Attenuations | -267.9dB |
TX antenna gain | 69.8 dBi |
Transmit power | 4kW [1] |
36 dBW | |
RX antenna gain | 40.7 dBi |
Received power | -130.2 dBW |
Noise power | -152 dBW |
System noise temp. | 150 K |
CNR | 21.8 dB |
Attenuations | -227.9 dB |
TX antenna gain | 42.0 dBi |
Transmit power | 200 W |
23.0 dBW | |
RX antenna gain | 71.0 dBi |
Received power | -141.9 dBW |
Noise power | -152 dBW |
System noise temp. | 150 K |
CNR | 10.1 dB |
The satellite antenna has 1.3 meters of diameter with efficiency 0.6. The DSN antenna has 34 meters diameter with efficiency 0.7. The antenna gain G of the appropriate antenna is calculated as
where
Moreover, The thermal noise power is calculated as
where k is the Boltzmann's constant, B is the bandwidth. To achieve as high CNR as possible, we employ a BPSK modulation and the half-rate turbocode. A raised-cosine filterwith roll-off factor 0.5 is used as the pulse to achieve a RF bandwidth of 300kHz.
EIRP | 277 MW / 84.4 dBW |
Dish antenna gain | 30 dBi |
RX gain | 40.7 dBi |
SNR | -48.5 dB [2] |
TX power | 23.0 dBW |
TX gain | 40.7 dBi |
SNR | -47.8 dB [2] |
EIRP | 24kW / 43.8dBW |
RX gain | 85dB |
Attenuation (10km) | -11dB |
Received power | 18.8dBW |
Noise power | -144.5dBW |
System noise temp. | 150K |
Atm. noise temp. | 740K [2] |
Recall that the attenuation over the Venusian atmosphere increases with the frequency. Hence, we chose the lower frequency spectrum to mitigate the pathloss of the signal between two VIRGILs. For calculation, the average distance between two VIRGILs at 10 km is assumed. The temperature of the Venusian atmosphere is found from Fig. 1.