Table 1 Example of some parameters and estimated spacecraft potentials at the selected point shown as a pink cross in the right panel of Fig. 7
From: Development of space environment customized risk estimation for satellites (SECURES)
Long. [deg.] | Lat. [deg.] | Density [/cc] | Temperature [keV] | Pressure [nPa] |
|---|---|---|---|---|
220.0 | − 18.0 | 1.00 | 11.1 | 1.62 |
Eclipse = 1 Daylight = 0 | Scientific satellite | Commercial satellite | ||
|---|---|---|---|---|
Surface potential Φsc[V] | Surface potential ΦMAX [V] | Frame potential ΦFRAME[V] | Differential potential [V] | |
1 | − 8700 | − 5600 | − 8100 | 2500 |