Hirth 3002
German two-stroke aircraft engine
From Wikipedia, the free encyclopedia
The Hirth 3002 is a German aircraft engine, that was designed and produced by Hirth of Benningen for use in ultralight aircraft.[1]
| Hirth 3002 | |
|---|---|
| Type | Aircraft engine |
| National origin | Germany |
| Manufacturer | Hirth |
By March 2018, the engine was no longer advertised on the company website and seems to be out of production.[2]
Design and development
The Hirth 3002 is a four-cylinder, two-stroke, horizontally-opposed, 1,042 cc (63.6 cu in) displacement, fan-forced air-cooled, petrol engine design, with a mechanical gearbox reduction drive with reduction ratios from 2.03 to 3.79:1. It employs dual capacitor discharge ignition and produces 83 hp (62 kW) at 6000 rpm.[1]
Specifications (Hirth 3002 E)
Data from Tacke[1]
General characteristics
- Type: Four cylinder, two stroke aircraft engine
- Bore: 72 mm (2.8 in)
- Stroke: 64 mm (2.5 in)
- Displacement: 1,042 cc (63.6 cu in)
- Length: 380 mm (15.0 in)
- Width: 570 mm (22.4 in)
- Height: 338 mm (13.3 in)
- Dry weight: 42 kg (92.6 lb)
Components
- Fuel type: petrol
- Cooling system: fan-forced air
- Reduction gear: mechanical gearbox
Performance
- Power output: 83 hp (62 kW)
See also
Related lists