Advanced modeling of low energy electrons responsible for surface charging

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Advanced modeling of low energy electrons responsible for surface charging Natalia Ganushkina (1, 2), Stepan Dubyagin (1), Ilkka Sillanpää (1), Jean-Charles Matéo Vélez (3), Dave Pitchford (4) (1) Finnish Meteorological Institute, Helsinki, Finland (2) University of Michigan, Ann Arbor MI, USA (3) ONERA, Toulouse, France (4) SES ENGINEERING, Luxembourg The research leading to these results was partly funded by the European Union Seventh Framework Programme (FP7/2007-2013) under grant agreement No 606716 SPACESTORM and by the European Union s Horizon 2020 research and innovation programme under grant agreement No 637302 PROGRESS 12 th European Space Weather Week, November 23-27, 2015, Oostende, Belgium

Why are we interested in low energy electrons (< 200 kev) in the inner magnetosphere? Surface charging by electrons with < 100 kev can cause significant damage and spacecraft anomalies. The distribution of low energy electrons, the seed population (10 to few hundreds of kev), is critically important for radiation belt dynamics. Chorus emissions (intense whistler mode waves) excited in the low density region outside the plasmapause are associated with the injection of kev plasma sheet electrons into the inner magnetosphere. The electron flux at the kev energies is largely determined by convective and substorm-associated electric fields and varies significantly with geomagnetic activity driven by the solar wind variations on time scales of minutes! No averaging over an hour/day/orbit!

Surface charging events vs. geomagnetic conditions Events with consecutive absolute potentials < -10000 V Data: LANL (1989-2005), 1989-046, 1990-095, 1991-080, 1994-084, LANL-97A, LANL-01A and LANL-02A, MPA (Magnetospheric Plasma Analyzer), SOPA (Synchronous Orbit Particle Analyzer) and EPD (Energetic Particle Detector), from 1 ev to several MeV Matéo Vélez et al., Severe geostationary environments: from flight data to numerical estimation of spacecraft surface charging, Journal of Spacecraft and Rockets, submitted, 2015

Surface charging events vs. geomagnetic conditions High Fluxes at All Energies (HFAE) worst five minutes and worst fifteen minutes High Flux at Low Energy and Low Flux at High Energy (LFHE): max flux for 10-50 kev and min flux above 200 kev worst five minutes and worst fifteen minutes Matéo Vélez et al., Severe geostationary environments: from flight data to numerical estimation of spacecraft surface charging, Journal of Spacecraft and Rockets, submitted, 2015

It is challenging to model (nowcast) and forecast low energy electrons Following low energy electrons in large-scale magnetic and electric fields: Correct models for these fields are extremely hard to develop Specification of a correct initial conditions in the plasma sheet is very nontrivial Coefficients for radial diffusion when electrons move from the plasma sheet (10 Re) to inner regions (<6 Re) are far from being exact. How to introduce low energy electrons losses correctly? Electron lifetimes due to interactions with chorus and hiss, other waves, are they important? Substorms play a significant role in kev electron transport and energy increase. How to include them properly?

Inner Magnetosphere Particle Transport and Acceleration Model (IMPTAM) for low energy electrons (Ganushkina et al., 2013, 2014, 2015) traces electrons with arbitrary pitch angles from the plasma sheet to the inner L-shell regions with energies up to 300 kev in time-dependent magnetic and electric fields traces a distribution of particles in the drift approximation under the conservation of the 1st and 2 nd adiabatic invariants. Liouville theorem is used to gain information of the entire distribution function for the obtained distribution function, we apply radial diffusion by solving the radial diffusion equation electron losses: convection outflow and pitch angle diffusion by the electron lifetimes advantage of IMPTAM: can utilize any magnetic or electric field model, including self-consistent magnetic field and substorm-associated electromagnetic fields. Run online in real time: http://fp7-spacecast.eu and imptam.fmi.fi

Advances in IMPTAM for electrons Magnetic field model: Tsyganenko T96 (Dst, Psw, IMF By and Bz) Electric field model: Boyle et al. (1997) (Vsw, IMF B, By, Bz) Boundary conditions at 10 Re: newly developed empirical model for electron number density and temperature in the plasma sheet based on THEMIS observations (instead of Tsyganenko and Mukai (2003) model for ions) (Vsw, IMF Bz,Nsw) Radial diffusion with diffusion coefficients D LL (Brautigam and Albert, 2000) D LL 0.056Kp9.325 10 10 L Losses: Parameterization of the electron lifetimes due to interactions with chorus waves [Orlova and Shprits, 2014] and due to interactions with hiss waves [Orlova et al., 2014]: polynomial expressions with coefficients dependent on energy, radial distance, MLT sector and Kp.

Boundary conditions in the plasma sheet for modeling of kev electrons Near-Earth plasma sheet is the source for kev electrons in the inner magnetosphere. In the near-earth plasma sheet, continuous measurements of plasma sheet electrons are not available, in contrast to geostationary orbit. No solar wind driven empirical relations for electron fluxes or moments of electron distribution function which can be used easily for radiation belt modeling. Our previous studies [Ganushkina et al., 2013, 2014]: we set the model boundary at 10 R E and use the kappa electron distribution function. Parameters of the kappa distribution function: number density n and temperature T in the plasma sheet given by the empirical model derived from Geotail data by TM03 Tsyganenko and Mukai [2003]. The electron n is assumed to be the same as that for ions in the TM03 model, but Te/Ti = 0.2 is taken into account (Wang et al., 2012). Applying this model for boundary conditions has a number of limitations: (1) Model was derived from Geotail data for ions (limited detector energy range <40keV). (2) ratio Te/Ti can vary during disturbed conditions. (3) at distances closer than 10 Re, the correlation between Ti and Te might not exist at all and no certain ratio can be determined (Runov et al., 2015).

Model for electron temperature at 6-11 R e based on Cluster and THEMIS data: Empirical relations N Every point in the inner magnetosphere is defined by two normalized coordinates ϕ and R. The angle 2 Y GSM and R is the geocentric distance normalized by 10 R E. arctan X GSM The number density in the plasma sheet (Nps) is given in cm -3 as follows: ps 0. 715 0.3094 0.1486 N 1.187 1.104R B 2 0.2579 0.1148 0.1520 SW S N SW 1 3 10cm 5.75h 1 SW 0 0.33h S 0 2nT5. 25h t0 6.08h t 6.08h t N t dt, B t B t dt 0 0 t Nsw is the solar wind density and Bs is the sourthward IMF Bz. The temperature in the plasma sheet (Tps) is given in kev as follows: t 0.33h 0 S T ps 2 2.749 2.611R 0.6191 0.6271 R 0.5907 R 2 2 1.918R 1.466 2.224 R V SW 0.3587 B 0.513 S 0.6948R B 0.498 N 2 V t 1.83h t 3.58h 0 t V t 1.58h, B t B t dt, B t B t 0 0 SW S 0 S N 0 400km/ s 2nT1.5h t 0.33h 2nT3. 25 h 0 t0 SW 1 Vsw, Bs, and Bn are solar wind density, southward and northward IMF Bz components 1 1 0.33h N dt

Empirical model for plasma sheet electrons at 6-11 R e based on THEMIS data: Performance Hot plasma carried by BBFs (substorm injections)?

Losses for low energy electrons due to wave-particle interactions Parameterization of the electron lifetimes due to interactions with chorus waves [Orlova and Shprits, 2014]: polynomial expressions with 33 coefficients dependent on energy, radial distance, MLT sector and Kp. The model can be used for R=3-8 R E, Kp= 0-6, and electron energies from 1 kev to 2 MeV. MLT sectors include the night (-3 MLT 3), dawn (3 MLT 9), prenoon (9 MLT 12), and postnoon (12 MLT 15) segments.

Losses for low energy electrons due to wave-particle interactions Parameterization of the electron lifetimes due to interactions with hiss waves [Orlova et al., 2014]: two sectors, nightside at 21-06 MLT and dayside at 06-21 MLT, with corresponding coefficients. The obtained parameterization is valid for distances from 3 to 6 Re, Kp-indices up to 6, and energies from 1 kev to 10 MeV.

May 14 17, 2005 storm event absolute potentials < -10000 V LANL 1990-095: May 15, 2005, 0521 UT

May 14 17, 2005 storm event Smaller-scale flux variations are missing but values of modeled fluxes are close to observed ones

October 25, 2003 substorm event High Flux at Low Energy and Low Flux at High Energy (LFHE): max flux for 10-50 kev and min flux above 200 kev worst five minutes LANL 1994-084: October 25, 2003, 1454 UT

October 25, 2003 substorm event Substorm flux variations are missing but values of modeled fluxes are close to observed ones

Summary 1. IMPTAM is very suitable for modeling of fluxes of low energy electrons (< 200 kev) responsible for surface charging 2. It is NOT necessary to have even a moderate storm for significant surface charging event to happen 3. It is a challenge to model low energy electrons with their important variations on 10 min scales. Advance made: A revision of the source model at 10 Re in the plasma sheet was done using the particle data from THEMIS ESA and SST instruments for years 2007-2013. Most advanced representation of loss processes for low energy electrons due to wave-particle interactions with chorus and hiss were incorporated using electron lifetimes following Orlova and Shprits [2014] and Orlova et al. [2014]. 4. Modeling of 2 documented surface charging events detected at LANL: Smaller-scale flux variations are missing but values of modeled fluxes are close to observed ones 5. Still open issue: proper incorporation of substorm effects

Surface charging events vs. geomagnetic conditions Matéo Vélez et al., Severe geostationary environments: from flight data to numerical estimation of spacecraft surface charging, Journal of Spacecraft and Rockets, submitted, 2015