Solar Orbiter. Contents The mission The mission The orbit The orbit The instruments The instruments VIM: Visible-light Imager and Magnetograph VIM: Visible-light.

Slides:



Advertisements
Similar presentations
HMI Data Analysis Software Plan for Phase-D. JSOC - HMI Pipeline HMI Data Analysis Pipeline Doppler Velocity Heliographic Doppler velocity maps Tracked.
Advertisements

Solar Orbiter F2/F3 Presentations, 12 Sep 2000 Solar Orbiter A high-resolution mission to the Sun and inner heliosphere.
The BepiColombo Mission
Workshop „X-ray Spectroscopy and Plasma Diagnostics from the RESIK, RHESSI and SPIRIT Instruments”, 6 – 8 December 2005, Wrocław Spectroscopy Department.
Solar Orbiter Exploring the Sun-heliosphere connection
GONG 2010 – SoHO 24 Aix-en-Provence The Solar Orbiter Mission Max-Planck-Institut für Sonnensystemforschung Achim Gandorfer.
We are in a Revolutionary Period in our Understanding of the Sun because of New Data 10 Years of YOHKOH X-Ray Images 12 Years of SOHO Magnetograms, Dopplergrams,
Solar Energetic Particle Production (SEPP) Mission Primary Contacts: Robert P. Lin (UC Berkeley), John L. Kohl (Harvard-Smithsonian CfA) Primary Science.
HMI – Synoptic Data Sets HMI Team Meeting Jan. 26, 2005 Stanford, CA.
HMI/AIA Science Team Meeting, HMI Science Goals Alexander Kosovichev & HMI Team.
SDO Project Science Team 1 The Science of SDO. SDO Project Science Team 2 Sensing the Sun from Space  High-resolution Spectroscopy for Helioseismology.
1.B – Solar Dynamo 1.C – Global Circulation 1.D – Irradiance Sources 1.H – Far-side Imaging 1.F – Solar Subsurface Weather 1.E – Coronal Magnetic Field.
HMI Science Objectives Convection-zone dynamics and the solar dynamo  Structure and dynamics of the tachocline  Variations in differential rotation 
HMI Optics Package HMI Electronics Box The Solar Dynamics Observatory will be placed into an inclined geosynchronous orbit to maximize sunlit hours while.
Solar Polar Orbit Radio Telescope (SPORT): A Mission Concept for Interplanetary CMEs Imaging WU Ji, LIU Hao, SUN Weiying, ZHENG Jianhua, FENG Xueshang,
Instrumental & Technical Requirements. Science objectives for helioseismology Understanding the interaction of the p-mode oscillations and the solar magnetic.
HELAS, Nice 27 September 2006 Visible light Imager and Magnetograph T.Appourchaux on behalf of the VIM team IAS.
Solar Probe: Mission to the Sun Donald M. Hassler/David J. McComas Southwest Research Institute.
Science Requirements for Helioseismology Frank Hill NSO SPRING Workshop Nov. 26, 2013.
An Introduction to Helioseismology (Local) 2008 Solar Physics Summer School June 16-20, Sacramento Peak Observatory, Sunspot, NM.
1 Future solar missions (Based on the summary by R.A. Harrison) S. Kamio
1/30/20081 MESSENGER First Mercury Flyby First Mercury Flyby January 14, 2008 Speaker: Marilyn Lindstrom Program Scientist, NASA Headquarters NASA Museum.
Seminar in association with the MEDOC 12 campaign, Nov 2003 Solar Orbiter Work of the ESA/NASA Solar Orbiter Study Team Presented by Alan Gabriel, IAS.
Spacecraft Instruments. ► Spacecraft instrument selection begins with the mission description and the selected primary and secondary mission objectives.
CopyrightCopyright: NASA Hubble Composite of Pluto.
Max-Planck-Gesellschaft Max-Planck-Institut für Sonnensystemforschung J. Woch, 1 st HELAS Workshop, Nice, Sep , 2006 SOLAR ORBITER A Mission Overview.
Telescopes and the Atmosphere Our goals for learning How does Earth’s atmosphere affect ground-based observations? Why do we put telescopes into space?
Enabling Technology Development: High cadence imaging spectrograph development Low mass/power instrumentation Advanced communication/DSN for future deployment.
Made by: Anuuke Vannavong. Facts Diameter (km) km Distance from Sun (km)- 57,900,000 Mass (kg)- 33 x 10 to the power of 22 (kg) Surface Gravity.
Solar System Missions Division Solar Orbiter Next major Solar and Heliospheric mission ESA ILWS flagship Now with the Inner Heliospheric Sentinels.
RUSSIAN SPACE MISSIONS FOR SOLAR-TERRESTRIAL SCIENCE ILWS-2011 A.A. Petrukovich, L.M. Zelenyi Space Research Institute V.D. Kuznetsov IZMIRAN.
195 Å image – behind 195 Å image – Sun- Earth line – SOHO/ EIT image 195 Å image – Sun- Earth line – SOHO/ EIT image 195 Å image – ahead SECCHI Extreme.
Coordinated Observations between MPO and MMO Harri Laakso ESA/ESTEC, Noordwijk.
The Solar Wind.
The Solar Orbiter mission Solar Orbiter represents a new approach to solar studies. –A huge increase in discovery space The payload consists of a suite.
29 August, 2011 Beijing, China Space science missions related to ILWS in China
STEREO Planned Launch November, Stereo imaging of Sun; coronal mass ejections from birth to Earth impact. What determines geo-effectiveness of solar.
JAXA’s Exploration of the Solar System Beyond the Moon and Mars.
Solar Orbiter Mission (ESA) - The near-Sun phase  approach the Sun as close as 48 solar radii (~0.22 AU). At these distances, the angular speed of a spacecraft.
NASA Returns To Mercury in 2011 with MESSENGER. This is the first mission to Mercury since Mariner 10 in 1975 It will fully map the entire surface of.
Advanced Solar Theory (MT5810) OUTLINE 1.Observational properties of the Sun 2.MHD equations (revision) 3.Induction equation - solutions when R m >1 4.Magnetic.
Space Research Institute Russian magnetospheric & heliospheric missions.
1. Short Introduction 1.1 Overview of helioseismology results and prospects.
Space Research Institute Future Russian magnetospheric & heliospheric missions L.M. Zelenyi, A.A. Petrukovich, G.N.Zastenker, M.M.Mogilevsky, A.A.Skalsky.
020625_ExtReview_Nexus.1 NEXUS / SDO / ILWS SDO Science goals: How does solar variability directly affect life on Earth? SDO areas of interest: –Solar.
8:30-9:10 AM: Philip Scherrer, What Can We Hope to Learn from SDO Overview of SDO HMI Investigation HMI Instrument.
ILWS, DLR, Dr. Frings ILWS Related Activities in Germany Beijing, August 29, 2011.
Juno Steve Levin Juno Project Scientist April 1, 2016.
Helioseismology for HMI Science objectives and tasks* Data analysis plan* Helioseismology working groups and meetings *HMI Concept Study Report, Appendix.
Space Exploration Discovery New Frontiers Flagship.
한 미 려 – Introduction (1) 2.Instrument & Observe 3.Science 2.
WG5: EUV Imagers and XRS-type Instrumentation R. D
Preliminary Platform Design for KuaFu-A
Solar Probe Plus Scheduled to be launched in 2018 Solar Probe Plus will come closer to the Sun than any spacecraft has ever flown - and what it finds could.
Solar Dynamics Observatory (SDO)
Management Council Meeting, UCLA November 2012
L4+L5 Mission as an Ideal Project for International Collaboration
HMI Status P. Scherrer.
Inside Jupiter and Saturn
Upcoming Facilities of IIA
PSP, SO, and Ground-based Synoptic Observations from NSO
ISAS Solar Physics Yohkoh (1991- ) Hionotori ( )
HMI Science Investigation Overview
Cassini Retrospective
HMI Investigation Overview
HMI Data Analysis Pipeline
Flight Dynamics Michael Mesarch Frank Vaughn Marco Concha 08/19/99
Detectors of the New Projects at NAOC
HMI Data Analysis Pipeline
esa. int/solar-orbiter/51168-summary/;
Presentation transcript:

Solar Orbiter

Contents The mission The mission The orbit The orbit The instruments The instruments VIM: Visible-light Imager and Magnetograph VIM: Visible-light Imager and Magnetograph Helioseismology with VIM Helioseismology with VIM

Solar Orbiter: the mission Mission: Assessment phase Instruments: Concept phase Objective: Produce images of the Sun at an unprecedented resolution and perform closest in-situ measurements Launch: May 2015 End: January 2024 Cruise phase(3y), nominal phase(3y), extended phase(2y). Solar Electric Propulsion  Chemical Propulsion

Solar Orbiter

Solar Orbiter: the orbit Elliptical orbit around the Sun Proximity to the Sun  up to 0.27 A.U Inclination of up to 35º Cruise phase of approx. 3.4 year using gravity assists from Venus and Earth.  150-day-long science orbit. Close encounters with the Sun. Venus gravity assist maneuvers to increase inclination.

Solar Orbiter: the orbit Assisted by a series of Venus swing- bys, the spacecraft’s 150- day orbit will evolve gradually over the mission lifetime from an inclination of about 12 to 35 degrees to the solar equator. Assisted by a series of Venus swing- bys, the spacecraft’s 150- day orbit will evolve gradually over the mission lifetime from an inclination of about 12 to 35 degrees to the solar equator.

Solar Orbiter: the orbit

Solar Orbiter: the instruments Field Package: Field Package:  Radio and Plasma Wave Analyzer  Coronal Radio Sounding and Magnetometer Particle Package: Particle Package:  Energetic Particle detector  Dust detector  Neutron and Gamma-Ray Detector  Solar Wind Plasma Analyzer Solar remote sensing instrumentation: Solar remote sensing instrumentation:  Visible-light Imager and Magnetograph (VIM)  EUV Imager and Spectrometer  Coronagraph  Spectometer/Telescope for Imaging X-rays  Radiometer ???

Visible-Light Imager and Magnetograph (VIM) Vector magnetic field capabilities (priority). Vector magnetic field capabilities (priority). Line-of-sight velocity maps by observing 4-5 points on either side of a spectral line. Mention the possible lines  HMI, IMaX, GONG. Line-of-sight velocity maps by observing 4-5 points on either side of a spectral line. Mention the possible lines  HMI, IMaX, GONG. Two functions: Two functions: High resolution Telescope (HRT) High resolution Telescope (HRT) Full Disc Telescope (FDT) Full Disc Telescope (FDT) Using two telescopes that share filtergraph optics and detector. Magnetic field and velocities calculated on board Magnetic field and velocities calculated on board Telemetry restricted and only approx. ¼ of total VIM telemetry will be assigned to velocity data. Telemetry restricted and only approx. ¼ of total VIM telemetry will be assigned to velocity data.

Local Helioseismology with VIM Advantages Observation of high latitudes and the poles Observation of high latitudes and the poles Some very high resolution data Some very high resolution data Proximity to the sun. Not really needed for helioseismology Proximity to the sun. Not really needed for helioseismology Co-rotation (not clear what it means) Co-rotation (not clear what it means) Maybe continuous 256x256 full disk data Maybe continuous 256x256 full disk dataDisadvantages Short series of data (~10 days every 50 days) Short series of data (~10 days every 50 days) Variable resolution in a 512x512 grid (or less) Variable resolution in a 512x512 grid (or less)

Local Helioseismology with VIM Dynamic/Magnetic description of the solar subsurface at high latitudes and the poles. Dynamic/Magnetic description of the solar subsurface at high latitudes and the poles. Rings: Rings: Differential rotation close to the poles. Differential rotation close to the poles. Meridional circulation: Solve the multi-cell circulation mystery… Meridional circulation: Solve the multi-cell circulation mystery… Time Distance: Time Distance: Dynamics down to the tacholine at the poles. Dynamics down to the tacholine at the poles. Combined VIM-HMI/GONG for deep interior research. Combined VIM-HMI/GONG for deep interior research. Holography Holography Farside calibration/mapping the near side Farside calibration/mapping the near side Mapping the poles. Mapping the poles.