
What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 2R?
$
A.\dfrac{{5GmM}}{{6R}} \\
B.\dfrac{{2GmM}}{{3R}} \\
C.\dfrac{{GmM}}{{2R}} \\
D.\dfrac{{GmM}}{{3R}} \\
$
Answer
513.4k+ views
- Hint – In order to solve this question, firstly we will use the equation of gravitational potential energy i.e. $P.E = \dfrac{{ - Gm}}{r}$. Then we will find the kinetic energy from the total energy calculated to get the required result.
Formula used-
1) $P.E = \dfrac{{ - Gm}}{r}$
2) ${V_{orbit}} = \sqrt {\dfrac{{GM}}{R}} $
We are given that-
Mass of satellite = m
Mass of planet = M
Radius = R
Altitude h = 2R
Complete step-by-step solution -
Now, gravitational potential energy is the energy stored in an object as the result of its vertical position or height.
Using the equation of gravitational potential energy,
We get-
$P.E = \dfrac{{ - Gm}}{r}$
Potential energy at altitude$ = \dfrac{{GmM}}{{3R}}$
Orbital velocity- Orbital velocity is the velocity at which a body revolves around the other body. The velocity of orbit depends on the distance between the object and the center of the earth.
${V_{orbit}} = \sqrt {\dfrac{{GM}}{R}} $
Where mass of the body at center = M
Gravitational constant = G
Radius of the orbit = R
Here,${V_0} = \dfrac{{GmM}}{{R + h}}$
Now the total energy is-
${E_f} = \dfrac{1}{2}m{v_0}^2 - \dfrac{{GmM}}{{3R}}$
$ \Rightarrow {E_f} = \dfrac{1}{2}\dfrac{{GmM}}{{3R}} - \dfrac{{GMm}}{{3R}}$
$ \Rightarrow {E_f} = \dfrac{{GmM}}{{3R}}\left[ {\dfrac{1}{2} - 1} \right]$
$\therefore {E_f} = \dfrac{{ - GmM}}{{6R}}$
Now,${E_i} = {E_f}$ (total energy of satellite is equal to total energy of planet)
Also, the minimum required energy will be-
$K.E = \dfrac{{GmM}}{R} - \dfrac{{GmM}}{{6R}}$
$\therefore K.E = \dfrac{{5GmM}}{{6R}}$
Hence, the minimum required energy is $\dfrac{{5GmM}}{{6R}}$.
Therefore, option A is correct.
Note- While addressing this issue, we must realize that an object's gravitational potential energy is directly proportional to its height above the zero location, a doubling of the height would result in the gravitational potential energy being doubled.
Formula used-
1) $P.E = \dfrac{{ - Gm}}{r}$
2) ${V_{orbit}} = \sqrt {\dfrac{{GM}}{R}} $
We are given that-
Mass of satellite = m
Mass of planet = M
Radius = R
Altitude h = 2R
Complete step-by-step solution -
Now, gravitational potential energy is the energy stored in an object as the result of its vertical position or height.
Using the equation of gravitational potential energy,
We get-
$P.E = \dfrac{{ - Gm}}{r}$
Potential energy at altitude$ = \dfrac{{GmM}}{{3R}}$
Orbital velocity- Orbital velocity is the velocity at which a body revolves around the other body. The velocity of orbit depends on the distance between the object and the center of the earth.
${V_{orbit}} = \sqrt {\dfrac{{GM}}{R}} $
Where mass of the body at center = M
Gravitational constant = G
Radius of the orbit = R
Here,${V_0} = \dfrac{{GmM}}{{R + h}}$
Now the total energy is-
${E_f} = \dfrac{1}{2}m{v_0}^2 - \dfrac{{GmM}}{{3R}}$
$ \Rightarrow {E_f} = \dfrac{1}{2}\dfrac{{GmM}}{{3R}} - \dfrac{{GMm}}{{3R}}$
$ \Rightarrow {E_f} = \dfrac{{GmM}}{{3R}}\left[ {\dfrac{1}{2} - 1} \right]$
$\therefore {E_f} = \dfrac{{ - GmM}}{{6R}}$
Now,${E_i} = {E_f}$ (total energy of satellite is equal to total energy of planet)
Also, the minimum required energy will be-
$K.E = \dfrac{{GmM}}{R} - \dfrac{{GmM}}{{6R}}$
$\therefore K.E = \dfrac{{5GmM}}{{6R}}$
Hence, the minimum required energy is $\dfrac{{5GmM}}{{6R}}$.
Therefore, option A is correct.
Note- While addressing this issue, we must realize that an object's gravitational potential energy is directly proportional to its height above the zero location, a doubling of the height would result in the gravitational potential energy being doubled.
Recently Updated Pages
Why are manures considered better than fertilizers class 11 biology CBSE

Find the coordinates of the midpoint of the line segment class 11 maths CBSE

Distinguish between static friction limiting friction class 11 physics CBSE

The Chairman of the constituent Assembly was A Jawaharlal class 11 social science CBSE

The first National Commission on Labour NCL submitted class 11 social science CBSE

Number of all subshell of n + l 7 is A 4 B 5 C 6 D class 11 chemistry CBSE

Trending doubts
What is meant by exothermic and endothermic reactions class 11 chemistry CBSE

10 examples of friction in our daily life

One Metric ton is equal to kg A 10000 B 1000 C 100 class 11 physics CBSE

1 Quintal is equal to a 110 kg b 10 kg c 100kg d 1000 class 11 physics CBSE

Difference Between Prokaryotic Cells and Eukaryotic Cells

What are Quantum numbers Explain the quantum number class 11 chemistry CBSE

