Английская Википедия:Armstrong Siddeley Stentor

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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English

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]

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

Файл:Armstrong Siddeley Stentor RAFM Cosford.JPG
Cut-away Stentor on display at the Royal Air Force Museum Cosford

Шаблон:Rocketspecs

See also

Шаблон:Aircontent

References

Шаблон:Commons category Шаблон:Reflist

Шаблон:Armstrong Siddeley aeroengines Шаблон:Bristol aeroengines Шаблон:Rocket engines

  1. 1,0 1,1 Ошибка цитирования Неверный тег <ref>; для сносок Flight, 1960 не указан текст
  2. Шаблон:Cite book
  3. Шаблон:Cite web
  4. Шаблон:Cite journal
  5. Шаблон:Cite journal