7500 25,5 18,77 2,43
7800 24,9 18,33 2,29
       
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