This paper reviews the basic features of the Brayton cycle and discusses the selection of such cycle parameters as working fluid, pressure, and temperature. System performance, weight, and reliability characteristics are then considered in order to determine the suitability of this type of system for the intended space applications. It is shown that the Brayton cycle can be considered suitable for low-power solar and intermediate-power nuclear applications where low specific weight is not a critical requirement. To achieve the low specific weights required for electrical propulsion missions, turbine-inlet temperatures in the 3000 R region at power levels in the 500–1000 kw range appear to be necessary.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Brayton Cycle for Space Power


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1963




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Brayton cycle space power systems

    Pietsch, A. / Trimble, S.W. / Harper, A.D. | Tema Archiv | 1985


    Brayton Cycle Technology to Space Power

    Harty | Online Contents | 1994


    The Brayton Cycle for Space Power

    Warner L. Stewart / Arthur J. Glassman / Richard P. Krebs | NTRS | 1963


    Brayton Cycle Radioisotope Space Power System

    Schultz, R. L. / Melber, W. E. | SAE Technical Papers | 1964


    Brayton Cycle Conversion for Space Solar Power

    Komerath, Narayanan / Dessanti, Brendan | AIAA | 2012