A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being designed that will meet the performance requirements of a three-stage shrouded pump. Benefits of the new pump include lower manufacturing costs, reduced weight, and increased payload to orbit.


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    Titel :

    High Head Unshrouded Impeller Pump Stage Technology


    Beteiligte:
    R. W. Williams (Autor:in) / S. E. Skelley (Autor:in) / E. T. Stewart (Autor:in) / A. R. Droege (Autor:in) / G. H. Prueger (Autor:in)

    Erscheinungsdatum :

    2000


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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