The Walter Vega was a five-cylinder, air-cooled, radial engine for aircraft use, built in Czechoslovakia in the late 1920s.
|Walter Vega, radial five-cylinder|
|Type||Radial aircraft engine|
|Manufacturer||Walter Aircraft Engines|
|Designed by||František Adolf Barvitius|
- Type: five-cylinder radial engine
- Bore: 105 mm (4.1 in)
- Stroke: 120 mm (4.7 in)
- Dry weight: 102.5 kg (226 lb)
- Designer: František Adolf Barvitius
- 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
|Wikimedia Commons has media related to Walter Vega.|
- Flight - 25 July 1929, p. 762. Retrieved: 29 May 2012
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 168.
- Němeček, Václav (1968). Československá letadla (1918-1945), pages 368, Praha: Naše vojsko.
- Walter Vega
- Foreign engines at Olympia (Flight 1929, July 25, p. 778)
- Polish PWS 8 biplane, with Walter "Vega" engine (Flight 1930, August 8, p. 888)