06.03.2013 Views

Propagation Effects Handbook for Satellite Systems - DESCANSO ...

Propagation Effects Handbook for Satellite Systems - DESCANSO ...

Propagation Effects Handbook for Satellite Systems - DESCANSO ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Table 6.3-2. Rain Rates Exceeded <strong>for</strong> 0.01% of the Time<br />

Climate ABCDEFG HJKLMNP<br />

Rate 8 12 15 19 22 28 30 32 35 42 60 63 95 145<br />

SteR 2 Determine the effective rain height, hr, from;<br />

hr = 4.0<br />

= 4.0 - 0.075 (<br />

+- 361 +: j6~< 36°<br />

(6.3-11)<br />

where $is the latitude of the ground station, in degrees N or S.<br />

W Calculate the slant path length? h~ horizontal Projection<br />

LG, and reduction factor, rpr from:<br />

For @ ~ 5°,<br />

= (h r - hO)/sin (@) (6.3-12)<br />

LG = L~ COS (@) (6.3-13)<br />

rp (6.3-14)<br />

1 + 0.~45LG<br />

where @ is the elevation angle to the satellite~ in degrees~ and ho<br />

is the height above mean sea level of the ground terminal location~<br />

in km. (For elevation angles less then 5°~ see Section 306).<br />

Step 4 Obtain the specific attenuation coefficients~ K anda, at the<br />

frequency and polarization angle of interest from Table 6.3-3. For<br />

frequencies not on the table, use logarithmic interpolation <strong>for</strong> K<br />

and linear interpolation <strong>for</strong> a. For polarization tilt angles other<br />

than linear horizontal or vertical, use the relationships on Figure<br />

6.3-6, Step 4, to obtain K and a.<br />

Step 5 Calculate the attenuation exceeded lar 0.01% of an average<br />

year from;<br />

Ao,o1 = K Ro.01~ LS r p (6.3-15)<br />

6-34

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!