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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 => nov ’07
• new website Radio monitoring @ http://secchirh.obspm.fr
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STEREO Public Relations
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PICARD Mission
PREMOS2
SOVAP
SODISM
Phase C/D in progressLaunch planned for 2nd quarter 2009
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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)=> space weather
- Solar oscillations
from the ground :
- diameter, limb shape and asphericity,
- local atmosphere turbulence
PICARD SCIENTIFIC PRODUCTS
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TARANIS
• Dedicated to understandingAtmosphere/ionosphere/magnetospherecoupling (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 septemberLaunch 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
DESIR
LYOT
HEBS
Phase A ended (PRR) on 7 june, 2007 Launch objective 2012-2013
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SMESE payload required performances
Wavelength/Energy
Field of View
Spatial resolution
Cadence
LYOT : L imager
121.6 nm Full Disk 1.1 arcsec 10 s
LYOT :L coronagraph
121.6 nm 5*5 solar radii
2.3 arcsec 20 s
DESIR :Infra-red Telescope
35 ≤ 1 ≤ 80 microns
100≤ 2 ≤ 250 microns
Full Disk 50 arcsec at 35 microns
100 ms
HEBS 10-500keV200keV-10MeV10MeV-600MeV
Full Disk Full disk 1 s, down to 32 ms
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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 Sun’s atmosphere.
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PICARD SMESE
PROGRAMMATIC SCHEME
TARANIS
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■ Following an open AO to the French Scientific community
■ Mission scheme
■ See presentation at IHY 2nd European General Assembly (Turin, 18-23 june)
Technical support to PHOIBOS proposal
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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 @CDPP, K. Bocchialini @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 dataInstrument Co-Is, Guest Investigators restricted rightsPublic: 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
60x60x50 cm bus
S-Band TTC (Kiruna/Toulouse)
Bus waiting row
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MYRIADE CAPACITY
■ Orbit inclination > 20°■ Altitude 600km< >1000km■ 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 > 60w (highly orbit dependant)■ Mass memory 16 Gbits■ S-Band 400 kb/s as baseline
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MYRIADE OPTIONS
■ propulsion V ~80 m/s (DEMETER, TARANIS…)
■ X-Band telemetry (>a 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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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?
FURTHER INTERNATIONAL COOPERATION