Table J-6: Parameters (appearing in Eq. (C-15) to account for modified meteoroid fluxes encountered by spacecraft in circular Earth orbits at various altitudes
|
Altitude [km] |
|
sf |
K |
|
100 |
2,04 |
0,50 |
1,09 |
|
200 |
2,03 |
0,58 |
1,09 |
|
400 |
2,00 |
0,63 |
1,09 |
|
800 |
1,94 |
0,70 |
1,08 |
|
1 000 |
1,92 |
0,72 |
1,08 |
|
2 000 |
1,81 |
0,79 |
1,08 |
|
4 000 |
1,65 |
0,87 |
1,07 |
|
10 000 |
1,41 |
0,95 |
1,05 |
|
20 000 |
1,26 |
0,98 |
1,04 |
|
35 790 (GEO) |
1,16 |
0,99 |
1,03 |
|
100 000 |
1,06 |
1,00 |
1,01 |
|
At 1 AU |
1,00 |
1,00 |
1,00 |
|
NOTE: |
|||
is the weighted mean gravitational enhancement factor for
the velocity distribution of