Gravitation is the force of attraction between any two masses in the universe. It governs the motion of planets, satellites, stars, and all objects on Earth. This chapter from cbse syllabus class 11 physics explains Newtonβs universal law of gravitation, acceleration due to gravity, gravitational field and potential, motion of satellites, and Keplerβs laws of planetary motion.
Universal Law of Gravitation
Sir Isaac Newton was the first to propose that the same force which causes an apple to fall to the ground also governs the motion of celestial bodies. According to him, any two objects in the universe attract each other with a force that:
- Is directly proportional to the product of their masses.
- Is inversely proportional to the square of the distance between them.
- Acts along the line joining the two bodies.
Mathematically, F = Fm1m2/r2; where:
- F = gravitational force
- m1, m2 = masses of the two objects
- r = distance between their centres
- G = universal gravitational constant
The value of F was first calculated by Cavendish in 1798 using the torsion balance experiment. Its value is β G = 6.67 x 10-11 Nm2kgβ2.
Importance of the Universal Law of Gravitation
The law is universal as it applies to all objects in the universe, irrespective of size and distance. It explains:
- Motion of planets around the Sun
- Motion of the Moon around the Earth
- The phenomena of tides due to the Moon and Sun
- Artificial satellite orbits
- Falling of objects on Earth
Acceleration Due to Gravity (g)
When an object falls freely near the Earthβs surface, it experiences an acceleration directed towards the center of the Earth. This is called acceleration due to gravity, denoted by g.
For an object of mass mm on Earth:
For an object of mass m on Earth β F = GMm/R2; where M is the mass of Earth and R is the radius of Earth.
But F = mg, therefore: g = GM/R2. Thus, g depends on G, M, and R. The average value of g on Earth is approximately 9.8 m/s2.
Variation of g
Acceleration due to gravity is not constant everywhere. It varies with altitude, depth, latitude and shape of Earth.
(i) Variation with Altitude
At height h above Earthβs surface β gh = GM/(R + h)2 = g(R2/(R + h)2)
If h<<R: gh β g(1 β 2h/R) Thus, g decreased with altitude.
(ii) Variation with Depth
At depth d below Earthβs surface β gd β g(1 β d/R) Thus, g decreases linearly with depth and becomes zero at the center of the Earth.
(iii) Variation with Latitude
Due to Earthβs rotation, effective gravity decreases as we move from poles to equator.
At latitude Ξ¦: gβ = g β RΟ2cos2Ξ¦; where Ο is angular velocity of Earth. At the equator, reduction is maximum, and at poles, there is no effect.
Gravitational Field
A gravitational field is the region in space around a mass in which another mass experiences a force of attraction. The gravitational field strength or gravitational intensity at a point is defined as the gravitational force experienced by a unit mass placed at that point.
E = F/m = GM/r2
Gravitational Potential Energy
The gravitational potential energy of a body of mass mm at a distance rr from the center of Earth is β U = β GMm/r. The negative sign indicates that the potential energy is taken as zero at infinity and decreases as the body comes closer to Earth.
For small height h β U = mgh
Gravitational Potential
Gravitational potential at a point is the work done in bringing a unit mass from infinity to that point without acceleration.
V = β GM/r
Relation between field and potential β E = β dV/dr
Escape Velocity
The escape velocity is the minimum velocity with which a body must be projected from Earthβs surface so that it can escape Earthβs gravitational pull and never return.
Derivation:
Condition: Total energy β₯ 0 β 1/2mve2 β GMm/R = 0 β ve = β(2GM/R) = β2gR
For Earth, ve β 11.2km/s. It is independent of the mass of the body.
Orbital Velocity of Satellites
A satellite revolves around Earth in a circular orbit due to the balance of gravitational force and centripetal force β GMm/r2 = mv2/r β v = βGM/r. This velocity is called orbital velocity. For a satellite close to Earthβs surface: v β 7.9km/s.β
Time Period of Satellite
The orbital period is given by β T = 2Οr/v = 2Οβr3/GM. This is also called Keplerβs Third Law of Planetary Motion.β
Height of Geostationary Satellites
A geostationary satellite appears stationary relative to Earth. It has:
- Time period = 24 hours
- Rotates in equatorial plane
- Same angular velocity as Earth
From T = 2Οβr3/GM, the height comes out to be about 36,000 km above Earthβs surface.
Energy of Satellite
The total energy of a satellite in orbit is the sum of its kinetic and potential energies.
K = 1/2 mv2 = GMm/2r; and U = β GMm/r β E = K + U = β GMm/2r
Thus, energy is negative, indicating a bound system.
Keplerβs Laws of Planetary Motion
Johannes Kepler proposed three laws:
- Law of Orbits - Planets revolve around the Sun in elliptical orbits with the Sun at one focus.
- Law of Areas - A line joining the planet and the Sun sweeps out equal areas in equal intervals of time.
- Law of Periods - Square of the orbital period is directly proportional to the cube of the semi-major axis. Consequently, T2 β r3.
Newton later proved these laws mathematically using his law of gravitation.
Weightlessness
Weight is the force with which a body is attracted towards the Earth. In an orbiting satellite, both the satellite and the body inside it fall freely under gravity. Hence, relative to each other, they appear weightless. This condition is called weightlessness.
Conclusion
Gravitation explains motion from falling objects to planetary orbits. Understanding Newtonβs law, variation of g, gravitational potential, and satellite motion is essential for solving numerical problems and understanding celestial mechanics.
FAQs
Q1. What is escape velocity?
Ans. It is the minimum velocity required for a body to escape from Earthβs gravitational field without any further acceleration. For Earth, it is about 11.2 km/s.
Q2. What are geostationary satellites?
Ans. Satellites that revolve around the Earth in 24 hours in the equatorial plane in the same direction as Earthβs rotation. They appear stationary with respect to Earth.
Q3. What is the difference between gravitational force and electrostatic force?
Ans. Gravitational force is always attractive, very weak, and acts between masses. Electrostatic force can be attractive or repulsive, much stronger, and acts between charges.
Q4. Does the value of g remain constant everywhere on Earth?
Ans. No, the value of g varies with altitude, depth and latitude of the place.
Q5. What is the difference between mass and weight?
Ans. Mass is the amount of matter in a body, constant everywhere, scalar. Weight is the force with which Earth attracts a body, depending on g, vector.
Q6. What is the difference between orbital velocity and escape velocity?
Ans. Orbital velocity keeps the body in circular orbit. Escape velocity removes the body completely from the gravitational field.






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