Question #37827

Given:G= 6.67259×10E−11Nm2/kg2.
A 1520 kg geosynchronous satellite or-
bits a planet similar to Earth at a radius
1.93×10E5
km from the planet’s center. Its
angular speed at this radius is the same as the
rotational speed of the Earth, and so they ap-
pear stationary in the sky. That is, the period
of the satellite is 24 h
.
What is the force acting on this satellite?

Expert's answer

Answer on Question #37827- Physics – Astronomy | Astrophysics

Given: G = 6.67259×10E−11Nm2/kg2. A 1520 kg geosynchronous satellite orbits a planet similar to Earth at a radius 1.93×10E5 km from the planet's center. Its angular speed at this radius is the same as the rotational speed of the Earth, and so they appear stationary in the sky. That is, the period of the satellite is 24 h. What is the force acting on this satellite?

Solution

The orbit of satellite is stationary. Whence we get that the gravitational force GMmr2\frac{GMm}{r^2} is equal to sum of centrifugal force mω2rm\omega^2 r and some force FF. Here G=6.672591011m3kgs2G = 6.67259 \cdot 10^{-11} \frac{m^3}{kg \cdot s^2} is gravitational constant, M=5,9721024kgM = 5,972 \cdot 10^{24} kg is mass of planet (mass of Earth),


r=1.93105km=1.93108mr = 1.93 \cdot 10^5 \, \text{km} = 1.93 \cdot 10^8 \, \text{m}


is radius of satellite's orbits, ω=2πT=2π24h=7.272105rad/s\omega = \frac{2\pi}{T} = \frac{2\pi}{24h} = 7.272 \cdot 10^{-5} \, \text{rad/s}

angular speed of satellite on orbit, T=24h=86400sT = 24h = 86400 \, \text{s}

is period of one revolution around Earth, m=1520kgm = 1520 \, \text{kg}

is mass of satellite.


GMmr2=F+mω2r\frac{GMm}{r^2} = F + m\omega^2 rF=GMmr2mω2rF = \frac{GMm}{r^2} - m\omega^2 rF=1535.09NF = -1535.09 \, \text{N}

Answer:

F=1535.09NF = -1535.09 \, \text{N}, force is acting to the center of planet.

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