College Physics: Gravitation
G.6 Gravitational Intensity and Potential
G.6.1 Gravitational Intensity
G.6.2 Gravitational Potential
G.6.3 Gravitational Potential Energy
The gravitational potential energy at infinity is assumed to be zero.
Click here for Solved Example G.7: Gravitational Potential Energy
G.7 SatellitesA satellite is any body revolving around a large heavenly body like a planet. For example, the Moon is a satellite of the Earth. The Moon is a natural satellite. There may even be artificial or man-made satellites revolving round a planet.
Consider a satellite of mass m at a distance r from the center of the planet rotating at an angular velocity w. If the mass of the planet is M, then the motion of the satellite is governed by the following force balance.
G.7.1 Time Period of a Satellite
The time taken by a satellite to complete one revolution round a planet is called its time period T, and an expression for it can be easily calculated using equation (G.19) as follows.
Equation (G.20) is basically Kepler's Third Law as applied to satellites.
For the case of a satellite revolving around the Earth in a circle at a height h from the Earth's surface with h much smaller than R, equation (G.21) may be approximated by
Click here for Solved Example G.8: Time Periods and Orbital Velocities of Satellites
G.8 Escape VelocityThe escape velocity of a body is defined as the minimum velocity with which a body must be projected from the surface of the Earth, so that it may not return.
The work done in taking a body from the surface of the Earth to infinity is
If a body is to be projected such that it may never return, then its kinetic energy must equal this work done as given below.
Thus, the expression for the escape velocity is
For the Earth, the value of the escape velocity is 11.2 km/s.
Click here for Solved Example G.9: Escape Velocity of a Satellite
G.9 PlanetsThe equations derived above for satellites are valid for planets with M representing the mass of the sun (rather than the Earth) and m representing the mass of the planet (rather than the satellite). The sun may be treated as an inertial frame of reference as its mass is several times more than that of the planet. The path of the planets may be assumed to be circular rather than elliptical because the difference in major and minor axes is not much. The greatest difference amongst the nine planets in our solar system is for Pluto which is only 3%.