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Armstrong Siddeley Motors Project design study (POR 63/1): P.173 Preliminary design...
Catalogue reference: PA1716/5/8/40
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This record is a file about the Armstrong Siddeley Motors Project design study (POR 63/1): P.173 Preliminary design... dating from October 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)
- PA1716/5/8/40
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Title (The name of the record)
- Armstrong Siddeley Motors Project design study (POR 63/1): P.173 Preliminary design study of an axial-flow turbo-jet of 25,200 lb sea level static thrust
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Date (When the record was created)
- October 1955
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Description (What the record is about)
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Leading particulars and estimated performance data of a lightweight axial-flow turbo-jet of 48' maximum diameter designed for fighter application and operation up to M.2 above 36,000 feet. The sea level static thrust of the engine is 25,200 lbs with a DAMF of 314 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.173
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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/bc7d8a98-642d-4811-a92f-c3e24c35165d/
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: PA1716/5/8/40
Armstrong Siddeley Motors Project design study (POR 63/1): P.173 Preliminary design study of an axial-flow turbo-jet of 25,200 lb sea level static thrust