State and prove Kepler’s second law (Law of Areas) of planetary motion.
"The line that joins any planet to the sun sweeps equal areas in equal intervals of time". It is shown in figure.
The planet $P$ moves around the sun in an elliptical orbit. The shaded area is the area $\Delta \mathrm{A}$ swept out in a small interval of time $\Delta t$.
This law comes from the observations that planets appear to move slower when they are farther from the sun than when they are nearer.
The law of areas can be understood as a consequence of conservation of angular momentum which is valid for any central force.
The line of action of force which is acting on planet is passing through the sun, hence the torque of any planet $\tau=r \mathrm{~F} \sin \pi=0$. So the conservation of angular momentum of any planet remains constant.
Let the sun be at the origin and let the position and momentum of the planet be $\vec{r}$ and $\vec{p}$.
The area swept out by the planet of mass $m$ in time interval $\Delta t$ is $\Delta \mathrm{A}$.
From figure area of right triangle $\Delta S P P^{\prime}$
(Note : For $\Delta t \rightarrow 0$ )
$\Delta \mathrm{A}=\frac{1}{2} \times$ base $\times$ perpendicular
$\Delta \mathrm{A}=\frac{1}{2}(\vec{r} \times \vec{v} \Delta t)$
(Here, $\mathrm{PP}^{\prime}=\Delta \mathrm{S}=\nu \Delta t$ )
Dividing $\Delta t$ on both side of equation $(1)$,
$\frac{\Delta \overrightarrow{\mathrm{A}}}{\Delta t}=\frac{1}{2}(\vec{r} \times \vec{v})$
but momentum of planet $\vec{p}=m \vec{v}$
$\therefore \vec{v}=\frac{\vec{p}}{m}$
Given below are two statements: one is labelled as Assertion $(A)$ and the other is labelled as Reason $(R)$.
$Assertion$ $(A)$ : The angular speed of the moon in its orbit about the earth is more than the angular speed of the earth in its orbit about the sun.
$Reason$ $(R)$: The moon takes less time to move around the earth than the time taken by the earth to move around the sun.
In the light of the above statements, choose the most appropriate answer from the options given below:
The orbital speed of Jupiter is
Two satellites are launched at a distance $R$ from a planet of negligible radius. Both satellites are launched in the tangential direction. The first satellite launches correctly at a speed $v_0$ and enters a circular orbit. The second satellite, however, is launched at a speed $\frac {1}{2}v_0$ . What is the minimum distance between the second satellite and the planet over the course of its orbit?
Match List$-I$ With List$-II$
$(a)$ Gravitational constant $(G)$ | $(i)$ $\left[ L ^{2} T ^{-2}\right]$ |
$(b)$ Gravitational potential energy | $(ii)$ $\left[ M ^{-1} L ^{3} T ^{-2}\right]$ |
$(c)$ Gravitational potential | $(iii)$ $\left[ LT ^{-2}\right]$ |
$(d)$ Gravitational intensity | $(iv)$ $\left[ ML ^{2} T ^{-2}\right]$ |
Choose the correct answer from the options given below:
When a satellite moves around the earth in a certain orbit, the quantity which remains constant is :