Catalogue description 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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Details of PA1716/5/8/39
Reference: PA1716/5/8/39
Title: 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
Description:

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
Date: September 1955
Held by: Coventry Archives, not available at The National Archives
Former reference in its original department: Project design/P.172F
Language: English
Physical description: 1 Item

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