An overview of the Starlight Mission is presented. Mission summary: June 2006 launch to heliocentric orbit; Nominal 6 month mission with option of additional 6 month extension; Validate autonomous formation flying system: range control to 10 cm bearing, control to 4 arcmin; Demonstrate formation flying optical interferometry.The original 3 spacecraft design did not fit the budget. 2 spacecraft concept demonstrates all key areas of formation flying interferometry. Collector flown on the surface of a virtual paraboloid, with combiner at the focus. It Gives a baseline of 125 m with a fixed delay of only 14 m.


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    Titel :

    An Overview of the StarLight Mission


    Beteiligte:
    Lay, Oliver (Autor:in) / Blackwood, Gary (Autor:in) / Dubovitsky, Serge (Autor:in) / Duren, Riley (Autor:in)


    Erscheinungsdatum :

    2004-04-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Overview of the StarLight Mission

    O. Lay / G. Blackwood / S. Dubovitsky et al. | NTIS | 2004



    Autonomous formation flying sensor for the Starlight Mission

    Purcell, G. / Young, L. / Vozoff, M. et al. | NTRS | 2001


    Description of the StarLight mission and spacecraft concept

    Deininger, W.D. / Weiss, M.A. / Wiemer, D.J. et al. | IEEE | 2001


    Preliminary stray light analysis for the StarLight Mission

    Noecker, C. / Fleming, J. / Gorham, P. | IEEE | 2001