The CPS is an in-space cryogenic propulsive stage based largely on state of the practice design for launch vehicle upper stages. However, unlike conventional propulsive stages, it also contains power generation and thermal control systems to limit the loss of liquid hydrogen and oxygen due to boil-off during extended in-space storage. The CPS provides the necessary (Delta)V for rapid transfer of in-space elements to their destinations or staging points (i.e., E-M L1). The CPS is designed around a block upgrade strategy to provide maximum mission/architecture flexibility. Block 1 CPS: Short duration flight times (hours), passive cryo fluid management. Block 2 CPS: Long duration flight times (days/weeks/months), active and passive cryo fluid management.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Cryogenic Propulsion Stage


    Beteiligte:
    Jones, David (Autor:in)

    Kongress:

    Cryogenic Propulsion Stage ; 2011 ; Huntsville, AL, United States


    Erscheinungsdatum :

    2011-08-05


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Cryogenic Propulsion Stage

    D. Jones | NTIS | 2011


    Nuclear Cryogenic Propulsion Stage

    M. G. Houts / T. Kim / W. J. Emrich et al. | NTIS | 2014


    Nuclear Cryogenic Propulsion Stage

    M. G. Houts / T. Kim / W. J. Emrich et al. | NTIS | 2014


    Nuclear Cryogenic Propulsion Stage

    M. G. Houts / T. Kim / W. J. Emrich et al. | NTIS | 2014


    Nuclear Cryogenic Propulsion Stage

    M. G. Houts / T. Kim / W. J. Emrich et al. | NTIS | 2014