Rotax 914
From Wikipedia, the free encyclopedia
The Rotax 914 is a turbo-charged, four-cylinder, horizontally-opposed aircraft engine with air-cooled cylinders and water-cooled heads. It commonly powers light aircraft and UAVs.
[edit] Specifications
- Bore: 79.5 mm (3.1 in)
- Stroke: 61 mm (2.4 in)
- Displacement: 1.2 L (74 cu in)
- Power: 84 kW (115 hp) at 5,800 rpm (with a 5 minute time limit)
[edit] Applications
- Denel Aerospace Systems Bateleur
- Aero Adventure Pegasus
- IAI Heron
- Titan T-51 Mustang
- M&D Flugzeugbau Samburo
- RQ-1 Predator
- NAL Hansa
[edit] References
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