Selection and design considerations of components for high performance turbopumps for aircraft or rocket engine applications; following conclusions reached: takeoff weight of rockets and missiles is directly effected by turbopump efficiency and required suction specific speed; turbine selection is governed by weight and efficiency; aircraft turbopumps are capable of operation at much higher speeds due to their shorter operating life. Bibliography.


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    Titel :

    High speed turbo pumps


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Boretz, J.E. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1956 Pumps



    Erscheinungsdatum :

    1956


    Format / Umfang :

    59 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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