Jabiru 5100
From Wikipedia, the free encyclopedia
The Jabiru 5100 is a lightweight four-stroke, horizontally-opposed aircooled aircraft engine, manufactured by Jabiru Aircraft.
The engine is direct drive and is fitted with alternators, silencers, vacuum pump drives and dual ignition systems as standard equipment.
[edit] Specifications
General characteristics
- Type: Flat-8
- Bore: 97.5 mm (3.84 in)
- Stroke: 85.0 mm (3.346 in)
- Displacement: 5077 cm³ (310 in³)
- Length: 960 mm (37.79 in)
- Width: 638 mm (25.12 in)
- Height: 445 mm (17.54 in)
- Dry weight: 117 kg (257 lbs) with exhaust, carburetors, starter motor, alternator & ignition system
Components
- Fuel system: Mechanical fuel pump
- Fuel type: AVGAS 100/130
- Oil system: Wet sump
- Cooling system: Aircooled
Performance
- Power output: 126.8 kW (170 hp) @ 2700 RPM (continuous); 134.2 kW (180 hp) @ 3000 RPM (intermittent)
- Compression ratio: 8:1
- Fuel consumption: 26 liters/h @ 2750 RPM (75% power)
- Power-to-weight ratio: 1.10 kW/kg
