This chapter explores the concept of gravitation, detailing Kepler's laws and Newton's universal law of gravitation, gravitational potential energy, acceleration due to gravity, and the behavior of satellites and escape speed.
Gravitation is a fundamental force that attracts two bodies towards each other. Our first experiences with gravitation happen when objects fall back to the earth, illustrated by Galileo's findings that all objects fall at the same rate regardless of mass.
Kepler formulated three laws regarding planetary motion:
These laws paved the way for Newton’s law of gravitation.
Newton's Universal Law states:
Every body in the universe attracts every other body with a force proportional to the product of their masses and inversely proportional to the square of the distance between them.
This can be expressed mathematically as:
$$ F = G \frac{m_1 m_2}{r^2} $$
where G is the gravitational constant ( 6.67 x 10^-11 N m²/kg²).
The gravitational constant was first accurately measured by Henry Cavendish using a torsion balance in 1798.
Gravity can be expressed as:
$$ g = \frac{GM}{R^2} $$
Here, M is the mass of the Earth, and R is the radius of the Earth. The gravitational acceleration decreases with altitude and can be expressed for heights or depths:
The escape speed from the Earth's surface is given by:
$$ v_e = \sqrt{\frac{2GM}{R}} $$
This speed for the Earth is approximately 11.2 km/s. If an object is thrown with this speed or greater, it can escape the Earth’s gravitational influence.
Gravitational potential energy (U) between two masses can be calculated:
$$ U = - G \frac{m_1 m_2}{r} $$
The energy of a satellite in orbit comprises its kinetic and potential energy:
For circular orbits, total energy is negative indicating the system is bound.
Satellites orbiting the Earth follow Kepler’s laws. The period of orbit can be calculated using:
$$ T^2 = \frac{4\pi^2}{G M}R^3 $$
For artificial satellites, the time period and radius can effectively be utilized to understand their motion and properties.