Three German Engine Fuel Systems

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 October 1943


BMW 801A/1 The engine is a radial, air‐cooled, fourteen‐cylindcr, double‐bank motor of 42 litres capacity, 6–5/1 compression ratio and 156 mm. bore and stroke.


(1943), "Three German Engine Fuel Systems", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 10, pp. 293-302.




Copyright © 1943, MCB UP Limited

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