Catalogue description 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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Details of PA1716/5/8/40
Reference: PA1716/5/8/40
Title: 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
Description:

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
Date: October 1955
Held by: Coventry Archives, not available at The National Archives
Former reference in its original department: Project design/P.173
Language: English
Physical description: 1 Item

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