written 5.6 years ago by
teamques10
★ 68k
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modified 5.6 years ago
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Data:
Output power Pt =100 W
Diameter of transmitter antenna =5m
Diameter of receiver antenna =5m
Transmission frequency = 6.25GHz
System noise temeperature =140 K
To find: EIRP (Equivalent/Effective Isotropic Radiated Power), G/T Ratio
Solution:
Gain of transmitter antenna = $Gt = \eta (10.472 f D)^2$
Where $\eta$ = antenna radiation efficiency = 0.55 (Assumption)
f = frequency in GHz
D = diameter of antenna in meter
$Gt = 0.55 (10.472 × 6.25 × 5)^2 = 58900.90$
$\text{Gt in Decibel} = [Gt] = 10 \ log (58900.900) = 47.70 dB $
$ 2EIRP = \frac{PtGt}{4 \pi r^2} = \frac{100 \times 58900.90 }{4×π×(35786×103)^2} $
{Assumption r = 35786 km = height of geostationary satellite}
$2EIRP = 36.6 n W/m^2$
$G/T =Gr/T = \frac{58900.90}{140} = 420.72$
$G/T \text{ in decibel} = [G/T] =10 \ log (420.72) = 26.23 dB$
Note: In this numerical the receiving frequency 4.5 GHz is mentioned but $G/T$ ratio is always calculated at satellite antenna where the received frequency is same as transmitting frequency = 6.25 GHz.