Concord supersonic transport will be powered by 4 Olympus 593 turbojet engines; Bristol Siddeley will provide turbojets; jet pipe; propulsive nozzles, reversers and silencers are SNECMA contribution; choice of optimum-cycle engine for supersonic aircraft is compromise; maximum thrust is required at takeoff, during transonic acceleration and when cruising; at same time low consumption is essential while cruising and during considerable time at subsonic speeds; development problems involved; Concord flight plan; problems raised by intake and exhaust system.


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    Title :

    Concord propulsion


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 85 , n 2876


    Publication date :

    1964


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Concord Progress

    Edwards, George | Emerald Group Publishing | 1964


    Exit Concord Express

    Online Contents | 1994