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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
For deltawing and ulm airplane

SCHEDULE OF STATIC THRUST
Engine VICTOR 1 matriculation V102
Poly-V belt reduction
ratio 1:270
Double blade pushing propeller
wood made
162x112 GT
TESTING CONDITIONS
T 12°C - P 1048 Mb - UR 45%
Locality Torre Maina 04/02/2000
Altitude (S.L.M.) 300 m
RPM Consumption
l/hr
Kg
of thrust
6150 8,8 126
6000 7,8 114
5500 6 94
5000 5 76
4500 3 45
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TECHNICAL DATA
Displacement
cc
362
Bore
mm
80
Stroke
mm
72
Compression Ratio
9,5/1
Power
Hp
44
kW
32,75
RPM
6.200
Weight of the engine ready to fly
Kg 32
Lamellar intake with Bing 36 carburetor
Alluminium cylinder with Nikasil ceramic coating
Exhaust resonance system. Poly-V belt reduction
Double Ducati electronic ignition with alternator to recharge battery in fly
Electric starter
Flying consumption at 5400 RPM, 6 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
1:270 Crown gear 183 mm / Pinion 68 mm
1:280 Crown gear 183 mm / Pinion 65 mm
1:300 Crown gear 183 mm / Pinion 61 mm
Click here to enlarge

Click here to enlarge

Click here to enlarge

Click here to enlarge


POWER AND TORQUE
RPM Hp kW Kgm
3000 15 11,04 3,58
3200 16 11,78 3,58
3500 20 14,72 4,08
4000 24 17,66 4,3
4500 31 22,81 4,87
5000 35 25,76 5,01
5500 38,8 28,56 5,01
6000 42 30,91 5,01
6200 43,5 32,02 5,01
6500 44,5 32,75 4,87
6700 40,6 29,88 4,3
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