The Armstrong Siddeley Stentor, latterly Bristol Siddeley BSSt.1 Stentor, was a two-chamber HTP rocket engine used to power the Blue Steel stand-off missile carried by Britain's V bomber force.[1][2] The high thrust chamber was used for the first 29 seconds, after which it was shut down and a smaller cruise chamber was used for the rest of the powered flight.[3][4][5]

Quick Facts Stentor, Type ...
Stentor
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Stentor rocket engine showing the large main nozzle (top) and the smaller cruise nozzle (bottom)
Type Rocket engine
National origin United Kingdom
Manufacturer Armstrong Siddeley
First run c.1960
Major applications Blue Steel missile
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Design and development

It was fuelled by hydrogen peroxide with kerosene.[1]

The engine incorporated an integral tubular mounting frame which was attached by six lugs to the rear bulkhead of the missile airframe, the complete engine being enclosed in a tube-shaped fairing with the nozzles at the rear.

Applications

Engines on display

Preserved Stentor engines are on display at the following museums:

Specifications

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Cut-away Stentor on display at the Royal Air Force Museum Cosford

Data from [6]

General characteristics

  • Type: two chamber liquid-propellant rocket engine
  • Length: 58 in (1,473 mm)
  • Diameter: 38 in (965 mm) wide, 44.5 in (1,130 mm) high
  • Dry weight: 747 lb (339 kg) including oil and nitrogen
  • Fuel: kerosene
  • Oxidiser: hydrogen peroxide

Components

  • Pumps:

Performance

See also

Related development

Related lists

References

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