Euclid An ESA mission to map the Dark Universe Andy Taylor Institute for Astronomy, Edinburgh 1 ESA Cosmic Vision proposal imaging & photometric survey spectroscopic survey Euclid All sky imaging, photometric & spectroscopic survey ESA M-class mission in assessment phase 600Meuro = 450Meuro (ESA)+150Meuro(agencies) 2 Euclid Goals Science Case: • • • • Dark Energy Dark Gravity Dark Matter Initial Conditions 3 Dark Energy Dark Energy characterized by an Equation of State: P = wρ c 75% of energy budget. 2 w = -1/3 (string/curvature) w = -1 Λ Scale factor, a w = 0 (CDM) a∝t 2 / 3(1+ w ) t If w = -1 energy-density is Einstein’s Cosmological Constant, Λ. 4 Dark Energy/Dark Gravity • Big Questions: • Is Dark Energy Λ? – Fine-tuning problem: ρV ≈ 10 – Coincidence problem: ρV ≈ ρ m −120 m 4 pl • Parameterize by PV = [ w0 + wa (1 − a )]ρV 5 Dark Energy: w0-wa constraints SN+CMB Euclid: Lensing BAO (Open models) Evolution of w: z w( z ) = w0 + wa 1+ z CMB Planck Flat (k=0) models 6 • Primary probes – Weak Lensing (WL) – Baryonic oscillations (BAO) Massey et al. Nature 445 (2007) Euclid Cosmological probes – Galaxy clustering – Redshift space distorsions – Cluster counts – Int. Sachs-Wolfe (cc CMB) Euclid collaboration 2008 • Secondary probes 7 Weak Lensing • Shape of background galaxies distorted by foreground DM • Cosmic shear is ~ 1%. Must be measured to high accuracy Background sources Dark matter halos Observer 8 Weak Lensing • Space: space – small and stable PSF ⇒ larger number of resolved galaxies ⇒ reduced systematics ground 9 + Distances (Redshifts): 3D WL • Distances for 109 galaxies from redshifted colours. − optical colours possible with ground-based survey (e.g. PS1+2). • Need Infra-Red (IR) colours from space for high accuracy. OPTICAL + IR OPTICAL zphoto zphoto ztrue ztrue Abdalla et al 2007 (UCL) 10 Baryonic Acoustic Oscillations • Signature of acoustic oscillations seen in CMB • Typical size 150Mpc now • Need large volume Space: – Large sky coverage – Access to IR Æ deeper ⇒ larger number of galaxies ⇒ 3D spectroscopic information 11 Euclid Cosmological goals • Measure Equation of state with ~1% on w0 and ~10% on wa. • Nature of Dark Matter • Initial conditions (Inflation) • Test of General Relativity • Evolution of galaxies • Clusters physics 12 Dark Matter • 3-D mass mapping: – Goal: All-sky, high-resolution maps & fly-through. • WDM: – X-sections & mass. • Neutrino’s: – mν, Nν, ∆mν • CDM: – Substructure – high resolution – Particle Physics constraints: axions, neutralino’s? • Intrinsic Alignments: – Halo model, simulations 13 Initial Conditions • Inflationary Perturbation Parameters: – – – – – – As Scalar perturbation amplitude ns Scalar spectral index α Scalar spectral index running r Tensor-to-Scalar ratio fNL Non-Gaussianity AISO Isocurvature perturbation modes 14 Combination of Probes • WL • BAO: • P(k): • z-distortions: • ISW: • Clusters: + CMB • Covariances between Probes? • Consistency tests? 15 Euclid: all sky survey Wide Extragalactic 20,000 deg2 Galactic Plane Deep ~50 deg2 16 Legacy • Visible/NIR imaging survey: – Morphologies and colors for billions of galaxies out to z~2, 3D Dark Matter maps • Spectroscopic survey: – 3D maps of the luminous matter distribution, spectra of 200 million galaxies out to z~2 • Deep survey: – Infrared imaging to H(AB)=26 and spectroscopy to H(AB)=24: galaxies 2<z<7, Objects 7<z<10 color selected from YJH (Impossible from ground) • Galactic survey: – Milky way 17 Mission & Payload • Soyuz launcher from Kourou (French Guiana). • L2 orbit • 5 year mission • Telescope 3 mirrors with 1.2m primary • Data rate Max 700Gb/day (compressed) • Stop and stare. 18 3 Instruments Visible Imaging channel: Æ galaxy shapes • 36 CCD detectors – AOCS (4 ccd) – 0.5 deg2 – 0.10’’ pixels, 0.21’’ PSF FWHM – 4096 red pixels / CCD • broad band R+I+Z (0.55-0.92µm) 19 3 Instruments NIR Photometry channel: Æ photo-z’s • HgCdTe detectors • 16 arrays – 0.5 deg2 – 0.3’’ pixels ~ PSF – 2048x2048 pix / array • 3 bands Y,J,H (1.0-1.7µm) 20 3 Instruments NIR Spectro channel: Æ redshifts of 1/3 of galaxies • Slitless spectroscopy • Investigating: Digital Micro-mirror Devices (DMD) based multi-object slit • 0.5 deg2 • 0.9-1.7µm 21 Data Handling Challenges • Galaxy surveys: – Need to measure shape of 3 billion galaxies (see Tom Kitching’s talk). – Measure spectra of 1 billion galaxies. • Data flow: – – – – 700Gb/day (compressed) 250Tb/year 1.3 Pb total (c.f Pan-STARRS-1) Based on Astrowise & PS1 IPP. 22 Level 1: Telemetry Euclid Raw data House-keeping Euclid 2A: Raw data processing Flat fielding Dark subtraction CTE correction Pipeline Level 2A 2B: Catalogue Production Aperture Photometry Astrometry PSF characterization Source extraction Star-galaxy separation Shape/shear measurement Photo-z’s Level 2B Level S Simulations 3: Science Analysis 3-D dark matter maps 3-D cosmic shear Shear ratios Intrinsic Alignments Cosmological Parameters Level 3 Level 4 4: Data Archive/VO 23 Data Analysis Challenges • Peta-Bytes of data to push through pipeline. • 6 layers: 1. 2. 3. 4. 5. 6. • Data acquisition, book keeping, data compression Raw Data Reduction Shape analysis (see Tom Kitchings talk) Science analysis (map making, power spectra, etc) Data Archiving Simulations How do we simulate large dynamic range? – – And Monte-Carlo surveys ~1000 times? c.f. CMB temperature & polarisation experiments (i.e QUaD analysis). 24 Simulating Euclid Surveys • Do we need ensembles of LCDM Millennium simulations to test methods, estimate covariance and understand systematics? • Develop Dark Energy/Gravity simulations. (Kiessling et al 2009) • Do we need a Millennium Simulation at each point in parameter space? Simulated all-sky convergence at z =1 (Teyssier et al 2008) 25 Simulations Challenge • How do we get from here to Peta-scale simulations? • Joint DUEL and Astrosim initiative to explore a pathway to peta-scale sims for Euclid in Zurich later this year (ANT, A. Amara, R. Teyssier). • Engage computing & simulation community and European theorists to support mission. 26 ESA/NASA IDECS Negotiations • ESA and NASA worried about: – costs (M-class mission) – NASA/DOE JDEM (eg Planck vs WMAP). • • 6th Jan 2009 start of discussions April 2009 – discussions on hold. • Options: 1. 2. 3. ESA Euclid for WL and BAOs Joint ESA/NASA/DOE IDECS for WL & BAOs ESA DUNE WL only and NASA Adept BAO only. 27 Summary • • • • • • Euclid launch: 2017. 5 year mission 1.4 Pb of data 3 billion galaxies over 3π to z=1 3 Instruments: Vis, NIP, NIS Methods: WL + BAO (+ secondary and legacy). • Science goals: Dark energy, dark matter, initial conditions, modified gravity. • Computing challenges: data compression, data reduction, shape analysis, power spectra & parameters, data archiving, simulations. 28 End 29