
A research satellite of mass $200$ kg circles the Earth in an orbit radius $\dfrac{{3{R_E}}}{2}$ , where ${R_E}$ is the radius of the Earth. Assuming the gravitational pull on a mass of $1$ kg on the Earth’s surface to be $10\,N$ , the pull on the satellite will be:
A) $890\,N$
B) $889\,N$
C) $885\,N$
D) $892\,N$
Answer
221.7k+ views
Hint: Gravitational pull on a mass of $1$ kg on the Earth’s surface is given as $10\,N$ . 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 ${R_E}$ from the centre of Earth is given as:
$F = \dfrac{{G{M_E}m}}{{{R_E}^2}}$
Here, ${M_E}$ is the mass of Earth.
Now, for a body having mass of $1$ kg, this force will be:
$F = \dfrac{{G{M_E} \times 1}}{{{R_E}^2}} = \dfrac{{G{M_E}}}{{{R_E}^2}}$
But this force is given to be of $10\,N$ .
$\therefore F = \dfrac{{G{M_E}}}{{{R_E}^2}} = 10\,N$ --equation $1$
The mass of the research satellite is $m = 200$ kg
the distance of the object from the centre of the Earth is $\dfrac{{3{R_E}}}{2}$
Therefore, the gravitational pull on the research satellite will be:
$$F = \dfrac{{G{M_E} \times 200}}{{{{\left( {\dfrac{3}{2}{R_E}} \right)}^2}}}$$
$$ \Rightarrow F = \dfrac{{800}}{9} \times \dfrac{{G{M_E}}}{{{R_E}^2}}$$
But from equation $$1$$ , we have $\dfrac{{G{M_E}}}{{{R_E}^2}} = 10\,N$ , thus:
$$ \Rightarrow F = \dfrac{{800}}{9} \times 10$$
$$ \therefore F = 888.8\,N = 889\,N$$
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.
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 ${R_E}$ from the centre of Earth is given as:
$F = \dfrac{{G{M_E}m}}{{{R_E}^2}}$
Here, ${M_E}$ is the mass of Earth.
Now, for a body having mass of $1$ kg, this force will be:
$F = \dfrac{{G{M_E} \times 1}}{{{R_E}^2}} = \dfrac{{G{M_E}}}{{{R_E}^2}}$
But this force is given to be of $10\,N$ .
$\therefore F = \dfrac{{G{M_E}}}{{{R_E}^2}} = 10\,N$ --equation $1$
The mass of the research satellite is $m = 200$ kg
the distance of the object from the centre of the Earth is $\dfrac{{3{R_E}}}{2}$
Therefore, the gravitational pull on the research satellite will be:
$$F = \dfrac{{G{M_E} \times 200}}{{{{\left( {\dfrac{3}{2}{R_E}} \right)}^2}}}$$
$$ \Rightarrow F = \dfrac{{800}}{9} \times \dfrac{{G{M_E}}}{{{R_E}^2}}$$
But from equation $$1$$ , we have $\dfrac{{G{M_E}}}{{{R_E}^2}} = 10\,N$ , thus:
$$ \Rightarrow F = \dfrac{{800}}{9} \times 10$$
$$ \therefore F = 888.8\,N = 889\,N$$
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.
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