Hirth F-40
The Hirth F-40 is a German aircraft engine, that was designed and produced by Hirth of Benningen for use in ultralight aircraft.[1]
| Hirth F-40 | |
|---|---|
| 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 F-40 is a four-cylinder, two-stroke, 1,300 cc (79.3 cu in) displacement, liquid-cooled, gasoline engine design, with a helical gear mechanical gearbox reduction drive. It produces 120 hp (89 kW) at 4800 rpm.[1]
Specifications (F-40)
Data from Tacke[1]
General characteristics
- Type: Four cylinder, two stroke aircraft engine
- Bore: 76 mm (3.0 in)
- Stroke: 69 mm (2.7 in)
- Displacement: 1,300 cc (79.3 cu in)
- Dry weight: 69 kg (152.1 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: helical gear mechanical gearbox
Performance
- Power output: 120 hp (89 kW)
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Hirth. "All Engines". www.hirth-engines.de. Retrieved 19 March 2018.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.