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 | |
|---|---|
| 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
Related lists
| |
|---|---|
| License produced engines | |
| Opposed engines |
|
| Inline engines | |
| V-12 engines | |
| Radial engines | |
| Turbojets | |
| Turboprops | |