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  • Satellite Test of the Special and General Relativity Theory: a Proposal

    Paper number

    IAC-13,A2,1,4,x20155

    Author

    Dr. Deborah Aguilera, DLR, German Aerospace Center, Germany

    Coauthor

    Dr. Thilo Schuldt, DLR, German Aerospace Center, Germany

    Coauthor

    Mr. Ruven Spannagel, DLR, German Aerospace Center, Germany

    Coauthor

    Mr. Alexander Milke, ZARM - University of Bremen, Germany

    Coauthor

    Dr. Norman Gürlebeck, ZARM - University of Bremen, Germany

    Coauthor

    Dr. Sven Herrmann, ZARM - University of Bremen, Germany

    Coauthor

    Dr. Claus Lämmerzahl, ZARM - University of Bremen, Germany

    Coauthor

    Dr. Bernd Biering, DLR, German Aerospace Center, Germany

    Coauthor

    Prof. Hansjörg Dittus, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Prof. Claus Braxmaier, ZARM - University of Bremen, Germany

    Year

    2013

    Abstract
    We propose a small satellite mission that aims for testing the foundations of special relativity. It will perform a Kennedy-Thorndike (KT) experiment, where a potential boost anisotropy of the velocity of light is measured by comparing a length reference (i.e. a highly stable optical resonator) with a molecular frequency reference. This experiment in space increases its sensitivity significantly (factor of $>$100) with respect to an equivalent terrestrial test. A sensitivity of 10$^{-18}$ in the measurement of the Kennedy-Thorndike coefficient is targeted.
    
    The experiment uses state-of-the-art laser technology. For realizing a small satellite compatible payload, the use of diode-laser technology is favorable and currently already under investigation with respect to other space experiments. A laser wavelength of 1030/1016nm is foreseen as its second harmonics accesses narrow linewidth transitions in molecular iodine.  For the KT experiment, one laser is stabilized to a high finesse cavity and a second laser is frequency doubled to a wavelength of 515/508nm and stabilized to a hyperfine transition in molecular iodine. Both lasers are directly compared in a beat measurement and analyzed with respect to a possible boost dependency of the speed of light. 
    
    In the last years, we realized an iodine-based frequency reference at a wavelength of 532nm on elegant breadboard (EBB) level where a frequency stability of 10$^{-15}$ at 1000s integration time was demonstrated in a beat measurement with a laboratory-type cavity setup. In a current activity the iodine frequency reference is further developed with respect to compactness and thermal and mechanical stability. A compact iodine setup on engineering model (EM) level is currently developed. This setup uses a fused silica baseplate with dimensions of 18cm x 38cm x 4cm where the optical components are directly glued to. This setup uses a 10cm x 10cm iodine cell in nine-path configuration and will be subjected to environmental tests such as vibration and thermal cycling. 
    
    In a parallel activity, the development of a space compatible optical resonator setup with a finesse of 10$^5$ of the resonator and a controlled temperature stabilization of $\sim$1$\mu$K is planned.
    
    Techniques for laser frequency stabilization are key technologies not only for the proposed KT experiment mission but also for a variety of other future space missions such as LISA/NGO, GRACE-FO, and missions using aperture-synthesis such as Darwin/TPF.
    Abstract document

    IAC-13,A2,1,4,x20155.brief.pdf

    Manuscript document

    IAC-13,A2,1,4,x20155.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.