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CATALOGUE

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AIRCRAFT ENGINEERING AND MAINTENANCE<br />

ENGINES<br />

SH-340<br />

TWO- STROKE FOUR-CYLINDER<br />

AIR-COOLED ENGINE<br />

Main Specifications:<br />

Take-off weight<br />

up to 160 kg<br />

Cylinder capacity 340 cm 3<br />

Bore<br />

52 mm<br />

Stroke<br />

40 mm<br />

Degree of compression 9,5<br />

Maximum torque (at 6750 rpm)<br />

22,8 N/m<br />

RPM range<br />

1100…8800 rpm<br />

Fuel A 95-98 Gasoline with synthetic oil for two-cycle engines in the ratio 50:1<br />

Specific Fuel Consumption (at 75% power)<br />

370 gHP/hr<br />

Carburetor<br />

Two floatless Walbro WB with integral fuel pump<br />

Ignition system<br />

Magneto or contactless electronic, battery ignition<br />

Weight<br />

8220 g<br />

ASO-2V, ASO-2VM<br />

AUTOMATIC CHAFF DISPENSER<br />

It is used on the An-Series aircrafts and<br />

Mi-Series helicopters and designed for<br />

jamming missile radars and IR seekers.<br />

Main Specifications:<br />

Operating voltage<br />

27 V<br />

Magazine capacity (Qty of rounds in 1 section) 32<br />

Overall dimensions (without connectors)<br />

768,5x125,5x60,5<br />

Weight:<br />

ASO-2V<br />

12,7 kg<br />

ASO-2VM<br />

14,9 kg<br />

101

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