SHELLS-hires
Version: 1The SHELLS electron radiation belt model was developed to easily and accurately describe the near-Earth electron flux environment both in real time and retrospectively in order to monitor and analyze space weather impacts to satellites on-orbit. The high energy electrons modeled by SHELLS can penetrate through satellite shielding and build up charge in dielectric materials and on spot shields sometimes resulting in a sudden electrical discharge that triggers anomalous satellite behavior. The model specifies electron flux at high altitude locations (L=3-6.3 and a range of near equatorial and off equatorial magnetic field values) by mapping electron fluxes measured at low altitudes (~850 km) by the POES/MetOp satellite constellation using a neural network derived algorithm.
Inputs
SHELLS is driven by near real time measurements of low altitude electron fluxes and the Kp-index. More specifically, it uses the log10 of the integral electron fluxes measured by the MEPED instruments along each complete pass of a POES/MetOp satellite through the radiation belts (L=3-8). The data from each pass are binned into .25 L shell bins that are then mapped to a consistent longitude and hemisphere using statistical asynchronous regression to remove orbital variations (see Green et al. [2021] for details on the input data processing). Additionally, it uses the Kp index and the maximum Kp index in the last 3 days (here Kp is the standard index multiplies by 10)
Outputs
The general output of the SHELLS model is electron fluxes (#/cm2-s-str-keV) from L=3-6.3 and energies from 200-3000 keV with local pitch angles from 0-90 degrees.
The SHELLS model provides 2 different real time run products. One is a dataset of electron flux along the trajectory of a GPS satellite. The output for this GPS product is a text file and L binned plots of the electron fluxes for the last 25 days. The output files contain time at a 5-minute cadence, the L shell based on the OP Quiet field (L), the flux (columns called E flux xxx keV) of electrons with local 90-degree pitch angle and energies 200,500,800,1000,2000 keV, the upper and lower quartiles of the flux (columns labeled upper q and lower q), and the local B field from the OP Quiet field model.
The other dataset contains near equatorial electron flux at a fixed set of L-shells (3,3.5,4,4.5,5,5.5,6) and energies (200-3000 at a 200keV step). The daily JSON files update every hour and contain data at a 1-hour times cadence. The values included in the JSON file are time, Eflux[time,Ls,energy], L[time,L], Bmirror[time,L], upper q[time,L,energy], lower q[time,L,energy], Kp[time], and Kp max[time]. Here upper q is the upper quartile of the electron flux and lower q is the lower quartile. Kp is the Kp index and Kp max is the maximum in the prior 3 days.
Model is time-dependent.
Domains
- Magnetosphere / Inner Magnetosphere / RadiationBelt
Space Weather Impacts
- Near-earth radiation and plasma environment (aerospace assets functionality)
Phenomena
- Particle Dynamics
- Seed Population for the Ring Current and Radiation Belt / Preconditioning
Publications
- Claudepierre, S.G., & O'Brien, T. P. (2020). Specifying high-altitude electrons using low-altitude LEO systems: The SHELLS model. Space Weather, 18, e2019SW002402. https://doi.org/10.1029/2019SW002402
- Green, J. C., O’Brien, T. P., Claudepierre, S. G., & Boyd, A. J. (2021). Removing orbital variations from low altitude particle data: Method and application. Space Weather, 19, e2020SW002638. https://doi.org/10.1029/2020SW002638
- Boyd, A. J., Green, J. C., O’Brien, T. P., & Claudepierre, S. G. (2023). Specifying high altitude electrons using low-altitude LEO systems: Updates to the SHELLS model. Space Weather, 21, e2022SW003338. https://doi.org/10.1029/2022SW003338
Code
Code Languages: Python
Contacts
- Janet Green, Space Hazards Applications, LLC (Model Developer)
- Paul O'Brien, Aerospace Corp (Model Developer)
- Yihua Zheng, NASA GSFC CCMC (CCMC Model Host)
Publication Policy
In addition to any model-specific policy, please refer to the General Publication Policy.