Chapter 7 โ Gravitation
One force holds you to the ground, keeps the Moon in its orbit and steers the planets round the Sun. This chapter finds its law and uses it to weigh the Earth, launch satellites and escape into space.
An apple falls from a branch. The Moon, $384\,000\ \text{km}$ away, sails on round the Earth and never comes down. Mars wanders across the night sky, now forwards, now backwards. For most of history these looked like three quite different things โ earthly objects fall, heavenly ones go round. The great discovery of the seventeenth century was that they are the same thing: the Moon is falling too, all the time, but it is moving sideways so fast that it keeps missing the Earth.
This chapter follows that idea from the sky to the launch pad. You will start with Kepler's three laws, distilled from years of careful observation of the planets, and see how Newton explained all of them with one law of universal gravitation and one constant, $G$. Then you will bring the law down to Earth: where the value $g=9.8\ \text{m/s}^2$ comes from, how it weakens up a mountain and down a mine, and how it lets you calculate the mass of the Earth. Finally you will replace $mgh$ with a potential energy that works at any distance, and use it to find how fast a rocket must go to escape the Earth, how fast a satellite must move to stay in orbit, and how much energy it holds there.
- state Kepler's three laws, use $r_p=a(1-e)$, $r_a=a(1+e)$, $v_pr_p=v_ar_a$ and $T^2\propto a^3$, and explain the law of areas as conservation of angular momentum;
- use Newton's law of gravitation $F=\dfrac{Gm_1m_2}{r^2}$ with superposition, and the shell results for spheres;
- derive $T^2=\dfrac{4\pi^2}{GM}r^3$ for a circular orbit and use it to find the masses of the Sun, the Earth and the planets;
- derive $g=\dfrac{GM}{R^2}$ and its variation with height, $\dfrac{g}{(1+h/R)^2}\approx g\left(1-\dfrac{2h}{R}\right)$, and with depth, $g\left(1-\dfrac dR\right)$;
- use the gravitational potential energy $U=-\dfrac{GMm}{r}$ and the potential $V=-\dfrac{GM}{r}$, and show that they reduce to $mgh$ near the surface;
- calculate escape speed $\sqrt{2gR}$, orbital speed $\sqrt{GM/r}$, period, and the energies $K=-E$, $U=2E$ of a satellite;
- tackle Board, JEE Main, JEE Advanced and NEET-style problems on gravitation (with geostationary orbits as a JEE Advanced extension).
Sections in this chapter
Kepler's Laws and the Universal Law of Gravitation
Elliptical orbits, the law of areas, $T^2\propto a^3$, Newton's inverse-square law, the constant $G$ and weighing the Sun.
Acceleration due to Gravity and Its Variation
Where $g=9.8\ \text{m/s}^2$ comes from, the mass of the Earth, and how $g$ changes with height and with depth.
Gravitational Potential Energy, Escape Speed and Satellites
$U=-GMm/r$, gravitational potential, escape speed, orbital speed and period, and the energy of a satellite.