Bristol Siddeley BS.605

1960s British aircraft rocket engine From Wikipedia, the free encyclopedia

The Bristol Siddeley BS.605 was a British take off assist rocket engine of the mid-1960s that used hydrogen peroxide and kerosene propellant.

National originUnited Kingdom
First run14 March 1965
Quick facts BS.605, Type ...
BS.605
BS.605 on display at the Royal Air Force Museum Cosford
TypeRATO rocket engine
National originUnited Kingdom
ManufacturerBristol Siddeley
First run14 March 1965
Major applicationsBlackburn Buccaneer
Developed fromArmstrong Siddeley Stentor
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Design and development

The BS.605 design was based on the smaller of two combustion chambers of the earlier Armstrong Siddeley Stentor. A pair of retractable BS.605 engines were fitted to Buccaneer S.50 strike aircraft of the South African Air Force for hot and high operations. The BS.605 was also considered for the Bluebird CMN-8, a design for a supersonic land speed record car, to be driven by Donald Campbell.[1]

Applications

Engines on display

Specifications

Working parts on display at the Midland Air Museum

Data from [citation needed]

General characteristics

  • Type: Rocket engine
  • Length: 42 in (1,067 mm)
  • Diameter: 12 in (305 mm)
  • Dry weight: 366 lb (166 kg)
  • Fuel: Hydrogen peroxide/Kerosene

Components

  • Pumps:

Performance

  • Thrust: 4,000 lbf (18 kN) for 30 seconds Rated at 8,000 lbf (35.6 kN) [3]
  • Burn time:

See also

References

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