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Armstrong Siddeley Viper

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Viper
Preserved Rolls-Royce Viper Turbojet
Type Turbojet
Manufacturer Armstrong Siddeley
Rolls-Royce Limited
First run April Template:Avyear
Major applications BAC Jet Provost
Hawker Siddeley Dominie
Developed from Armstrong Siddeley Adder

The Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol-Siddeley and Rolls-Royce Limited. It entered service in 1953 and remains in use with the Royal Air Force, powering its Dominie T1 navigation training aircraft.[1]

Design and development

The design originally featured a seven-stage compressor based on their Sapphire engine — the Viper is in effect a small scale Sapphire.

The Viper was developed as an expendable engine for powering a target drone, the Jindivik,[2] but the limited-life materials used were subsequently replaced with standard ones.

Engines on display

Preserved Viper engines are on public display at the:

Applications

Specifications (Viper ASV.12)

Data from [3]

General characteristics

  • Type: Turbojet
  • Length: 64.0 in (1625 mm)
  • Diameter: 24.55 in (966 mm)
  • Dry weight: 549 lb (249 kg)

Components

  • Compressor: Seven stage axial
  • Combustors: Annular, 24 burners
  • Turbine: Single stage
  • Fuel type: AVTUR, AVTAG
  • Oil system: scavenge, metered

Performance

See also

Related development

Comparable engines

Related lists

References

Notes

  1. ^ Dominie T1 www.raf.mod.uk. Retrieved: 14 October 2009
  2. ^ Gunston 1989, p.20.
  3. ^ Flight Global Archive - 1955 Retrieved: 3 November 2008

Bibliography

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