An in-depth study and selection of practical propellant surface tension acquisition system designs for two specific future cryogenic space vehicles, an advanced cryogenic space shuttle auxiliary propulsion system and an advanced space propulsion module is reported. A supporting laboratory scale experimental program was also conducted to provide design information critical to concept finalization and selection. Designs using localized pressure isolated surface tension screen devices were selected for each application and preliminary designs were generated. Based on these designs, large scale acquisition prototype hardware was designed and fabricated to be compatible with available NASA-MSFC feed system hardware.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study and design of cryogenic propellant acquisition systems. Volume 1: Design studies


    Beteiligte:
    Burge, G. W. (Autor:in) / Blackmon, J. B. (Autor:in)

    Erscheinungsdatum :

    1973-12-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Design of propellant acquisition systems for advanced cryogenic space propulsion systems

    Burge, G. W. / Blackmon, J. B. / Castle, J. N. | NTRS | 1973



    Cryogenic Propellant Management Device: Conceptual Design Study

    Wollen, Mark / Merino, Fred / Schuster, John et al. | NTRS | 2010