Electrical power for Space Station Freedom will be generated by large photovoltaic arrays with a beginning of life power requirement of 30.8 kW per array. The solar arrays will operate in a Low Earth Orbit (LEO) over a design life of fifteen years. This paper provides an analysis of the predicted solar array electrical performance over the design life and presents a summary of supporting analysis and test data for the assigned model parameters and performance loss factors. Each model parameter and loss factor is assessed based upon program requirements, component analysis and test data to date. A description of the LMSC performance model future test plans and predicted performance ranges are also given.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Solar array electrical performance assessment for Space Station Freedom


    Beteiligte:
    Smith, Bryan K. (Autor:in) / Brisco, Holly (Autor:in)

    Kongress:

    AIAA, AHS, and ASEE, Aerospace Design Conference ; 1993 ; Irvine, CA, United States


    Erscheinungsdatum :

    01.02.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space Station Freedom Solar Array Design

    Winslow | Online Contents | 1993



    Space Station Freedom Solar Array Design Development

    Winslow, Cindy | SAE Technical Papers | 1992


    Space Station Freedom solar array design development

    Winslow, C. / Bilger, K. / Baraona, C. | Tema Archiv | 1989


    Space Station Freedom Solar Array Tension Mechanism Development

    Allmon, C. / Haugen, B. / United States; National Aeronautics and Space Administration et al. | British Library Conference Proceedings | 1994