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.

Design and development 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

See also

References