Walter Mars I
The Walter Mars I was a nine-cylinder, air-cooled, radial engine for aircraft use built in Czechoslovakia in the late 1920s.The Mars I was the largest capacity design of a series of three similar radial engines developed by the Walter company. Common cylinders were used for the five-cylinder Walter Vega and the seven-cylinder Walter Venus, the Mars I being a nine-cylinder engine.Applications
- ANBO III
- Breda Ba.15
- DAR 4
- DAR 6
- Fizir FN
- Focke-Wulf A 33
- Letov Š-32
- SET 10
Specifications
