Walter Castor

Castor
Walter Castor III
Type	Radial aero engine
National origin	Czechoslovakia
Manufacturer	Walter Aircraft Engines
First run	1929

The Walter Castor was a Czechoslovakian seven-cylinder, air-cooled radial engine for powering aircraft that was developed in the late 1920s. The Super Castor was a nine-cylinder development.^[1]

Applications

• Aero A.35
• Aero A.304 (Super Castor)
• Airspeed Envoy
• Breda Ba.25
• Dornier Do K
• Fizir F1V
• Hopfner HV-6/28
• Letov Š-28
• Rogozarski AZR
• Savoia-Marchetti S.71

Engines on display

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

• Prague Aviation Museum, Kbely

Specifications (Castor)

Data from Flight.^[2]

General characteristics

• Type: 7-cylinder radial piston engine
• Bore: 135 mm (5.3 in)
• Stroke: 170 mm (6.7 in)
• Dry weight: 248 kg (547 lb)

Components

• Valvetrain: One intake and one exhaust valve per cylinder
• Fuel system: Zenith carburettor
• Fuel type: Petrol
• Cooling system: Air-cooled

Performance

• Power output: 194 kW (260 hp) at 1,850 rpm (maximum power)
• Compression ratio: 6:1
• Power-to-weight ratio: 0.78 kW/kg (0.48 hp/lb)

See also

Comparable engines

• Armstrong Siddeley Lynx

Related lists

• List of aircraft engines

References

Notes

1. Gunston 1989, p. 174.
2. Flight - The Walter Castor - 14 February 1929 Retrieved: 19 October 2010

Bibliography

• Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9