Update of the French activities relevant to ILWS

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Update of the French activitiesrelevant to ILWS

• Jean-Yves Prado, CNES

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Report from CNES

• STEREO
• PICARD
• TARANIS
• SMESE
• Technical support to PHOIBOS proposal to Cosmic
  Vision
• Data Issues
• Back-up slides on MYRIADE

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STEREO

• STEREO Space Weather beacon Ground Station gt
  nov 07
• new website Radio monitoring _at_
  http//secchirh.obspm.fr

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STEREO Public Relations
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PICARD Mission
Phase C/D in progress Launch planned for 2nd
quarter 2009
SOVAP
PREMOS2
SODISM
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PICARD SCIENTIFIC PRODUCTS
from orbit - Diameter, limb shape and
asphericity in the continuum - TSI (x2) - 5
spectral channels (215,393, 535, 607, 782 nm) -
Activity (images at 215 nm and Ca II)gt space
weather - Solar oscillations from the ground
- diameter, limb shape and asphericity, -
local atmosphere turbulence
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TARANIS

• Dedicated to understanding
• Atmosphere/ionosphere/magnetosphere
• coupling (sprites, elves, blue jets)
• Microcameras photometer -MCM- CEA (JP)
• EM measurements -IEM- LPCE (PL,TCH)
• X-gamma Detector -XGD- LANL (USA), DNSC (DK)
• Detector of high Energy ElectronsCESR (TCH)

• Quasi Sun Synchronous Orbit (2hrs LT drift/year)

Phase B will start in september Launch expected
for 2011
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TARANIS OBJECTIVES
Description - characterization of the sprites
and associated emissions, measurements of their
occurrence frequency and of their distribution at
the scale of the earth. (caméras, EM waves, X and
? spectra, high energy electrons) - study of the
effects of the magnetic latitude and volcanic
activity Implied mechanisms - determination
of the nature of the triggering phenomena (cosmic
radiation) - determination of the source
mechanisms (EM waves, X and ? spectra, high
energy electrons) - study of the nature of the
explosive dissipation of energy in the ionosphere
and magnetosphere (EM waves, X and ? spectra,
high energy electrons) Global impact -
determination of the effects on the upper
atmosphere, ionosphere and magnetosphere (EM
waves, high energy electrons, associated ground
based measurements, other satellites) -
evaluation of the coupling atmosphere -
 ionosphere - magnetosphere and inter-planetary
medium
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SMESE
LYOT
DESIR
HEBS
Phase A ended (PRR) on 7 june, 2007 Launch
objective 2012-2013
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SMESE payload required performances
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SMESE Firsts

• First combined imaging (disk, corona) in Ly ?
  with high time resolution and sensitivity to
  trace the development of CMEs in the low corona
  first polarimetric corona measurements,
• First ever measurements of solar flares in the
  far infrared, key range for relativistic leptons
  and chromospheric plasma heated during flares,
• First hard X-ray/gamma ray spectrometry at the
  highest energies ever attained with a
  solar-dedicated instrument, to study the most
  energetic electrons and nuclear processes in the
  Suns atmosphere.

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PROGRAMMATIC SCHEME
PICARD
SMESE
TARANIS
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Technical support to PHOIBOS proposal

• Following an open AO to the French Scientific
  community
• Mission scheme
• See presentation at IHY 2nd European General
  Assembly (Turin, 18-23 june)

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Data Issues

• Support from CNES to thematic data centres
  (CDPP, MEDOC)
• Data sets from CNES supported missions/instrument
  data some others
• Support to development of tools
• POC contact C. Jacquey _at_CDPP, K. Bocchialini
  _at_MEDOC
• Data policy for PI missions OK for openness,
  rapidity on a case by case basis
• quality/reliability issues
• priority to the PI for use of data
• matrix of access rights defined by Scientific
  Committee of the relevant mission
• Typicaly Mission PI/CoIs
  all rights on all data
• Instrument Co-Is, Guest Investigators
  restricted rights
• Public access to all data after a TBD delay (6
  months to 2 years)

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MYRIADE SERIES

• More than 20 spacecraft based on the same bus
  and systems
• in flight or in preparation

Bus waiting row
60x60x50 cm bus
S-Band TTC (Kiruna/Toulouse)
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MYRIADE CAPACITY

• Orbit inclination gt 20
• Altitude 600kmlt gt1000km
• DNEPR launcher as the reference
• Geocentric, inertial, solar or along the
  velocity vector pointing
• Pointing precision of 0.1 (actuation), 5.10-3
  (knowledge)
• Attitude control system in nominal mode uses a
  stellar sensor, four reaction wheels and three
  magnetic torquers
• up to 80 kg mass allocation to the P/L (when no
  propulsion/TM-X)
• Power available to the P/L gt 60w (highly orbit
  dependant)
• Mass memory 16 Gbits
• S-Band 400 kb/s as baseline

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MYRIADE OPTIONS

• propulsion DV 80 m/s (DEMETER, TARANIS)
• X-Band telemetry (gta few Gbits/day)
• TM rate 16-50 Mb/s depending on the ground
  station G/T
• additional sun pointing device (PICARD,
  LYOT/SMESE)
• quick deorbit kit under study

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A few examples of the MYRIADE versatility

• DEMETER, TARANIS waves and particle
  instruments
• PARASOL Lidar for
  atmospheric science
• PICARD, SMESE Solar observation
• MICROSCOPE Fundamental physics
• ARGOS Localization
• ESSAIM, SPIRALE, ELINT Defense

• commercial availability of the bus (ASTRIUM, AAS)

DNEPR launch
ARIANE 5 launch
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FURTHER INTERNATIONAL COOPERATION

• Earth Observation as a paradigm?
• a unique object, many possible instruments
• curiosity driven science in competitition with
  monitoring science
• shift from mammoth s/c (ENVISAT) to series of
  small specialized satellites
• 
  
• A Solar Train?