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3.Calculation of Transmit EIRP (in dB
W)&operating FD
1. Transmit
power per carrier It
is the power given to the antenna at the Earth station to
radiate power. Its range lice in the watts.
2. Transmitter feeder
loss Losses will occur in the connection between the
transmitting antenna and the transmitter proper. Such losses will occur in the
connecting wave-guides, filters and couplers.
3.Antenna pointing loss
When a satellite link is established, the ideal
situation is to have the earth station and satellite antennas aligned for
maximum gain. There are two possible sources of off axis loss , one at the
satellite and one at the earth station . The off axis loss at the satellite is
taken in to account by designing the link for operation on actual satellite
antenna contour. The off axis losses at the earth station is referred to as the
antenna pointing loss.
Antenna pointing losses are usually only a few
tenths of a decibel.
4. No of carriers
By frequency
multiplexing scheme we can transmit any number of carriers through an antenna.
5.Transmit EIRP This is the product of actual
power given to transmitting antenna and antenna power gain of transmitting
antenna.
That the equivalent isotropic
power (EIRP) may be defined as
EIRP=PTGT
EIRP is often expressed in
decibels relative to 1 watt, or dBW. Let Pt be in Watts then
EIRP = [PT]+[GT] dBW
If we consider transmitter feeder
loss & antenna pointing loss in to account
Transmitter EIRP= 10 log
(Transmitter power per carrier )-Transmitter Feeder loss +
Transmitter antenna gain antenna pointing loss
(db
W)
..[3]
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Example
Calculation of transmit
EIRP for an antenna having the following data. Transmit power per carrier- 0.28 W, antenna feeder
loss-1.00 dB, antenna pointing loss-0.70 dB And transmitter antenna gain
45.21dB.
Solution
Transmit EIRP = 10 log (0.28)-1 + 45.21- 0.70
= 37.98 dB
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6.Satellite operating flux density (dB /Sq m)
The traveling tube amplifier in a satellite transponder
exhibits power output saturation. The flux density required in the receiving
antenna to produce saturation of the TWTA is termed the saturation flux
density.
Satellite operating flux density = Transmitter EIRP Up
link Rain attenuation 162.2
(dB /Sq m)
.[4]
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Example
: calculate satellite operating flux density (dB /Sq m)for the
satellite having EIRP 37.98 dB and no rain attenuation .
Solution
Satellite operating
flux density dB/Sq m = 37.98- 162.2
= -124.21 dB/Sq m
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7. Amplifier back off
To reduce inter-modulation distortion, the operating point
of the TWT must be shifted to the linear portion of the curve, the reduction in
input power being referred as input back off. When multiple carriers present,
the power around saturation, for any carrier, is somewhat less than the achieved
with single carrier operation.
The input
back-off is the difference in decibels between the carrier input at the
operating point, and saturation input that would be required for single carrier
operation.
8.Power
rating of ground transmitter
It the power
delivered by the ground transmitter. Power rating
of ground transmitter can be
expressed as
Power rating
of ground transmitter =10((10 log (Number of carriers * Power per
carrier)+amplifier backoff)/10)
.[5]
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Example : calculate power rating of ground
transmitter operating at following conditions. Number of carriers- 1, Power per carrier- 0.28 W,
Amplifier back off-0 dB.
Solution
Power rating of ground transmitter
= 10((10 log
(Number of carriers * Power per carrier)+amplifier backoff)/10)
= 0.28 W
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