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Chapter 4 Solution to Problems

Chapter 4 Solution to Problems

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A satellite in GEO orbit is a distance of 39,000 km from an earth station. The required flux density at the satellite to saturate one transponder at a frequency of 14.3 GHz is -90.0 dBW/m2. The earth station has a transmitting antenna with a gain of 52 dB at 14.3 GHz. Find: a. The EIRP of the earth station Answer: EIRP = Pt + Gt = Pt + 52 dBW 3 ...

  Chapter, Satellite

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