The Platzer MA 12 P/Nissan is a German aircraft engine, produced by Michael Platzer of Guxhagen for use in ultralight aircraft.[1]
| Platzer MA 12 P/Nissan | |
|---|---|
| Type | Aircraft engine |
| National origin | Germany |
| Manufacturer | Michael Platzer |
Design and development edit
The engine is a four-cylinder four-stroke, in-line, 1,235 cc (75.4 cu in) displacement, liquid-cooled, automotive conversion gasoline engine design. It has a poly V belt reduction drive with a reduction ratio of 2.6:1. It employs a magneto ignition system and produces 33 hp (25 kW) at 5600 rpm. The engine has a compression ratio of 10.3:1.[1]
Specifications (Platzer MA 12 P/Nissan) edit
Data from Tacke[1]
General characteristics
- Type: Four cylinder, four stroke aircraft engine
- Bore: 71 mm (2.8 in)
- Stroke: 78 mm (3.1 in)
- Displacement: 1,235 cc (75.4 cu in)
- Length: 650 mm (25.6 in)
- Width: 550 mm (21.7 in)
- Height: 400 mm (15.7 in)
- Dry weight: 54 kg (119.0 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: poly V belt
Performance
- Power output: 33 hp (25 kW)
See also edit
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