Spacecast Richard B Horne, S. A. Glauert, N. P. Meredith, D. Boscher, V. Maget, A. Sicard, D. Heynderickx and D. Pitchford Forecasting the High Energy.

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Presentation transcript:

Spacecast Richard B Horne, S. A. Glauert, N. P. Meredith, D. Boscher, V. Maget, A. Sicard, D. Heynderickx and D. Pitchford Forecasting the High Energy Electron Radiation Belts within the FP7 SPACECAST Project ESWW9, Brussels, 6th November 2012

Radiation Damage to Satellites Solar energetic particles Single event upsets Degrades solar array power High energy electrons (Rad. belts) Internal charging – ESD Low energy electrons Surface charging - ESD Total ionizing dose Micrometeoroids and debris - ESD

Magnetic Storms – Radiation Belts The electron radiation belts are highly variable Electron flux can change by 5 orders of magnitude within 3 minutes Note higher radiation for GNSS/Galileo orbits Boeing – launch to GTO and use plasma thrusters – 1-2 months in radiation belts Baker et al. Nature [2004] > 2 MeV electron flux Distance (Re) Geostationary orbit Slot region Usually benign – except during large storms Galileo orbit

Forecasting Concept It takes ~ minutes for the solar wind to flow from the ACE satellite to the Earth Access ACE satellite data in real time and use it to drive our forecasting models Use a forecast of Kp index from Swedish Inst. Sp. Phys. (Lund) and BGS (UK) and data from Europe, USA and Japan We use physical models –Like weather forecasting ACE satellite Radiation Belts

We use Physical Models that Include Wave-Particle Interactions Wave-particle interactions cause electron acceleration and loss Cause variability Changed ideas lasting 40 years Antarctic observations Satellite observations

Radial Diffusion: Transport of Electrons Across the Magnetic Field Fast solar wind drives ultra-low frequency (ULF) waves Oscillations in the Earth’s magnetic field ULF waves enhance electron transport across the magnetic field Radial diffusion

Testing the BAS Radiation Belt Model CRRES Relativistic Electrons ~1MeV J  (cm -2 s -1 sr -1 keV -1 ) BAS Model with Radial Diffusion only J  (cm -2 s -1 sr -1 keV -1 ) BAS Model with Radial Diffusion and Waves

FMI model server Web Serv er MySQL Database BAS model server SWPC GOES, ACE Central server and database DHC Satellite operators Service providers Scientists General public Academia BGS Kp,Dst RT Lund Kp,Dst FC Potsdam Kp QL Kyoto Dst QL NGDC Kp,Dst Arch Post Processing ONERA model server FTP Web Servic e SPACECAST Forecasting System

SPACECAST – Forecast >800 keV electrons 3 hour model forecast GOES satellite data Model

SPACECAST – Forecast >800 keV electrons 3 hour forecast at Geo Note whole rad belt: GEO + MEO >800 keV electron flux increases Kp index GOES data Solar wind Dst and SW pressure GOES orbit

SPACECAST > 2 MeV Electrons Satellite data affected by SW

Risk of Satellite Charging - ESD Geosynchronous OrbitGNSS/Galileo Orbit Model results converted into a risk index based on previous satellite anomalies Risk depends on satellite design Needs close collaboration with satellite operators and designers

March 2012 Forecast in red data in blue Magnetopause in Green

Benefits of Physical Models Forecast what is likely to happen – enables mitigation Reconstruct what happened in the past - identify the cause of satellite anomalies Construct data where there are little/no observations – GNSS orbits Calculate extreme conditions based on physical principles Calculate number of particles precipitating into the atmosphere - effects on low altitude satellites, ionization and GPS signals

Conclusions SPACECAST makes real time forecasts of the radiation belts for satellite operators Forecast for 3 hours, updated every hour, and translated into a risk index Unique features Physical models, that include wave-particle interactions Forecast for the whole radiation belts – including GNSS/Galileo orbits European led – with USA and Japan Forecasts can be improved by Coupling the solar wind/magnetopause to the radiation belts Including low energy electrons – surface charging Options to model extreme events and orbits where there is little/no data

Acknowledgements The research leading to these results has received funding from the European Union Seventh Framework Programme (FP7/ ) under grant agreement no