The Walter Regulus was a Czechoslovakian five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp).[1][2]
Regulus | |
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Walter Regulus II | |
Type | Radial aero engine |
National origin | Czechoslovakia |
Manufacturer | Walter Aircraft Engines |
First run | 1934 |
A preserved example of the Walter Regulus engine is on display at the following museum:
Data from Jane's all the World's Aircraft 1931[3]
Comparable engines
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License produced engines | |
Opposed engines |
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Inline engines | |
V-12 engines | |
Radial engines | |
Turbojets | |
Turboprops |