Presentation Transcript
SAMPEX/PET proton model : SAMPEX/PET proton model D. Heynderickx1, M.D. Looper2, J.B. Blake2
1BIRA, Belgium
2Aerospace Corp., U.S.A.
Overview : Overview Variability of the low altitude trapped proton environment
Strengths and shortcomings of AP-8
SAMPEX mission and PET instrument
New model development
Coordinate system
Data binning
Solar cycle dependence and seasonal variations
Sample model outputs and comparison to AP-8
Work to do
Model software and distribution issues
Low altitude proton flux variations : Low altitude proton flux variations Geomagnetic secular variation
Solar cycle activity
Solar proton events
Changes in atmospheric density
AP-8 strengths and shortcomings : AP-8 strengths and shortcomings Strengths
Widely known and used, integrated in existing applications
Provides (nearly) full energy range 100 keV – 400 MeV
Provides complete spatial coverage
Reasonably straightforward to use with TRARA
Shortcomings
No updates since 1970; would be very difficult to do
No real solar cycle dependence
No error bars ('probably a factor of two')
TRARA doesn’t work well at low altitude
SAMPEX mission : SAMPEX mission SMEX mission
Launched in 1992
Still operational?
Orbit: 520 x 670 km, 82º, Sun pointing
3 month periodicity in orbit configuration
Most of the time in non-spinning mode
For this study: proton/electron telescope (PET)
Proton/Electron Telescope : Proton/Electron Telescope Array of Si solid state detectors
Passive shielding + anti-coincidence through guard rings
dE/dx – total energy technique + coincidence logic -andgt; 15 channels
Opening angle: 58º -andgt; large geometric factor
Counts and livetimes over 6s are stored because of telemetry limits
PET Channels : PET Channels
Coordinate system : Coordinate system (B,L) type coordinates not well suited for low altitudes
Alternatives: Kaufmann K = I√B; minimum altitude on drift shell
Proton flux time series : Proton flux time series Monthly averages + F10.7
Averages + inverse F10.7
Averages + inverse F10.7 + inverse MSIS atmospheric density
Solar cycle dependence : Solar cycle dependence Monthly averages grouped by month
Hysteresis effect
Different behaviour for descending and ascending phases
Two separate fits work better
Seasonal variations : Seasonal variations Annual variation of F10.7 fit parameters (coloured lines)
Sine fit with fraction of year (black lines)
MSIS total mass density
Inverse density
Model fluxes : Model fluxes Fit was applied to all energy, K and hmin bins
Model consists of tables of fit coefficients
Slide13 :
Work to do : Work to do Further validation of fitting procedure
Smoothing in (hmin,K) plane
Spectrum fits
Elimination of data contaminated by SEP events
Validation with AZUR, CRRES, … data
Final model format : Final model format Presently: tabel of sine fit coefficients for (E,hmin,K,F10.7,DOY)
Sine fit parameters are extracted from (E,hmin,K) bin
DOY is used with sine fit to generate coefficients for parabolic F10.7 function
F10.7 function yields flux
Energy dependence could also be fitted
Low altitude proton model is probably not far away from standardization
Software and distribution issues : Software and distribution issues Software implementation
Currently in IDL, will be ported to Fortran
Stand-alone version for use with SPENVIS
'library' type version as a subroutine callable from IDL, Fortran, C, …
Distribution
Model source code and coefficients on web site, downloadable after user identification
Regular updates when new data become available or fitting improves; notification of registered users
Code for calculating magnetic coordinates must be available as well (UNILIB, …)
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