written 7.0 years ago by | • modified 7.0 years ago |
Mumbai University > EXTC > Sem 8 > Satellite Communication and Networks
Marks: 10M
written 7.0 years ago by | • modified 7.0 years ago |
Mumbai University > EXTC > Sem 8 > Satellite Communication and Networks
Marks: 10M
written 7.0 years ago by |
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 = η (10.472 f D)2
Where η =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
Gt in Decibel =[Gt] =10 log (58900.900 =47.70 dB)
$2EIRP = PtGt / 4πr^2$
$= 100 × 58900.90/[4 × π × (35786 × 10^3)^2]$
{Assumption r =35786 km = height of geostationary satellite}
= 36.6 nW/m2
G/T = Gr/T = 58900.90/140 = 420.72
G/T 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 = 6.25GHz.