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The Jabiru 2200 is a lightweight four-stroke, horizontally-opposed aircooled engine, used in aircraft. The engine is direct drive and is fitted with alternators, silencers, vacuum pump drives and dual ignition systems as standard.

[edit] Specifications

General characteristics

• Type: Flat-4
• Bore: 97.5 mm (3.84 in)
• Stroke: 74 mm (2.91 in)
• Displacement: 2200 cm³ (134 in³)
• Length: 562 mm (22.12 in)
• Width: 582 mm (22.91 in)
• Height: 445 mm (17.54 in)
• Dry weight: 60 kg (132 lbs) with exhaust, carburetors, starter motor, alternator & ignition system

<h3>Components

• Fuel system: Mechanical fuel pump
• Fuel type: AVGAS 100/130
• Oil system: Wet sump
• Cooling system: Aircooled

<h3>Performance

• Power output: 64 kW (85 hp) @ 3300 RPM
• Specific power:
• Compression ratio: 8:1
• Fuel consumption: 15 liters/h @ 2750 RPM (75% power)
• Power-to-weight ratio: 1.07 kW/kg

[edit] References

• Jabiru Aircraft: 4 Cylinder Engine
• Horizontally-Opposed Piston Aero Engines: Jabiru