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Armstrong Siddeley Motors Project design study (POR 62/2): P.172F Preliminary design...
Catalogue reference: PA1716/5/8/39
What’s it about?
This record is a file about the Armstrong Siddeley Motors Project design study (POR 62/2): P.172F Preliminary design... dating from September 1955.
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Full description and record details
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Reference (The unique identifier to the record described, used to order and refer to it)
- PA1716/5/8/39
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Title (The name of the record)
- Armstrong Siddeley Motors Project design study (POR 62/2): P.172F Preliminary design study of an axial-flow turbo-jet of 21,700 lb sea level static thrust
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Date (When the record was created)
- September 1955
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Description (What the record is about)
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Leading particulars and estimated performance of a lightweight axial-flow turbo-jet of 44' maximum diameter, designed for fighter application and operating up to M.2 above 36,000 feet. The seal level static thrust of the engine is 21,700 lb, with a DAMF of 264 lb per sec
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Held by (Who holds the record)
- Coventry Archives & Research Centre
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Former department reference (Former identifier given by the originating creator)
- Project design/P.172F
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Language (The language of the record)
- English
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Physical description (The amount and form of the record)
- 1 Item
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/b51832d0-8cad-478c-94da-4c661aadd656/
Catalogue hierarchy
This record is held at Coventry Archives & Research Centre
Within the fonds: PA1716
Rolls-Royce Heritage Trust, Coventry Branch - Records of Armstrong Siddeley, Bristol...
Within the sub-fonds: PA1716/5
Armstrong Siddeley/Bristol Siddeley & Rolls-Royce Gas Turbines
Within the sub-sub-fonds: PA1716/5/8
Armstrong Siddeley Motors, Bristol Siddeley, Rolls-Royce Project Design Study
You are currently looking at the file: PA1716/5/8/39
Armstrong Siddeley Motors Project design study (POR 62/2): P.172F Preliminary design study of an axial-flow turbo-jet of 21,700 lb sea level static thrust