CNA D
From Wikipedia, the free encyclopedia
The CNA D, often known as the CNA D.4, was a four-cylinder, air-cooled, horizontally opposed engine built in Italy by Compagnia Nazionale Aeronautica (CNA) between 1940 and 1951 to power light aircraft.[1]
| D | |
|---|---|
| |
| CNA D.4 on display at Museo Nazionale Scienza e Tecnologia Leonardo da Vinci | |
| Type | 4-cylinder air-cooled horizontally opposed piston engine |
| National origin | Italy |
| Manufacturer | Compagnia Nazionale Aeronautica (CNA) |
Applications
Data from Erickson[1]
- Adam RA-14 Loisirs
- Ambrosini SAI.10
- CNA PM.1
- CNA MPL
- CVV Tartuca
- Druine Condor
- GCA Pedro
- GCA Etabeta
- Lombardi FL.3
- Lombardi FL.5
- Lombardi FL.7
- Macchi MB.308
- Viberti Muscal
Specifications
Data from [1]
General characteristics
- Type: 4-cyl. air-cooled horizontally-opposed piston engine
- Bore: 100 mm (3.9 in)
- Stroke: 95 mm (3.7 in)
- Displacement: 3 L (180 cu in)
- Dry weight: 80 kg (180 lb)
Performance
- Power output: 45 kW (60 hp) at 2,100 rpm
- Compression ratio: 5.3:1
- Specific fuel consumption: 0.34 kg/kW hr (0.56 lb/hp hr)[2]
See also
Related lists
References
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