The Space Infrared Telescope Facility (SIRTF) is a cryogenically cooled, space based, one meter class telescope for infrared astronomy. A recent mission option study has moved SIRTF from a previous low earth orbit (900 km) shuttle launched design to a high earth orbit (100,000 km) Titan IV/Centaur launched design. The mission option study requirements and trades relating to the structural configuration and the chosen SIRTF design are described. Also discussed is a dynamic stress analysis of the new SIRTF baseline structural design which has been performed using finite element modeling and simulated launch interface loads.


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    Titel :

    SIRTF high earth orbit mission conceptual structural design and analysis


    Beteiligte:

    Kongress:

    Cryogenic Optical Systems and Instruments IV ; 1990 ; San Diego, CA, United States


    Erscheinungsdatum :

    1990-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    SIRTF in high earth orbit

    Werner, Michael W. / Brooks, Walter F. / Manning, Larry A. et al. | NTRS | 1989


    SIRTF in High Earth Orbit

    M. W. Werner / W. F. Brooks / L. A. Manning et al. | NTIS | 1989


    SIRTF mission design

    Garcia, M. / Bonfiglio, E. P. | NTRS | 2003


    The SIRTF mission

    Werner, M.W. / Bothwell, M. | Elsevier | 1993


    The SIRTF Mission

    Werner, M.W. | Online Contents | 1993