Karsten Danzmann- Gavitational Wave Space Missions

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    Gavitational WaveSpace Missions

    Karsten Danzmann

    Albert Einstein Institute Hannover

    LIGO-G070743-00-Z

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    Quantum Fluctuations in the Early Universe

    Merging super-massiveblack holes (SMBH) atgalactic cores

    Phasetransitionsin theEarly

    Universe

    Captureof blackholes andcompact

    stars bySMBH

    Mergingbinaryneutronstars and

    blackholes indistantgalaxies

    Neutronstarquakesandmagnetars

    Gravitational Wave Spectrum

    ASTROD DECIGO

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    A Collaborative NASA/ESA Mission

    Cluster of 3 S/C in heliocentric orbit

    Laser interferometer measures distance changesbetween free flying test masses inside the S/C

    Equilateral triangle

    with 5 million km arms

    Trailing the Earth by

    20 (50 million km)

    Inclined against

    ecliptic by 60

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    Cosmic backgrounds,superstring bursts?

    Massive Black Hole Binary (BHB)

    inspiral and merger

    Ultra-compact binaries

    Extreme Mass RatioInspiral (EMRI)

    LISA: A Universe Full ofStrong GW Sources

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    Absolute Distances from SMBH Mergers:

    Hubble Constant and Dark Energy

    100s of events expected to z~3 ~10s to z~20

    Cosmological distance requiresredshift via identification of host

    Noise from weak lensing Comparable precision to CMB, WL,BAO, CL, SN techniques

    Absolute & independentmeasurement

    100 BHB, 3000 SNIa (Dalal et al

    0601275), includes lensing noise

    H0and Dark Energy parameterspotentially measured to

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    LISA layout

    Laser transponder with 6 links, all transmitted to ground

    Diffraction widens the laser beamto many kilometers

    1 W sent, still 100 pW receivedby 40 cm Cassegrain

    Michelson with 3rd armand Sagnac mode

    Can distinguish bothpolarizations of a GW

    Can form Null combination!main transponded

    laser beams

    reference

    laser beams

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    NRC Beyond

    Einstein Review

    November 6-8, 2006Washington

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    BEPAC Recommendations for LISA

    "On purely scientific grounds LISA is the mission that is most promisingand least scientifically risky. Even with pessimistic assumptions aboutevent rates, it should provide unambiguous and clean tests of the theoryof general relativity in the strong field dynamical regime and be able tomake detailed maps of space time near black holes. Thus, the

    committee gave LISA its highest scientific ranking."

    " LISA is an extraordinarily original and technically bold mission concept.LISA will open up an entirely new way of observing the universe, withimmense potential to enlarge our understanding of physics and astronomyin unforeseen ways. LISA, in the committees view, should be theflagship missionof a long-term program addressing Beyond Einsteingoals."

    "NASA should invest additional Beyond Einstein funds in LISAtechnology development and risk reduction, to help ensure that theAgency is in a position to proceed in partnership with ESA to a new startafter the LISA Pathfinder results are understood."

    LISA was recommended second in implementation because of moneyand programmatics. But even assuming an unnecessarily pessimisticfinancial contribution from ESA, and being second in Beyond Einstein, the

    assumed launch date of LISA as ESA Cosmic Vision Mission L1 in2018 is still feasible and the committee strongly recommends that.

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    LISA Status

    ESA-NASA collaboration agreement since August 2004

    Joint Management Structure working well!

    Mission Formulation Study began in January 2005

    Technology precursor LISA Pathfinder in Phase C/D

    Launch in 2010

    LISA technically well on track for launch in 2015!

    Launch date is determined by budget

    ESA SPC Meeting 22 Feb 2007: LISA L1 launch in 2018!

    NASA Beyond Einstein Review: Report released September 6, 2007

    LISA is Flagship mission! Schedule compatible with ESA!

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    0.1m 10m 1 Hz 100 10k

    4x107 4x105 4x103 M 40 0.4frequency

    f/ binary black hole mass whose freq at merger=

    f

    Current detectors

    BBO3rd generation

    Adv detectors

    LISA

    10-22

    10-23

    10-24

    10-25

    5/(yr Hz) | 1/Hz

    ASTROD

    Adapted from Sathya

    DECIGO

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    ASTROD Mission Concept

    Sun

    Inner Orbit

    Earth Orbit

    Outer OrbitLaunch Position

    .Earth (800 days after launch)

    L1 point

    Laser Ranging

    S/C 2

    S/C 1

    from W T Ni

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    ASTROD technological

    requirements Weak-light phase locking to 100 fW.

    Heterodyne interferometry and data analysis for unequal-

    arm interferometry. Coronagraph design and development: sunlight in the

    photodetectors should be less than 1 % of the laser light.

    High precision space clock and/or absolute stabilized laserto 10-17.

    Drag-free system. Accelerometer noise requirement: (0.3-1)10-15[1+10(/3mHz)2] ms-2Hz-1/2 at 0.1 mHz