Walter Castor
The Walter Castor was a Czechoslovak seven-cylinder, air-cooled radial engine for powering aircraft that was developed in the late 1920s. The Super Castor was a nine-cylinder development. Castor I production began in 1928, Castor II in 1932 and the Castor III in 1934.
Applications
- Aero A.35
- Aero A.304
- Airspeed Envoy
- Breda Ba.25
- Dornier Do K
- Fizir F1V
- Hopfner HV-6/28
- Letov Š-28
- Rogozarski AZR
- Savoia-Marchetti S.71