Question
Question: A research satellite of mass \(200\) kg circles the Earth in an orbit radius \(\dfrac{{3{R_E}}}{2}\)...
A research satellite of mass 200 kg circles the Earth in an orbit radius 23RE , where RE is the radius of the Earth. Assuming the gravitational pull on a mass of 1 kg on the Earth’s surface to be 10N , the pull on the satellite will be:
A) 890N
B) 889N
C) 885N
D) 892N
Solution
Gravitational pull on a mass of 1 kg on the Earth’s surface is given as 10N . Use the formula of force due to the gravitational pull of the Earth. Then divide the force of gravitational pull on mass of 1 kg with the force between Earth and satellite to get the required answer.
Complete step by step solution:
We need to find the force acting on the satellite due to the gravitational pull of the Earth. We are given the value of force on a mass of 1 kg due to gravitational pull of the Earth.
The force F acting on a body of mass m which is at a distance of RE from the centre of Earth is given as:
F=RE2GMEm
Here, ME is the mass of Earth.
Now, for a body having mass of 1 kg, this force will be:
F=RE2GME×1=RE2GME
But this force is given to be of 10N .
∴F=RE2GME=10N --equation 1
The mass of the research satellite is m=200 kg
the distance of the object from the centre of the Earth is 23RE
Therefore, the gravitational pull on the research satellite will be:
F=(23RE)2GME×200
⇒F=9800×RE2GME
But from equation 1 , we have RE2GME=10N , thus:
⇒F=9800×10
∴F=888.8N=889N
This is the pull on the satellite.
Thus, option C is the correct option.
Note: The given options are very close to the final answer, be careful while calculating the values. We were directly given the value of some constants indirectly so be careful to not put unnecessary values such as mass of Earth and the radius of radius. Instead make use of the given values this will save time and there will be less chances of calculation mistakes.