Walter Regulus

Regulus
Walter Regulus II
TypeRadial aero engine
National originCzechoslovakia
ManufacturerWalter Aircraft Engines
First run1934

The Walter Regulus was a Czechoslovak five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp).

Engines on display

A preserved example of the Walter Regulus engine is on display at the following museum:

Specifications (Regulus)

Data from Jane's all the World's Aircraft 1931

General characteristics

Components

Performance

See also

Comparable engines

Related lists

References

  1. ↑ Gunston, Bill (1989). World encyclopaedia of aero engines (Fully rev. 2nd ed.). P. Stephens. p. 174. ISBN 1-85260-163-9.
  2. ↑ "ENGINES AT THE SHOW" (pdf). Flight. XXVI (1352): 1250–1255. 22 November 1934. Retrieved 26 December 2018.
  3. ↑ Grey, C.G., ed. (1931). Jane's all the World's Aircraft 1931. London: Sampson Low, Marston & company, ltd. p. 29d.