HKS 700E
http://dbpedia.org/resource/HKS_700E an entity of type: AircraftEngine102687423
The HKS 700E is a twin-cylinder, horizontally opposed, four stroke, carburetted aircraft engine, designed for use on ultralight aircraft, powered parachutes and ultralight trikes. The engine is manufactured by HKS, a Japanese company noted for its automotive racing engines.
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HKS 700E
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25558267
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1017601335
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two intake and two exhaust valves per cylinder
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at 6200 rpm for three minutes for take-off and at 5800 rpm continuous
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Cliche & HKS
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Twin cylinder four-stroke aircraft engine
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Two cylinder, four-stroke aircraft engine
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equipped with electrical system, electric starter, carburetors, gearbox, exhaust system, oil tank and cooler
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The HKS 700E is a twin-cylinder, horizontally opposed, four stroke, carburetted aircraft engine, designed for use on ultralight aircraft, powered parachutes and ultralight trikes. The engine is manufactured by HKS, a Japanese company noted for its automotive racing engines.
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11.3
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free air cylinders, with oil-cooled cylinder heads
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680.0
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dry sump with a trochoid pump
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A-type gearbox with 2.58:1 ratio, limit of 4,000kg/cm2 inertial load. The B-type gearbox with 3.47:1 ratio, limit of 6,000kg/cm2 inertial load
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*Jabiru 2200
*KFM 112M
*Pegasus PAL 95
*Rotax 912
*ULPower UL260i
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8555