CBSE Class 11 Physics • Chapter 07
Chapter Overview: This chapter explores the fundamental force of Gravitation. We will study Kepler's Laws of Planetary Motion, Newton's Universal Law, Acceleration due to Gravity ($g$), Gravitational Potential Energy, and the physics of Satellites.
Figure 7.1: Kepler's Laws (Elliptical Orbit & Equal Areas)
Q: The distance of two planets from the Sun are $10^{13} \text{ m}$ and $10^{12} \text{ m}$ respectively. Find the ratio of their time periods.
Ans: Using Kepler's Law $T^2 \propto R^3$:
$\frac{T_1^2}{T_2^2} = \frac{R_1^3}{R_2^3} = \left(\frac{10^{13}}{10^{12}}\right)^3 = (10)^3 =
1000$.
$\frac{T_1}{T_2} = \sqrt{1000} = 10\sqrt{10} \approx \mathbf{31.6}$.
Figure 7.2: Gravitational Force between two masses
Statement: Every body in the universe attracts every other body with a force which is directly proportional to the product of their masses and inversely proportional to the square of the distance between them.
$$ F = G \frac{m_1 m_2}{r^2} $$
Where $G = 6.67 \times 10^{-11} \text{ Nm}^2\text{kg}^{-2}$ (Universal Gravitational Constant).
Note: Gravitational force is a central force (acts along the line joining centers) and is conservative in nature.
Figure 7.3: Variation of g with distance r from center
The acceleration produced in a body due to the gravitational force of the earth.
$$ g = \frac{GM}{R^2} $$
At Earth's surface, $g \approx 9.8 \text{ m/s}^2$.
Figure 7.3a: Geometry for Variation of g with Height and Depth
Step 1: Start with the formula for g at the surface of the Earth.
$$ g = \frac{GM}{R^2} \quad \text{...(i)} $$
Step 2: At a height $h$ above the surface, the distance from the center is $(R+h)$. Let the acceleration due to gravity be $g_h$.
$$ g_h = \frac{GM}{(R+h)^2} \quad \text{...(ii)} $$
Step 3: Divide equation (ii) by (i):
$$ \frac{g_h}{g} = \frac{\frac{GM}{(R+h)^2}}{\frac{GM}{R^2}} = \frac{R^2}{(R+h)^2} = \frac{R^2}{R^2(1+\frac{h}{R})^2} = \left(1 + \frac{h}{R}\right)^{-2} $$
Step 4: Apply Binomial Expansion for $h \ll R$ (neglecting higher order terms):
$$ \left(1 + \frac{h}{R}\right)^{-2} \approx 1 - \frac{2h}{R} $$
Conclusion: The value of g decreases linearly with height for small altitudes.
Step 1: Assume Earth is a uniform sphere of density $\rho$. Mass $M = \text{Volume} \times \rho$.
$$ M = \frac{4}{3}\pi R^3 \rho $$
$$ \therefore g = \frac{GM}{R^2} = \frac{G}{R^2} \left(\frac{4}{3}\pi R^3 \rho\right) = \frac{4}{3}\pi G R \rho \quad \text{...(i)} $$
Step 2: At depth $d$, the body is at a distance $(R-d)$ from the center. Only the inner sphere of radius $(R-d)$ exerts a net gravitational force. The outer shell's force cancels out.
Mass of inner sphere $M' = \frac{4}{3}\pi (R-d)^3 \rho$.
$$ g_d = \frac{GM'}{(R-d)^2} = \frac{G}{(R-d)^2} \left(\frac{4}{3}\pi (R-d)^3 \rho\right) = \frac{4}{3}\pi G (R-d) \rho \quad \text{...(ii)} $$
Step 3: Divide (ii) by (i):
$$ \frac{g_d}{g} = \frac{\frac{4}{3}\pi G (R-d) \rho}{\frac{4}{3}\pi G R \rho} = \frac{R-d}{R} = 1 - \frac{d}{R} $$
Conclusion: $g$ decreases with depth. At center ($d=R$), $g_d = 0$.
Q: At what height above the earth's surface does the value of $g$ become half of its value on the surface? ($R = 6400 \text{ km}$)
Ans: $g_h = g \frac{R^2}{(R+h)^2}$. given $g_h = g/2$.
$\frac{1}{2} = \frac{R^2}{(R+h)^2} \Rightarrow \frac{1}{\sqrt{2}} = \frac{R}{R+h}$.
$R+h = \sqrt{2}R \Rightarrow h = (\sqrt{2}-1)R = 0.414 \times 6400 \approx \mathbf{2650 \text{ km}}$.
Figure 7.3b: Work done in bringing mass m from Infinity to P
Definition: Gravitational Potential Energy at a point is the amount of work done in bringing a body of mass $m$ from infinity to that point without acceleration.
Proof:
Consider a body of mass $m$ at a distance $x$ from Earth (Mass $M$). The Gravitational Force is:
$$ F = \frac{GMm}{x^2} $$
Work done to move it by a small distance $dx$ towards the Earth (force and displacement are in same direction):
$$ dW = F \cdot dx = \frac{GMm}{x^2} dx $$
Total work done in bringing the body from infinity ($x = \infty$) to a point $P$ at distance $r$ ($x = r$) is obtained by integration:
$$ W = \int_{\infty}^{r} \frac{GMm}{x^2} dx $$
$$ W = GMm \int_{\infty}^{r} x^{-2} dx = GMm \left[ \frac{x^{-1}}{-1} \right]_{\infty}^{r} $$
$$ W = -GMm \left[ \frac{1}{x} \right]_{\infty}^{r} = -GMm \left( \frac{1}{r} - \frac{1}{\infty} \right) $$
Since this work is stored as potential energy ($U = W$):
Note: The negative sign indicates that the potential energy decreases as the body moves closer to the Earth, and the force is attractive.
Q: Find the potential energy of a body of mass $m$ at a height of $h = R$ from the surface of earth.
Ans: Distance from center $r = R + h = R + R = 2R$.
$U = - \frac{GMm}{2R} = - \frac{1}{2} mgR$ (Since $GM/R^2 = g, GM/R = gR$).
Figure 7.3c: Projectile launch for Escape Velocity
Definition: The minimum velocity required to project a body vertically upwards from the surface of earth so that it escapes the gravitational field of earth.
Proof (Work-Energy Theorem):
Let a body of mass $m$ be projected with velocity $v_e$ from the surface of Earth ($R$).
1. Kinetic Energy given at surface: $K = \frac{1}{2}mv_e^2$
2. Work done by gravity as body moves from surface ($R$) to infinity ($\infty$) is negative of PE change, or we can say work done against gravity to reach infinity:
$$ W = \int_{R}^{\infty} \frac{GMm}{x^2} dx = GMm \left[ -\frac{1}{x} \right]_{R}^{\infty} $$
$$ W = -GMm \left( \frac{1}{\infty} - \frac{1}{R} \right) = \frac{GMm}{R} $$
For escape, Initial Kinetic Energy $\ge$ Work Required to escape:
$$ \frac{1}{2}mv_e^2 = \frac{GMm}{R} $$
$$ v_e^2 = \frac{2GM}{R} \Rightarrow v_e = \sqrt{\frac{2GM}{R}} $$
Since $g = \frac{GM}{R^2} \Rightarrow GM = gR^2$, we can substitute:
For Earth, $g=9.8, R=6.4\times 10^6 \Rightarrow v_e \approx 11.2 \text{ km/s}$.
Figure 7.4: Satellite in Orbit (Circular Path)
Principle: For a satellite to orbit in a circular path, the Gravitational force provides the necessary Centripetal force.
From Figure 7.4:
$$ F_G = F_C $$
$$ \frac{GMm}{r^2} = \frac{mv_o^2}{r} $$
Where $r = R + h$. Canceling $m$ and one $r$:
$$ \frac{GM}{r} = v_o^2 \Rightarrow v_o = \sqrt{\frac{GM}{r}} $$
Since $g = GM/R^2 \Rightarrow GM = gR^2$, and near surface $r \approx R$:
Time Period is the time taken to complete one revolution.
$$ T = \frac{\text{Circumference}}{\text{Orbital Speed}} = \frac{2\pi r}{v_o} $$
Substituting $v_o = \sqrt{GM/r}$:
Squaring both sides gives Kepler's Third Law ($T^2 \propto r^3$).
1. Potential Energy (U): $U = -\frac{GMm}{r}$
2. Kinetic Energy (K): $K = \frac{1}{2}mv_o^2$. Substituting $v_o^2 = GM/r$:
$$ K = \frac{1}{2}m \left(\frac{GM}{r}\right) = \frac{GMm}{2r} $$
3. Total Energy (E): $E = K + U$
Note: Total energy is negative, implying the satellite is bound to Earth.
Q: A satellite revolves very near to the earth's surface. Its orbital velocity is...
Ans: $v_o = \sqrt{gR} = \sqrt{9.8 \times 6.4 \times 10^6} \approx \mathbf{7.92 \text{ km/s}}$.
Geostationary Satellite:
Polar Satellite:
Question: Why does an astronaut feel weightless inside a satellite?
Ans: The satellite and the astronaut are both in a state of free fall towards the Earth with the same acceleration ($g' = v^2/r$). The normal reaction force between the astronaut and the satellite floor becomes zero ($N = m(g - a) = 0$). Hence, weightlessness is felt.
Question: Derive the expression for the total energy of a satellite orbiting the earth.
Ans: Kinetic Energy $K = \frac{1}{2}mv^2 = \frac{1}{2} \frac{GMm}{r}$.
Potential Energy $U = - \frac{GMm}{r}$.
Total Energy $E = K + U = \frac{GMm}{2r} - \frac{GMm}{r} = \mathbf{-\frac{GMm}{2r}}$.
Negative sign implies the satellite is bound to the Earth.