Fuel Management for Concorde: A brief account of the fuel system and the fuel pumps developed for the aircraft
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 March 1971
Abstract
THE complete Concorde fuel system, part of which is described below, has been designed by the British Aircraft Corporation in conjunction with Aerospatiale of France. Plessey Dynamics Group's contribution has been to design and develop the several types of fuel pump to meet the very exacting requirements of the B.A.C. specifications.
Citation
Turner, H.G. (1971), "Fuel Management for Concorde: A brief account of the fuel system and the fuel pumps developed for the aircraft", Aircraft Engineering and Aerospace Technology, Vol. 43 No. 3, pp. 36-39. https://doi.org/10.1108/eb034746
Publisher
:MCB UP Ltd
Copyright © 1971, MCB UP Limited