A geostationary satellite is a satellite that is always at a fixed position with respect to any position on the planet, i.e. as the planets rotate around their axis, the satellite rotates at the same angular rate as the the planet. The planet Mercury has a radius r= 2.44x10° m and a mass m=3.301× 1023 kg. An average solar day

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A geostationary satellite is a satellite that is
always at a fixed position with respect to any
position on the planet, i.e. as the planets
rotate around their axis, the satellite rotates
at the same angular rate as the the planet.
The planet Mercury has a radius
r= 2.44×10° m and a mass
m = 3.301× 1043 kg. An average solar day
on the planet Mercury is T= 1408 h. A
geostationary satellite of m, = 33775 kg is
at a height h = 2.405×10° m. (Use
%3D
N m2
for the
G = 6.674×10-11
kg2
gravitational constant).
1. Calculate the the average speed of the
geostationary satellite on its orbit
around the planet: V =
2. Calculate the centripetal acceleration
of the satellite at this height? a.=
3. What is the magnitude of the
centripetal force on the satellite?
F =
4. What is the magnitude of the
gravitational force on the satellite?
F =
Transcribed Image Text:A geostationary satellite is a satellite that is always at a fixed position with respect to any position on the planet, i.e. as the planets rotate around their axis, the satellite rotates at the same angular rate as the the planet. The planet Mercury has a radius r= 2.44×10° m and a mass m = 3.301× 1043 kg. An average solar day on the planet Mercury is T= 1408 h. A geostationary satellite of m, = 33775 kg is at a height h = 2.405×10° m. (Use %3D N m2 for the G = 6.674×10-11 kg2 gravitational constant). 1. Calculate the the average speed of the geostationary satellite on its orbit around the planet: V = 2. Calculate the centripetal acceleration of the satellite at this height? a.= 3. What is the magnitude of the centripetal force on the satellite? F = 4. What is the magnitude of the gravitational force on the satellite? F =
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