Sunbeam Spartan

Spartan
TypeV-12 air-cooled piston engine
National originBritain
ManufacturerSunbeam
Designer
Major applicationsSaunders T.1
Manufactured1917
Number builtprototypes only

The Sunbeam Spartan was a British 12-cylinder aero-engine designed and built in 1916.

Design and development

Louis Coatalen concentrated on water-cooled engines for the most part, but did design an air-cooled V-12 named Spartan. Little is known of this engine which had a bore of 105 mm (4 in) and stroke of 130 mm (5 in), capacity of 14.03 L (856 cu in) and output of 149 kW (200 hp) driving a propeller through a reduction gearbox. The single overhead camshaft operated two inlet and two exhaust valves per cylinder via rockers, and ignition was supplied by two 6-cyl. magnetos supplying spark to one spark plug per cylinder.


Specifications (Spartan)

Data from Sunbeam Aero-Engines

General characteristics

Components

Performance

See also

Comparable engines

Related lists

References

  1. 1 2 3 4 5 6 7 Brew, Alec (1998). Sunbeam Aero-engines. Shrewsbury: Airlife Publishing. ISBN 1-84037-023-8.

Bibliography