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The ESA Science Programme: Status of Solar and Solar Terrestrial Missions and other initiatives of i

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Title: The ESA Science Programme: Status of Solar and Solar Terrestrial Missions and other initiatives of i


1
The ESA Science Programme Status of
Solar and Solar Terrestrial Missions and other
initiatives of interest for Space Weather
  • Hermann J. Opgenoorth
  • ESA ESTEC
  • Solar and Solar Terrestrial Missions Division
    (SCI-SH)
  • Research and Scientific Support Department
    (RSSD)

2
Mandatory Programme DisciplineProspects
M3
IRSI DARWIN
XEUS
SOLARORBITER
GAIA
LISA
BEPI COLOMBO
LTP

JWST
ROSETTA
  • Fundamental
  • Physics


F 2
VENUSEXPRESS
HERSCHEL
PLANCK
MARS EXPRESS
INTEGRAL
SMART 1
Time ?
ISO
HST
HUYGENS
ULYSSES
CLUSTER II
  • Planetary
  • Solar/STP
  • Astronomy

XMM NEWTON
SOHO CLUSTER
3
Ulysses
  • Joint ESA-NASA Mission The Heliosphere in 4-D
    Spatial 3-D and Time
  • Earlier anticipated end of Mission 30. Sept.
    2004
  • Recent ESA-SPC decision to extend the scientific
    operations by 3.5 years - March 2008 allowing
    third polar pass
  • Now discussed in NASA Advisory Structure
    Senior Review in 2005 - (under threat from recent
    NASA MODA cuts)
  • Key Scientific Goals in the Context of Extension
  • Energetic particle and dust dynamics effect of
  • reversed field polarity on latitude dependence
  • Reconfirm the north-south heliospheric asymmetry
  • 3-D structure of CMEs and heliospheric current
  • sheet in conjunction with ecliptic S/C like
    STEREO

4
SOHO Solar Cornerstone Mission
Presently THE Solar Observatory ESA / NASA
Collaboration since 1995 Currently 4 year mission
extension 2003-2007 Future
extension(2007-2009) proposal in 2006 Also s c
SOHO Bonus Mission discussed to provide
Coronagraph to International Living With a Star -
ILWS
5
Cluster ESAs Magnetospheric Cornerstone Mission
  • First 3-D satellite mission ever
  • ESA - NASA Collaboration
  • - since 2000

Earlier ESA-SPC decision 100 orbital data
coverage and 3 yr mission extension 2003 -
2005 Second extension for 22 years until
December 2009 decided in Febr. 2005 SPC Now at
largest separation
6
Cluster new regions subsolar point and auroral
acceleration
Cluster Extension
Magnetopause Subsolar point
2001
2009
7
Double Star Cluster Evolution of Reconnection
Cluster Extension
DSP
Cluster
Strong flow of plasma observed first at Double
Star and 5 min later at Cluster
From Pitout et al., 2005
8
Cluster at new region Near-Earth Current
Disruption
Cluster Extension
2001
Near-Earth tail Current Disruption
  • Crossing of tail at 8-10
  • Earth radii
  • Current Disruption key
  • process for substorms

2009
9
Cluster Extension
Complementarity of Themis and Cluster
  • THEMIS will be launched in 2006 with 1st tail
    season in February 2007

Themis
Cluster
THEMISs tail science benefits from Clusters
Solar Wind and ionospheric monitoring and half a
year later Cluster tail science benefits from
THEMISs upstream, sheath and magnetopause
monitoring. In addition vaste ground based
network in Canada and Europe for Cluster / Themis
  • From V. Angelopoulos, Berkeley, USA

10
DOUBLE STAR
China / ESA Collaboration
  • Two satellites equipped mainly with
    Cluster Spare Instruments
  • in Magnetospheric
    Polar and Equatorial orbits
  • DSP-E 550 km x 9
    Re DSP-P 350 km x 4 R
  • Commissioning Phase completed - ok, except
    attitude control
  • Excellent science results - in particular in
    coord. with Cluster
  • 1.5 yrs mission extension recently decided (May
    2005 SPC)

11
Extension summer 2005 Tail
  • Cluster 14-16 Re sep.1000-10000 km
  • DSP TC-1 9 Re apog. above equator
  • DSP TC-2 7 Re apogee in tail

09 Sept. 2005, 1600 UT
5 Re
XZ
lt Observe NENL and/or Bursty Bulk Flow at
Cluster and then monitor Current
Disruption and BBF breaking at DSP gt Observe
Current Disruption at DSP and then
outgoing rarefaction-wave at Cluster.
12
Extension summer 2006 Tail
  • Cluster 14-16 Re sep 1000-10000km
  • DSP TC-1 9 Re gradual sep. in Y
  • DSP TC-2 apogee in southern hemisphere

11 Sept 2006 0000
TC-1
XZ plane
XY plane
gt Observe the azimuthal extent and dynamics of
current disruption
13
Extended mission spring 2006 Cusp
  • Cluster at northern
  • magnetopause/cusp
  • 10000 km separation
  • TC-1 near the cusp
  • TC-2 at southern cusp
  • and in inner magneto-
  • sphere on dayside

XZ
XY
14
22 Dec 2005, 00 UT
Extended mission winter 2005
  • DSP TC-2 and IMAGE both in the southern
    hemisphere
  • Stereo ENA images of the ring current from the
    southern hemisphere
  • Observations require geomagnetic storms

15
  • Solar Orbiter
  • ESA-ILWS Flagship
  • in the long term
  • Selected as ESA Flexi-mission
  • launched within 10 yrs - lifetime 5 2 yrs
  • confirmed as part of COSMIC VISION
  • Formal negotiations about a potential
  • NASA contribution ( or collaboration
  • with Solar Sentinels ) in progress
  • - Inner Heliosphere In-Situ observations
  • and simultaneous Solar Remote Sensing
  • Orbit up to 35 deg out of the ecliptic, i.e.
  • topside view of polar regions and CMEs
  • observe the far-side of the Sun from a
  • co-rotating vantage point at 0.22 AU,
  • equivalent to 48 Solar radii

16
Solar Orbiter Status
  • (Confirmed as part of Cosmic Vision by SPC,
    June 2004)
  • Mission profile
  • Launch by Soyuz-Fregat 2-1b (either Oct 2013 or
    March 2015)
  • Cruise phase (SEP / Chemical Propulsion) 1.8 /
    3.3 yrs
  • Nominal science mission duration 2.8 yrs
  • Extended mission (high-latitude phase) 2.4 yrs
  • Minimum perihelion distance 48 solar radii
    (0.222 AU)
  • Maximum solar latitude 35 (in extended phase)
  • SPACECRAFT two industrial studies completed
    (Sci-A)
  • 6 month delta-study (chem. prop.) completed
  • PAYLOAD definition completed
  • Particles and Fields Package
  • Remote-sensing Package
  • PLAN Science Management Plan to SPC in
    February 2006
  • - coordinated AO with NASA (Solar Sentinels)
    Summer 2006

17
S-O Mission duration and solar cycle
18
The Solar-B satellite
  • JAXA successor to Yohkoh (Solar A)
  • Japan/US/UK mission (Norway, ESA)
  • Launch in Aug. 2006 aboard M-V rocket from
    Uchinoura Space Centre (USC)
  • Polar sun-synchronous orbit. 600 km altitude
  • Nearly continuous solar view (with no day/night
    cycling for nine months each year)
  • A coordinated set of optical, UV, and X-ray
    instruments to understand the dynamic Sun.
  • Mass 900 kg
  • Power 1000W
  • Telemetry 4Mbps
  • Data Recorder 8Gbit
  • Attitude Solar pointed
  • Stability 0.7 arcsec/1s
  • Launch Summer 2006

19
Solar-B Science Goals - Understanding the
Dynamic Sun
  • To understand the creation and destruction of the
    Sun's magnetic field.
  • To understand the modulation of the Sun's
    Luminosity.
  • To understand the generation of UV and X-ray
    radiation.
  • To understand solar wind and eruptions.
  • Provide the first accurate measurements of
    magnetic fields and electric currents that will
    reveal the causes of eruptions in the solar
    atmosphere

20
Solar-BThe 3 Instrument Suite
  • 0.5m Optical Telescope FPP (Focal Plane Package)
  • Spectro-Polarimeter
  • Broadband Filtergraph
  • Narrowband Filtergraph
  • XRT (X-Ray Telescope)
  • 9 filters hot-very hot corona
  • EIS (EUV Imaging Spectrograph)
  • 2x40 Å wide wavelength
  • region in EUV covering
  • transition region - corona

21
ESA Support to Solar-B
  • ESA, in sub-contractual collaboration with the
    Norwegian
  • Space Centre, will provide one additional
    downlink contact
  • to Solar-B for each of the 15 orbits per day
  • This will considerably improve the overall
    scientific data return
  • and the cadence of observations from the
    Solar-B mission
  • The European scientific community
  • will be catered with processed data
  • through a dedicated Solar B data
  • centre at the University of Oslo


22
Svalbard Ground Station for Solar-B
  • Reasons Antenna redundancy,
  • possibility to track all 15 orbits
  • every day and Norwegian
  • interest in the mission.

23
International Living with a Star - ILWS
(presently involving more than 25 space
agencies SC CNSA, CSA, ESA, (R)FSA, JAXA,
NASA )
MISSION
  • Stimulate, strengthen and coordinate space
    research
  • to understand the governing processes of the
    connected Sun-Earth system as an integrated
    entity.
  • (governing processes which affect life and
    society gt SpaceWeather)
  • simultaneous and coordinated observations
  • at strategic locations in the entire system
  • (supported by advanced analysis and model tools)

24
SWARM Mission Living Planet ESA - EOP
Earths Environment One mans noise is another
mans data
Earths Interior - Baseline mission
  • Selected by Earth Observation Program Board -
    Launch 2009
  • Electric Field Instrument
  • (Ion Drift Meter) provided by CSA in
    collaboration with ESA Science Programme
  • Optimisation of GEOSPACE
  • science - additional electron
  • instrument Conducto-meter
  • discussed

25
New KuaFu - selected for Phase BSolar Storm,
Aurora and Space Weather Exploration
Launch Date 2012
L1polar trip-star project
Pre-study supported by the National NSF of China
26
KuaFu-A at L1
Solar EUV emission
White light CME
Radio wave measurement
local plasma and magnetic field
High energy
particles KuaFu-B1B2 polar orbit
24 hours Aurora Image Apogee
Perig. Magnetic
field High energy
particles
27
Solar Wind, Aurora and Storms exploration (SWASE)
- recently de-selected
Proposed by Professor Z.X.Liu of CSSAR, Chinese
Academy of Sciences (elements of SWASE
will be added to New KuaFu)
28
ESAs Cosmic Vision, 2015-2025
  • Themes
  • What are the conditions for life and planetary
    formation?
  • How does the Solar System work?
  • From the Sun to the edge of the Solar System
  • First, the hierarchy of scales in the
    magnetosphere (e.g. M3, Magnetospheric SWARM)
  • Gaseous Giants and their Moons
  • The Building Blocks of the Solar System
    Asteroids and Small Bodies
  • What are the fundamental laws of the Universe?
  • How did the Universe originate and what is it
    made of?
  • Giovanni Bignami, chairman SSAC, 10 May 2005

29
Three scales of plasmas shocks as an example
30
Cross-Scale key concepts
  • Spacecraft on a hierarchy of scales
  • Electron group
  • Electron instruments
  • 3 axis electric and magnetic fields
  • Ion group
  • Fast ion instruments
  • Magnetic field instruments
  • Fluid group
  • Bulk plasma and field instruments
  • Energetic particles
  • Note
  • Need different instrumentation at each scale
  • Other agencies could provide one or more scales

31
Cross-Scale - The ESA context
  • Cosmic Vision 2015-2025
  • Relative to other CV mission concepts,
    Cross-Scale is
  • Cheap lt300M, baseline of single Soyuz-Fregat
    launch
  • Quick early in programme - by 2015?
  • Easy no technological show-stoppers
  • Potential for international collaboration JAXA
  • SCOPE 5-s/c mission for cross-scale plasma
    dynamics
  • Led by M. Fujimoto ISAS
  • First inter-agency discussions at two ESA /JAXA
    Bilaterals

32
European ILWS Strategy in an Overview
33
SCOPE the Japanese connection
  • Proposed ISAS five-spacecraft mission
  • Focus on electron dynamics at shocks and
    reconnection sites
  • Potential for incorporating SCOPE as the inner
    scale of Cross-Scale
  • This is only one possible scenario!

34
Magnetopause
EXAMPLE M-Pause crossing on Febr. 22, 2004 TC1
1930 UT sub-solar Cluster 2010 UT high lat. gt
Delta t 40 min Crossings so far 21 within 1
hour and only 4 within 15 mins
DSP-TC-1
Cluster
From Cornilleau et al., 2005
35
From Cornilleau et al., 2005
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