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    ESA > Our Activities > Human Spaceflight > Human Spaceflight Research

    Scientific Objectives

    ACES will conduct the first experiments with cold atoms under microgravity conditions equivalent to a freely falling laboratory; it will perform fundamental physics tests to high resolution, and develop applications in different areas of research.

    Scientific objectives

    The scientific objectives of the ACES mission are:

    • To demonstrate the performances of a new generation of space clocks
    • To achieve time and frequency transfer with stability better than 10-16
    • To perform fundamental physics tests

    The combination of PHARAO and SHM will define an on-board frequency reference whose fluctuations are expected to be below 10 ps per day. The ISS orbit will allow ground users to compare their own clock to the ultra-stable frequency reference provided by ACES. The results of these comparisons will provide new tests of fundamental laws of physics such as an improved measurement of the Einstein’s gravitational red-shift, a search for anisotropies of the speed of light, and a search for space-time variations of fundamental physical constants.


    ACES Mission Objectives

    Test of a new generation of space clocks
    Cold atoms physics microgravity Such studies will be essential for the development of atomic quantum sensors for space apllications (atomic clocks, atom interferometers, sensors based on quantum gases)
    PHARAO frequency stability and accuracy PHARAO performance: frequency instability better than 1•10-13•t-1/2 for 1s ‹t ‹10day, where t is the integration time expressed in s; frequency inaccuracy at the 10-16 level.
    SHM frequency stability SHM performance: frequency instability better than 1.5•10-13 at 1 s, 2.1•10-14 at 10 s, 5.1•10-15 at 100 s, 2.1•10-15 at 1000 s, and 1.5•10-15 at 10000 s of integration time.
    Stable and accurate time and frequency transfer via the ACES MWL
    Space-to-ground time and frequency transfer Time transfer stability better than 0.4 ps over one ISS pass, 8 ps after 1 day, and 25 ps after 10 days.
    Comparison of ground clocks Common view comparisons to an uncertainty level below 1 ps per ISS pass. Non-common view comparisons to an uncertainty level of 3 ps and 10 ps for space-to-ground comparisons separated by a dead time delta t of 1000 s and 10000 s respectively.
    Ground Clocks synchronization Absolute synchronization of ground clock time scales with an uncertainty of 100 ps.
    Contribution to atomic time scales Contribution to TAI and comparison of primary frequency standards with accuracy at the 10-16 level.
    Distribution of the ACES time scale Distribution to ground users of an atomic time scale with time accuracy at the 100 ps level.
    Fundamental physics tests
    Measurement of the gravitational red-shift Precision measurement of the Einstein’s gravitational red-shift to an uncertainty level of 2•10-6.
    Time variations of fundamental constants Search for time variations of the fine structure constant α at an uncertainty level of α-1•δα/δt ‹1•10-16 year-1 after 1 year, down to 3•10-17 after 3 years of mission duration.
    Search for Lorentz transformation violations and SME tests Search for anisotropies of the speed of light at the δc/c ‹1•10-10 uncertainty level.

    Conclusion

    The measurement of time has experienced spectacular progress over the last centuries and ACES will provide the next leap forward. Time really does fly on the International Space Station.

    ACES Scientific Applications

    Relativistic Geodesy Demonstration of a new technique for mapping the Earth gravitational potential with a resolution better than 1 m based on measurements of the differential gravitational red-shift between clocks on ground.
    Clock comparison and time transfer via ELT
    • Space-to-ground comparison of clocks via ELT to a time deviation better than 6 ps at 100 s of integration time, 4 ps between 300 s and 104 s, 7 ps between 105 s and 106 s.
    • Common view comparisons of ground clocks by laser link with time stability, expressed in time deviation, better than 6 ps after an ISS pass (~300 s of integration time).
    • Non-common view comparisons of ground clocks via laser link with a time stability, expressed in time deviation, better than 6 ps after 1000 s, 6 ps after 2000 s, 7 ps after 104 s of dead time.
    • Synchronization of ground clocks to a time accuracy of 50 ps (25 ps as target accuracy) via laser link.
    • Distribution of the ACES time scale to ground users with a time accuracy of 50 ps (25 ps as target accuracy) via laser link.
    Optical ranging via ELT
    • Laser ranging performance at the centimetre level for single shot, corresponding to a one-way time uncertainty of 50 ps (25 ps as target one-way time uncertainty per shot).
    • Calibration of the ACES MWL for ranging measurements with respect to ELT and comparisons of different ranging techniques: one-way optical ranging, two-way optical ranging, microwave ranging.
    • Study of troposphere and ionosphere biases by direct comparison of ranges both in the optical and microwave domain.
    GNSS applications
    • Support the comparison of the on-board ACES clocks with ground clocks via the GNSS network.
    • Support GNSS radio-occultation measurements.
    • Support GNSS reflectometry measurements.

    Conclusion

    The measurement of time has experienced spectacular progress over the last centuries and ACES will provide the next leap forward. Time really does fly on the International Space Station.

    Last update: 3 November 2011

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    • Related links
      • Atomic Clock Ensemble in Space (ACES)
        • ACES Payload
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            • ACES Time and Frequency Links
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