a. For auroral charging assessment, the following worstcase electron distribution function shall be used.
¾ For E ≤17,44 keV:
|
f(v) = 3,9 × 10-18 s3m-6 |
(8‑1) |
¾ For E > 17,44:
|
|
(8‑2) |
where
f(v) is the distribution function in sec3 m-6
N0 is the density in m-3
me is the electron mass in kg
kT0 is the thermal energy in J
E0 is in J
E is energy in J
and parameters of the worst case environment are:
N0 = 1,13E6 m-3
kT0 = 3,96 keV
E0 = 17,44 keV
NOTE This comes from [RD.7] and is based on work described in [RD.8]. Unfortunately, it is printed in [RD.7] with a typographical error.
b. For worst case auroral charging assessments, a thermal ion density of 125 cm-3 and temperature 0,2 eV shall be used.
NOTE This low ion density comes from a severe charging case seen on the DMSP spacecraft by [RD.9]. Measuring ionospheric thermal ion density during a strong charging event is potentially prone to errors because of the way the charged satellite alters ion trajectories, so there is a degree of uncertainty in this measurement.