Bristol Neptune

The Bristol Neptune was a seven-cylinder air-cooled radial engine developed in 1930. It had the same size cylinders as the earlier Mercury and Titan engines, 5.75 in (146 mm) x 6.5 in (165 mm) which gave a displacement of 1,182 cu in (19.3 L) and produced a maximum of 320 horsepower (239 kW). The Neptune was effectively a seven-cylinder version of the Titan.[1]

Neptune
The Bristol Neptune
Type Radial aircraft engine
Manufacturer Bristol Aeroplane Company
First run 1930
Major applications Bristol Type 110
Developed from Bristol Titan

Applications

Specifications (Neptune I)

Data from Lumsden. [1]

General characteristics

Components

Performance

See also

Related development

Comparable engines

Related lists

References

Notes

  1. Lumsden 2003, p.103.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
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