Motore VICTOR 2 matricola V213
Riduzione tipo "C" rapporto 1:276
Elica bipala in legno spingente 182 x 119 GT
SCHEDULE OF STATIC THRUST
Engine VICTOR 2 matriculation V213
Type "C" reduction
ratio 1:276
Double blade pushing propeller
wood made
182x119 GT
TESTING CONDITIONS
T 2°C - P 1048 Mb - UR 46%
Locality Torre Maina 17/01/2001
Altitude (S.L.M.) 300 m
RPM Propeller
Turns Kg
of thrust
2200 797 26
3125 1132 69.5
4075 1476 91
4250 1540 100
4435 1607 110
4700 1703 120
5050 1730 140
5350 1938 160
5800 2120 180
5900 2137 200
6000 2173 210
6200 2246 225
TECHNICAL DATA
Displacement
cc
724
Bore
mm
80 x 2
Stroke
mm
72 x 2
Compression Ratio
9,5/1
Power
Hp
92
kW
67,53
RPM
6.200
Weight of the engine ready to fly
Kg 52
Lamellar intake with two Bing 36 carburetors
Alluminium cylinders with Nikasil ceramic coating
Exhausts resonance system. Type "C" reduction
Double Ducati electronic ignition with alternator to recharge battery in fly
Electric starter
Flying consumption at 5400 RPM, 8 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
1:254 - 1:276 - 1:306 - 1:347 - 1:4
