Consider a satellite in stationary orbit that beams a signal earthward with a power of 4.9 kilowatts and a beamwidth covering a circular region with diameter 193 km on Earth. What is the root-mean- square electric field strength at the receiver within the illuminated area, assuming a uniform energy distribution? Use the free space permeability ln = 1.257×10-6 H/m and the free space permittivity e, = 8.85x10-12 F/m.
Consider a satellite in stationary orbit that beams a signal earthward with a power of 4.9 kilowatts and a beamwidth covering a circular region with diameter 193 km on Earth. What is the root-mean- square electric field strength at the receiver within the illuminated area, assuming a uniform energy distribution? Use the free space permeability ln = 1.257×10-6 H/m and the free space permittivity e, = 8.85x10-12 F/m.
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![Consider a satellite in stationary orbit that beams a signal earthward with a power of 4.9 kilowatts and a beamwidth covering a circular region with diameter 193 km on Earth. What is the root-mean-
square electric field strength at the receiver within the illuminated area, assuming a uniform energy distribution? Use the free space permeability lo = 1.257x10-6 H/m and the free space
permittivity eo = 8.85x10-12 F/m.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fd92556d3-4176-45e3-b375-3845edcaddf3%2F6b891c0d-591e-40bc-b446-3dc70d647a2e%2Fr1feaci_processed.png&w=3840&q=75)
Transcribed Image Text:Consider a satellite in stationary orbit that beams a signal earthward with a power of 4.9 kilowatts and a beamwidth covering a circular region with diameter 193 km on Earth. What is the root-mean-
square electric field strength at the receiver within the illuminated area, assuming a uniform energy distribution? Use the free space permeability lo = 1.257x10-6 H/m and the free space
permittivity eo = 8.85x10-12 F/m.
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