Digital Signal Processing Reference
In-Depth Information
A geostationary satellite is “parked” in an orbit of 35800 km above the
equator. This is the only orbit in which it can travel around the Earth syn-
chronously. At 45 o latitude, the distance from the Earth's surface is then
d = Earth's radius • sin(45°) + 35800 km = 6378 km • sin(45°)
+ 35800 km = 37938 km;
Transmitted power (e.g. Astra 1F):
Assumed transponder output power: 82 W = 19 dBW
Gain of the transmitting antenna 33 dB
Satellite EIRP (equivalent isotropic radiated power) 52 dBW
Free space attenuation:
Satellite-Earth distance = 37,938 km
91.6 dB
Transmitting frequency = 12.1 GHz
21.7 dB
Loss constant
92.4 dB
Free space attenuation
205.7 dB
Received power:
Satellite EIRP
52.0 dBW
Free space attenuation
205.7 dB
Clear sky attenuation
0.3 dB
Receiver directional error
0.5 dB
Polarisation error
0.2 dB
Received power at the antenna
-154.7 dBW
Antenna gain
37 dB
Received power
-117.7 dBW
Noise power at the receiver:
Boltzmann's constant
-228.6 dBW/K/Hz
Bandwidth = 33 MHz
74.4 dB
Temperature 20 o C = 273K+20K = 293K
24.7 dB
Noise figure of the LNB
1.0 dB
Noise power
-128.5 dBW
Carrier/noise ratio C/N:
Received power C
-117.7 dBW
Noise power N
-128.5 dBW
C/N
10.8 dB
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