By Nuclear and Space Radiation Effects Conference Short Course 1997
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Extra resources for Applying Computer Simulation Tools to Radiation Effects Problems
The figure shows that the variations in fluence level due to spacecraft orbit reach orders of magnitude. I-35 In general, the greatest inclination dependencies occur in the range of 0° c i c 30°, For inclinations gradually until about 60°. Over 60°, increasing inclination over 30°, the fluxes rise more has little effect on the proton flux levels. The largest altitude variations occur between 200 to 600 km where large increases in flux levels are seen as altitude rises. altitude is more gradual.
Note the penetrationat high energies. 8: ProtonLET valuesare insufficient particles produced by to cause single eventevents in deviceswith high LET thresholds. which have LETs high enough to cause SEES. Therefore, instead of proton LET, it is necessary to evaluate the ability of the primary proton to produce the secondary particles. This is determined by the energy of the proton, therefore, energy-flux spectra are used to define the proton single event upset hazard. g. the 1773 fiber optic data bus ).
As energy increases, the period decreases because of the greater relativistic mass. 1 second for 1 MeV electrons. It takes about 1/2 hour for 1 MeV protons to complete an azimuthal drift cycle at 1000 km and about 1 hour for electrons. of magnitude, the three motions Because the frequencies are of different orders are “uncoupled”. 1. The best way to characterize theoretical and model the trapped radiation environment approaches and experimental measurements. To simplify theoretical is to combine descriptions, a *Electricalfields are importantin high-latitudeevents and auroralphenomenabut me not steady,long-livedfeatures of the trappedregion.
Applying Computer Simulation Tools to Radiation Effects Problems by Nuclear and Space Radiation Effects Conference Short Course 1997
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