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The Helioseismic & Magnetic Imager on the Solar Dynamics Observatory J. T. Hoeksema for The HMI Team – Stanford University, LMSAL, HAO, ++ 1.B – Solar Dynamo ABSTRACT 1.J – Sunspot Dynamics Investigators using the Helioseismic and Magnetic Imager (HMI) will study the origin of solar variability and will characterize and understand the interior of the Sun and the various components of magnetic activity. HMI is part of the Solar Dynamics Observatory (SDO) a satellite scheduled for launch into geosynchronous orbit in 2009. SDO is NASA’s first Living With a Star (LWS) mission. HMI will measurement motions of the solar photosphere to study solar oscillations and will measure polarization to study the vector magnetic field. HMI will help establish the relationships between the internal dynamics and magnetic activity in order to understand solar variability and its effects. The prime goal of the mission is to develop the knowledge needed for a reliable predictive capability, one of the key elements of the International Living With a Star (ILWS) program. 1.C – Global Circulation 1.I – Magnetic Connectivity 1.A – Interior Structure 1.D – Irradiance Sources The Michelson Doppler Imager (MDI) instrument on SOHO has been making helioseismic and magnetic field observations of the Sun since the beginning of Solar Cycle 23. HMI will continue these important measurements from space into the next solar cycle. The HMI instrument is an evolution of the successful MDI design with key improvements in resolution, image cadence, continuity, and vector magnetic field measurement capabilities. Filtergrams of the Fe I spectral line at 617.3 nm made with the HMI tunable narrow band filter system determine motions of the solar photosphere to study solar oscillations. Polarization measurements in this same spectral line enable determination of all three components of the photospheric magnetic field. 1.E – Coronal Magnetic Field 1.H – Far-side Imaging 1.F – Solar Subsurface Weather 1.G – Magnetic Stresses The web site hmi.stanford.edu provides more information. HMI Principal Optics Package Components Fold Mirror Assembly BDS Beam-splitter Assembly Focal Plane Assembly Michelson Interferometer ISS Beam-splitter Assembly 1.A 1.B 1.C 1.D 1.E 1.F 1.G 1.H 1.I 1.J Alignment Mechanism Limb Sensor Assembly Filter Oven Assembly ISS Pre-Amp Electronics Box Lyot Filter Assembly Camera Electronics Box Oven Controller E-Box Telescope Assembly Focus Mechanism Primary Lens Assembly ISS Mirror Assembly Front Window Assembly Hollow Core Motors Front Door Assembly Sound speed variations relative to a standard solar model. Solar cycle variations in the sub-photospheric rotation rate. Solar meridional circulation and differential rotation. Sunspots and plage contribute to solar irradiance variation. MHD model of the magnetic structure of the corona. Synoptic map of the subsurface flows at a depth of 7 Mm. EIT image and magnetic field lines computed from the photospheric field. A ctive regions on the far side of the sun detected with helioseismology. Vector field image showing the magnetic connectivity in sunspots. Sound speed variations and flows in an emerging active region. Secondary Lens Assembly Structure HMI Observables Doppler Velocity Z Optical Characteristics: Effective Focal Length: 495 cm Telescope Clear Aperture: 14 cm Cadence X Y Mechanical Characteristics: Box: 0.84 × 0.55 × 0.16 m Over All: 1.19 × 0.83 × 0.30 m Mass: 44.0 kg First Mode: 73 Hz Vector Magnetic Field 45 s Precision 13 m/s Zero point accuracy 0.05 m/s Dynamic range ±6.5 km/s Line-of-Sight Magnetic Flux Cadence 45 s Precision 10 G Zero point accuracy 0.05 G Dynamic range ± 4 kG Continuum Intensity Cadence 45 s Precision 0.3% Accuracy pixel to pixel HMI Sun-Test Data Products 0.1% Cadence Precision: Polarization Sunspots (1kG<|B|<4kG) * |B| Azimuth Inclination Quiet Sun (0.1kG<|B|<2kG) * |B| Total flux density Azimuth Inclination 90 s 0.22% 18G 0.6º 1.4º 220 G 35 G 15º 18º * See Figure C.12 for details First Dopplergram First Magnetogram