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Question: The motion of a planet around the sun in an elliptical orbit is shown in the following figure. Sun i...

The motion of a planet around the sun in an elliptical orbit is shown in the following figure. Sun is situated in one focus. The shaded areas are equal. If the planet takes time t1{t_1} and t2{t_2} in moving from AA to BB and from CC to DD respectively then
(A) t1>t2{t_1} > {t_2}
(B) t1<t2{t_1} < {t_2}
(C) t1=t2{t_1} = {t_2}
(D) information incomplete

Explanation

Solution

Kepler’s law is applicable for the motion of the planet which moves around the centre of gravity, sun. use this law to solve this problem. Rearranging the Kepler’s law and substituting both the areas are the same provides the relation between the time taken.
Useful formula:
The formula of the Kepler’s law of planetary motion is given by
dAdt=constant\dfrac{{dA}}{{dt}} = {\text{constant}}
t1=t2{t_1} = {t_2}Where dAdA is the change in the area and dtdt is the change in the time taken to cover the area.

Complete step by step solution:
It is given that the Sun is the centre of the focus for the Earth to rotate in the elliptical path. From the given diagram and the given data, the shaded areas of ABAB and CDCD are the same. The time taken to cover the area of ABAB is t1{t_1} and the time taken to cover the area of CDCD is t2{t_2} .
Let us consider Kepler's law of the area of planetary motion. This law states that the line joining the sun and the planet will cover an equal area in the certain interval of time. This can also be said as the area velocity is constant.
dAdt=constant A1t1=A2t2 t1=A1A2t2  \dfrac{{dA}}{{dt}} = {\text{constant}} \\\ \dfrac{{{A_1}}}{{{t_1}}} = \dfrac{{{A_2}}}{{{t_2}}} \\\ {t_1} = \dfrac{{{A_1}}}{{{A_2}}}{t_2} \\\
Since the areas covered by both the lines are same, then A1=A2{A_1} = {A_2}
t1=t2{t_1} = {t_2}
Hence the time taken will also be equal for both the areas.

Thus the option (C) is correct.

Note: Let us see the derivation of the Kepler’s law used in the above solution. It is known that the L=mAtL = \dfrac{{mA}}{t} , bringing mm to left hand side of the equation, we get, Lm=At\dfrac{L}{m} = \dfrac{A}{t} . Since the sun is the centre of gravity, the angular momentum is constant. The mass is also constant. So the LHSLHS is also constant. Hence At=constant\dfrac{A}{t} = {\text{constant}} .