File
Armstrong Siddeley Motors Project design Office (POR 70/3): P.176 Mk.5 A supersonic...
Catalogue reference: PA1716/5/8/42
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This record is a file about the Armstrong Siddeley Motors Project design Office (POR 70/3): P.176 Mk.5 A supersonic... dating from May 1957.
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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)
- PA1716/5/8/42
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Title (The name of the record)
- Armstrong Siddeley Motors Project design Office (POR 70/3): P.176 Mk.5 A supersonic axial-flow turbo-jet engine
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Date (When the record was created)
- May 1957
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Description (What the record is about)
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At the design point of M.2 at 60,000 feet, the thrust of the engine with a two dimensional 2 shock intake is 4,400 lb with DAMF of 115 lb per sec. At the sea level static rating (intake recovery factor 100% and turbine inlet temperature 1400K) the thrust is 17,000 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.176
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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/101863aa-913c-44ea-8e88-ef8d35c06700/
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
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Armstrong Siddeley Motors Project design Office (POR 70/3): P.176 Mk.5 A supersonic axial-flow turbo-jet engine