A system level design and analysis has been conducted on an Earth Observation Satellite (EOS) system using the Interactive Design and Evaluation of Advanced Spacecraft (IDEAS) computer-aided design and analysis program. The IDEAS program consists of about 40 user-friendly technical modules and an interactive graphics display. The reflector support system and feed mast of the EOS spacecraft are constructed with box-truss structural concept, a lattice configuration which can be packaged for delivery in a single Shuttle flight and deployed in orbit. The deployed spacecraft consists of a 120-m by 60-m parabolic focal axis. The spacecraft was modeled for structural, thermal, and control systems analysis and structural elements were designed. On-orbit dynamic and thermal loading analyses were conducted; spacecraft weights and developmental and first unit costs were determined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Interactive analysis of a large aperture Earth observations satellite


    Beteiligte:
    Wright, R. L. (Autor:in) / Deryder, D. D. (Autor:in) / Ferebee, M. J., Jr. (Autor:in) / Smith, J. C. (Autor:in)

    Erscheinungsdatum :

    1983-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Interactive Analysis of a Large Aperture Earth Observations Satellite

    R. L. Wright / D. D. Deryder / M. J. Ferebee et al. | NTIS | 1983


    Interactive analysis of a large aperture Earth Observations Satellite

    Wright, R. L. / Deryder, D. D. / Ferebee, M. J., Jr. et al. | NTRS | 1983


    Japanese Earth Resources Satellite-1 synthetic aperture radar

    Nemoto, Y. / Nishino, H. / Ono, M. et al. | Tema Archiv | 1991


    Earth sensing with large aperture radiometers

    Wilson, W.J. | Tema Archiv | 1991


    Communication satellite systems using large aperture phased arrays

    LANGSETH, R. / REUDINK, D. / YEH, Y. | AIAA | 1974