The Walter Venus was a seven-cylinder, air-cooled, radial engine for aircraft use built in Czechoslovakia in the late 1920s.
Applications
Specifications
Data from Flight.[1]
General characteristics
- Type: 7-cylinder radial engine
- Bore: 105 mm (4.1 in)
- Stroke: 120 mm (4.7 in)
- Dry weight: 178 kg (393 lb)
Components
- Valvetrain: Overhead valve, one inlet and one exhaust valve per cylinder
- Fuel system: Zenith Type 50J carburettor
- Fuel type: Petrol
- Oil system: Pressure and scavenge pump
- Cooling system: Air-cooled
- Reduction gear: Direct-drive
Performance
See also
- Related lists
References
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 168.
- Němeček, V. (1968). Československá letadla. Praha: Naše Vojsko.
- moraviation.com
|
---|
| General | |
---|
| Military | |
---|
| Accidents/incidents | |
---|
| Records | |
---|
|