Table D-1: Degree power attenuation for an orbit at 25 000 km altitude
|
degree l |
Kaula signal power for this degree |
attenuation factor at H=25 000 km |
remaining signal power at H=25 000 km |
|
2 |
2,500E-06 |
6,250E-02 |
1,563E-07 |
|
3 |
1,111E-06 |
1,563E-02 |
1,736E-08 |
|
4 |
6,250E-07 |
3,906E-03 |
2,441E-09 |
|
5 |
4,000E-07 |
9,766E-04 |
3,906E-10 |
|
6 |
2,778E-07 |
2,441E-04 |
6,782E-11 |
|
7 |
2,041E-07 |
6,104E-05 |
1,246E-11 |
|
8 |
1,563E-07 |
1,526E-05 |
2,384E-12 |
|
9 |
1,235E-07 |
3,815E-06 |
4,710E-13 |
|
10 |
1,000E-07 |
9,537E-07 |
9,537E-14 |
|
12 |
6,944E-08 |
5,960E-08 |
4,139E-15 |
|
15 |
4,444E-08 |
9,313E-10 |
4,139E-17 |
|
20 |
2,500E-08 |
9,095E-13 |
2,274E-20 |
|
50 |
4,000E-09 |
7,889E-31 |
3,155E-39 |
|
100 |
1,000E-09 |
6,223E-61 |
6,223E-70 |
|
360 |
7,716E-11 |
1,813E-217 |
1,399E-227 |