Coordinated Investigation Program Reference Heliosphere IBEX Joins at the Right Time PowerPoint PPT Presentation

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Title: Coordinated Investigation Program Reference Heliosphere IBEX Joins at the Right Time


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Coordinated Investigation ProgramReference
HeliosphereIBEX Joins at the Right Time!
  • Eberhard MöbiusJoe Davila, Giannina Poletto,
    Steve Suess

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A Great and Timely Opportunity!
  • Voyager 1 Crossed the Termination Shock Now
    Roams the Heliosheath!Voyager 2 Will Follow at
    a Different Location
  • IBEX Launch is Planned June 2008

Remember 1957/58!The International Geophysical
Year (IGY)
We Stuck Our Head Above the Atmosphere
Look Forward to 2007/08! The International
Heliophysical Year (IHY)
NASA Keep Voyager, Ulysses, ACE, SOHO,.. Our
S3C Great Observatory Alive!!!
We are About to Stick Our Head Out of the
Heliosphere
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What Is the Configuration of Our Fleet?
  • Voyager 1 2 at Termination Shock and in
    Heliosheath
  • Ulysses on its last Fast Latitude Scan During A-
    HeliosphereTwo Extended Quadratures with
    Earth-Sun Line 06-07 07-08
  • ACE, SOHO, WIND provide Particle and Solar Image
    Observations from an Earth Vantage Point
  • STEREO Joins Inner Heliosphere Fleet Summer/Fall
    2006Providing Stereoscopic Views of Solar
    Transients
  • IBEX Joins Fleet June 2008Providing a Global
    View of the TS and LIC O Observations
  • Solar Wind takes 1 Year from the Sun to the TS
    (90 AU)
  • ENAs take 0.5 Years (4 keV/nuc) to 2 Years
    (0.25 keV/nuc) from the TS to IBEX IBEX
    Observes Response to 2006 - 08 Output During
    its Primary Mission Phase

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Voyagers at TS
TS Distance modeled by Wang Richardson
TSP at V2 observed at 77 AU If TSPs occur 7 AU
upstream TS at V2 is at 84 AUSept 2007 If
TSPs occur 4 AUTS at V2 is at 81 AUOct
2006(stationary shock)
Voyager 2
Voyager 1
Adapted fromRichardson, Stone
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Focus Areas of the CIP
  • Benchmark Set of LIC Parameters Outer Boundary
    Condition for the HeliosphereIncludes He (LIC
    Proper) H, O (Interface H, O) Composition
    (Constraints for Ionization Radiation)
  • Global Structure Size of the HeliosphereTopolog
    y, Structure Distance of Termination Shock and
    Heliopause LIC Magnetic FieldTransport of
    Cosmic Rays A- vs. A Heliosphere
  • Evolution of CIRs Isolated CMEs Follow
    Structures from the Sun Throughout the Heliosphere

Observation Period 2006 - 2008 (-2010 for
IBEX)Constitutes Solar Minimum Well Organized
Heliosphere Isolated Transients
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Benchmark Set of LIC ParametersReference
Heliosphere
  • LIC He Parameters (NHe, THe, vHe) at Solar
    Minimum Neutrals, UV, PU Ions (Ulysses, ACE,
    SOHO, Wind)Found that Ionization Plays Important
    Role
  • NH at TS (Ulysses, Voyager, ACE, SOHO) Pickup
    Ions Solar Wind Slow Down
  • NH in LIC Voyager at TSModeling of Filtering
    yields NH in LIC
  • LIC O Parameters (TO, vO,NO at TS), Slowdown,
    Heating Deflection of Secondary O (IBEX,
    Ulysses)Modeling of Filtering yields NO in LIC
  • Composition (Ulysses, ACE)Modeling yields
    Ionization Radiation Environment

Voyager at TS
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Global Structure Size of the Heliosphere
  • During this Solar Minimum we are Lucky to Muster
    Simultaneously- Spacecraft from Inside 1 AU
    (Messenger) up to the Heliosheath (Voyagers)- 3D
    Capability in the Inner Heliosphere (Ulysses
    Coronagraphs)- Global Imaging of the
    Heliospheric Boundary (IBEX)- Comprehensive
    Particle, Fields Solar Observations from 1 AU
    (ACE, SOHO, WIND STEREO)

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  • Ulysses Orbit in 2006-2008
  • S. T. Suess1 and the Ulysses Project
  • 1. National Space Science Technology Center,
    NASA Marshall Space Flight Center, MS XD12,
    Huntsville, AL 35801 USA

Quadratures, a unique Vantage Point of Ulysses
in 2006-2008 relative to the Earth, ACE, SOHO,
STEREO, Solar-B, etc. Voyager
Coronagraphs provide view of Coronain Plane of
Ulysses Orbit
S. T. Suess
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Ulysses-SWICS Overview
  • Ulysses SWEPAM SWICS Provide Unambiguos
    Information about Fast and Slow Solar Wind

von Steiger Fröhlich, ISSI SR-3, 2005
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Earth-Sun Ulysses Quadratures 2001-2009
  • Configuration in Fall 2001 was never quite a
    quadrature Ulysses at high heliographic latitude,
    but much less than 900 All periods were very
    short!
  • Quadratures in winters 2007 2008 feature times
    when the SOHO-Sun-Ulysses angle remains near 900
    for 5 months. Ulysses is at heliographic latitude
    near 900 Allows Monitoring of 3D SW Output

S. T. Suess
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Ulysses Orbit and Solar Cycle
Launch Dates of New Missions
IBEX Launch
S. T. Suess
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Evolution of CIRs Isolated CMEs
  • Solar Minimum is the Time of Isolated
    Transients- Co-Rotating Interaction Regions-
    Few Isolated CMEs
  • Spacecraft Constellation Allows 3D Tracking
  • Modeling of Transient Evolution - During Solar
    Minimum Allows a More Orderly Start- Spacecraft
    Constellation Allows Tracking Throughout the
    Heliosphere

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Ulysses in Fixed SOHO/Earth - Sun Coordinates
  • Ulysses moves S - N (Dec 19, 2006, - May 28,
    2008)
  • Fuchsia Portion Dec 19 2006 - May 28
    2007Ulysses within 5o of the Suns Limb
  • Green Portion Dec 2 2007 - May 28 2008Ulysses
    within 10o of the Suns Limb

Long quadratures - Allow 3D accumulation over
Solar Rotation - Provide long time to
catch activity towards Ulysses
S. T. Suess
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STEREO to be Launched Summer 2006
  • STEREO Positions During Ulysses Fast Latitude
    Scan
  • Ulysses Passes behind Earth (ACE, SOHO, Cluster
    etc)
  • Ulysses STEREO See 3D Evolution of Transients

S. T. Suess
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CIP Reference Heliosphere
  • We have an almost ideal Once in a Lifetime
    Opportunity to unravel the Heliospheric
    Structure and Temporal Evolution
  • Are there other Investigation Aspects that I
    missed?
  • Which Detailed Observations should be Performed
    on these Spacecraft to Provide Maximum Synergy?
  • Which Modeling Efforts should be Undertaken?
  • Any Additional- Targeted Observations-
    Monitors- Modeling Efforts?

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Ulysses-SWICS Overview
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Ulysses-SWICS Overview
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