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Revision: 11th Std >> Gravitation MAH-MHT CET (PCM/PCB) Gravitation

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Definitions [25]

Definition: Gravitation

"Every particle of matter in the universe attracts every other particle with a force directly proportional to the product of their masses and inversely proportional to the square of the distance between them. The direction of the force is along the line joining the particles."

or

The force by which the Earth attracts objects towards its centre is called gravitational force.

OR

The force of mutual attraction that any two objects in the universe exert on each other, which is directly proportional to the product of their masses and inversely proportional to the square of the distance between their centres, is called the gravitational force.

Definition: Universal Law of Gravitation

"Every particle of matter attracts every other particle of matter with a force which is directly proportional to the product of their masses and inversely proportional to the square of the distance between them."

Definition: Acceleration Due to Gravity

The gravitational force due to the earth on a body results in its acceleration. This is called acceleration due to gravity and is denoted by ‘g’.

OR

When a body falls towards the Earth under gravity, then the acceleration produced in the body due to gravity is called acceleration due to gravity, which is denoted by g.

Definition: Gravity with Depth

Acceleration due to gravity at depth d is the rate at which an object accelerates toward the Earth when placed at a distance d below the Earth's surface. It is defined as the gravitational force per unit mass acting on a body at that depth.

Definition: Latitude

Latitude is an angle made by the radius vector of any point from the centre of the Earth with the equatorial plane. Obviously it ranges from 0° at the equator to 90° at the poles.

Definition: Weight of an object

"Weight of an object is the force with which the Earth attracts that object."

Definition: Gravitational Potential

The gravitational potential energy per unit mass at a point is called gravitational potential.

OR

The negative of the work done by the gravitational force in displacing a unit mass from that point to infinity (or equivalently, the work done in bringing unit mass from infinity to that point without acceleration), is called Gravitational Potential.

VP = −\[\frac {GM}{r}\]
Definition: Potential Energy

"Potential energy is the work done against conservative force (or forces) in achieving a certain position or configuration of a given system."

OR

The energy stored in an object because of its position or state is called potential energy.

OR

The amount of work done against conservative forces which causes a change in P.E. is called potential energy.

Definition: Gravitational Potential Energy

The amount of work done in bringing a given body from infinity to that point against the gravitational force is called gravitational potential energy.

OR

The energy possessed by a system of two or more bodies by virtue of their positions and mutual gravitational attraction, which equals the work done against the gravitational force in assembling the system from infinity, is called Gravitational Potential Energy.

U = −\[\frac {Gm_1m_2}{r}\]
Definition: Escape velocity

"The minimum velocity with which a body should be thrown vertically upwards from the surface of the Earth so that it escapes the Earth’s gravitational field, is called the escape velocity (ve) of the body."

What is meant by the gravitational potential energy?

The gravitational potential energy refers to the potential energy that a body possesses as a result of the Earth's force of attraction to it.

Definition: Potential Difference

The potential difference (p.d.) between two points is equal to the work done per unit charge in moving a positive test charge from one point to the other.

OR

The work done per unit positive charge in moving a charge from one point to another in an electric field, is called potential difference between those two points.

Define the following:

Potential difference

 Potential difference: The potential difference between two points may be defined as the work done in moving a unit positive charge from one point to the other.

Definition: Potential at a Point

The potential at a point is defined as the amount of work done per unit charge in bringing a positive test charge from infinity to that point.

Define Electric potential.

Electric potential is a measure of work done on the unit's positive charge to bring it to that point against all electrical forces. It is represented as ‘V’.

Definition: Artificial Satellite

A man-made object that orbits a planet or other celestial body is called an artificial satellite.

Answer the following question in detail.

What is a critical velocity?

The exact horizontal velocity of projection that must be given to a satellite at a certain height so that it can revolve in a circular orbit round the Earth is called the critical velocity or orbital velocity (vc).

Definition: Satellite

The objects that revolve around the Earth are called Earth satellites.

Answer the following question.

Define the binding energy of a satellite.

The minimum energy required by a satellite to escape from Earth’s gravitational influence is the binding energy of the satellite.

Definition: Geosynchronous Satellite

A satellite that orbits the Earth at a height of approximately 36,000 km above the equator with a period of revolution of 24 hours is called a geosynchronous satellite.

Definition: Polar Satellite

A satellite that travels over Earth's poles, passing close to the Earth's surface, with a period of revolution of nearly 85 minutes is called a polar satellite.

Definition: Critical Velocity

The exact horizontal velocity of projection that must be given to a satellite at a certain height so that it can revolve in a circular orbit around the Earth is called the critical velocity or orbital velocity (vc).

OR

The horizontal velocity of projection that must be given to a satellite at a certain height so that it can revolve in a circular orbit around the Earth is called the critical velocity or orbital velocity (vc​).

Definition: Weightlessness

The feeling of weightlessness is the state where "there will not be any feeling of weight," and the weighing machine will record zero.

Definition: Time Period of a Satellite

The time taken by a satellite to complete one full revolution around the Earth is called the Time Period of the satellite.

Definition: Critical Velocity

The limiting velocity up to which flow is streamline and beyond which it changes to turbulent is called critical velocity.

vC​ = (Re ​× η)/(ρl)

Formulae [21]

Formula: Gravitation

Newton’s Universal Law of Gravitation:
F = \[G\frac{m_1m_2}{r^2}\]

where:

  • F = Gravitational force between two objects
  • m1,m2 = Masses of the two objects
  • r = Distance between the centers of the two masses
  • G = Universal gravitational constant = 6.67×10−11 Nm2/kg2
Formula: Kepler's Law

Kepler’s Third Law relates the time period T of a planet’s revolution to the semi-major axis a of its elliptical orbit:
T2 ∝ a3
where,

  • T = time period of revolution of the planet,
  • a = semi-major axis of the elliptical orbit.
Formula: Kepler's Second Law

The area swept by the planet of mass m in a given interval Δt is:

\[\Delta\vec{A}=\frac{1}{2}(\vec{r}\times\vec{v}\Delta t)\]

  • \[\vec r\]: Position vector of the planet (distance from Sun).
  • \[\vec v\]: Velocity vector of the planet.
  • Δt: Time interval.
  • \[\vec p\]: Linear momentum (\[\vec p\] = m\[\vec v\])
  • \[\vec L\]: Angular momentum (\[\vec L\] = \[\vec r\] × \[\vec p\])
Formula: Kepler's Third Law

T2 ∝ r3

That is,

\[\frac {T^2}{r^3}\] = constant = K

Where:

  • T: Period of revolution (time taken by the planet to complete one orbit)
  • r: Mean distance (or length of the semi-major axis) between the planet and the Sun
  • K: Constant value for all planets around the Sun
Formula: Universal Law of Gravitation

The gravitational force of attraction (F) between two bodies of mass m1 and m2 separated by a distance r is:

\[\mathbf{F} = \mathbf{G}\frac{m_1 m_2}{r^2}\]
  • F: Gravitational Force of attraction (in Newtons, N).

  • \[m_1, m_2\]: Masses of the two objects (in kilograms, kg).

  • r (or d in the first part): Distance between the two objects (in meters, m).

  • G: The constant of proportionality, called the Universal gravitational constant.

    • Value in SI units: \[G=6.67\times10^{-11}\mathrm{N}\cdot\mathrm{m}^2/\mathrm{kg}^2\]

    • Dimensions: \[[G]=[\mathrm{L}^3\mathrm{M}^{-1}\mathrm{T}^{-2}]\]

Formula: Acceleration due to gravity

The value of the acceleration due to gravity (g) on the surface of the Earth is given by the formula:

\[g = \frac{G M}{R^2}\]

Where:

  • g = Acceleration due to gravity (in m/s²).
  • G = Newton's Universal Gravitational Constant (≈ 6.67 × 10⁻¹¹ N · m² / kg²).
  • M = Mass of the Earth (≈ 6 × 1024 kg).
  • R = Radius of the Earth (≈ 6.4 × 10⁶ m).
Formula: Gravity with Altitude

The formulas for acceleration due to gravity (g) are provided below:

On the Earth's Surface:

\[g = \frac{G M}{R^2}\]

At height $h$ above the Earth's Surface:

\[g_h = g \frac{R^2}{(R+h)^2} \quad \text{or} \quad g_h = g \left(I + \frac{h}{R}\right)^{-2}\]

Simplified Formula for Small Altitudes ($h \ll R$):

\[g_h = g \left(1 - \frac{2h}{R}\right)\]

Definition of Terms:

  • g: Acceleration due to gravity on the Earth's surface.
  • gh: Acceleration due to gravity at height h above the Earth's surface.
  • G: Universal Gravitational Constant.
  • M: Mass of the Earth.
  • R: Radius of the Earth.
  • h: Altitude or height above the Earth's surface.
Formula: Gravity with Depth

Where:

  • gd = acceleration due to gravity at depth d
  • g = acceleration due to gravity at Earth's surface (approximately 9.8 m/s²)
  • d = depth below Earth's surface
  • R = radius of the Earth (approximately 6,371 km)
Formula: Gravity with Latitude

The effective acceleration due to gravity (g') at a point on the Earth's surface at latitude θ is given by:

\[g' = g - R\omega^2 \cos^2\theta\]

Where:

  • g': The effective acceleration due to gravity at latitude θ (m/s²).
  • g: The true acceleration due to gravity (without rotational effect) (m/s²).
  • R: The radius of the Earth (m).
  • ω: The angular velocity of rotation of the Earth (rad / s or s-1).
  • θ: The latitude of the point (in degrees or radians).
Formula: Weight of an object
w = mg
where: 
  • w is the weight of the object.
  • m is the mass of the object.
  • g is the acceleration due to gravity.
Formula: Potential Energy

Based on the relationship between work and energy, the change in potential energy is given by:

\[\vec F\] · d\[\vec x\] = dU

  • \[\vec{F}\]: The force acting on the object (external force applied against the conservative force).
  • \[d\vec{x}\]: The small displacement of the object.
  • dU: The change (increase) in the potential energy of the system.
Formula: Escape velocity

\[v_e=\sqrt{\frac{2GM}{R}}\]

  • ve = Escape velocity (minimum speed needed to escape Earth’s gravity)
  • G = Universal gravitational constant (6.674 × 10−11 Nm2/kg2)
  • M = Mass of the Earth (or celestial body)
  • R = Radius of the Earth (or distance from the centre of the mass to the object)
Formula: Gravitational Potential Energy

U(r) = -\[\frac {GMm}{r}\]

Where:

  • U(r) = Gravitational potential energy at distance r from Earth's center
  • G = Universal gravitational constant (6.67 × 10⁻¹¹ N·m²/kg²)
  • M = Mass of Earth (kg)
  • m = Mass of the object (kg)
  • r = Distance between the centers of mass of Earth and object (m)
  • Negative sign = Shows that potential energy is negative (zero at infinity)
Formula: Electric Potential at a Point

V = \[\frac {W}{Q}\]

or

W = QV

Formula: Critical velocity

vc = \[\sqrt{\frac{GM}{R+h}}\]

Where:

  • vc = critical velocity (m/s)
  • G = gravitational constant (6.67 × 10⁻¹¹ N·m²/kg²)
  • M = mass of the Earth (kg)
  • R = radius of the Earth (km)
  • h = height of satellite above Earth's surface (km)
Formula: Newton's Second Law of Motion

According to Newton's second law of motion:

F = ma

Where:

  • F is the net force acting on an object.
  • m is the mass of the object.
  • a is the acceleration of the object.

For a passenger in a lift, the net force in the downward direction is:

F = mg - N

Where:

  • F is the net force.
  • m is the mass of the passenger.
  • g is the gravitational acceleration (gravitational force is mg).
  • N is the normal reaction force exerted by the floor (this is the experienced/apparent weight).
Formula: Time Period of Satellite

T = \[2\pi\sqrt{\frac{(R+h)^3}{GM}}\]

Where:

  • T = Time period of the satellite (in seconds)
  • R = Radius of the Earth
  • h = Height of the satellite above Earth's surface
  • G = Universal gravitational constant
  • M = Mass of the Earth
  • (R + h) = r = Radius of the satellite's orbit
Formula: Kinetic Energy of Satellite

K.E. = \[\frac {GMm}{2r}\]

Formula: Potential Energy of Satellite

P.E. = -\[\frac {GMm}{r}\]

Formula: Total Energy of Satellite

T.E. = −\[\frac {GMm}{2r}\]

Formula: Binding Energy of Satellite

B.E. = −T.E. = \[\frac {GMm}{2r}\]

Theorems and Laws [5]

Law: Kepler's First Law

Kepler's First Law (Law of Ellipses)

  • Each planet moves in an elliptical orbit with the Sun at one focus.
  • This means planetary orbits are stretched circles, not perfect circles.
  • The ellipse has two foci; the Sun occupies one of these.
Law: Kepler's Second Law

Kepler's Second Law (Law of Equal Areas)

  • A line joining the planet and the Sun sweeps out equal areas in equal time intervals.
  • When the planet is nearer the Sun (perihelion), it moves faster.
  • When the planet is farther from the Sun (aphelion), it moves more slowly.
  • This law reflects conservation of angular momentum.
Law: Kepler's Third Law

Kepler's Third Law (Law of Periods)

  • The square of the time period of revolution of a planet is proportional to the cube of the semi-major axis of its orbit.
  • This means a planet farther from the Sun takes a longer time to complete an orbit.
Law: Universal Law of Gravitation

Statement:

The law which states that every particle of matter attracts every other particle in the universe with a force whose magnitude is directly proportional to the product of masses and inversely proportional to the square of distance between them is called Newton's Law of Gravitation.

Derivation:

Newton's Universal Law of Gravitation states that every particle of matter attracts every other particle of matter with a force which is:

  • Directly proportional to the product of their masses: F ∝ m1 ⋅ m2
  • Inversely proportional to the square of the distance between them: F ∝ \[\frac {1}{r^2}\]

Combining both, the gravitational force is expressed as:

F = G\[\frac{m_1m_2}{r^2}\]

where G is the Universal Gravitational Constant, measured by Henry Cavendish using the Cavendish balance, with the value:

G = 6.67 × 10−11Nm2/kg2

Shell Theorem

Statement:

The Earth can be thought of as many concentric spherical shells. According to the Shell Theorem:

  • The gravitational force from outer shells cancels out for an object inside them.
  • Only the mass beneath the object (i.e., at radius R − d) contributes to the gravitational force at that depth.

Proof:

Starting with the equation for acceleration due to gravity at the surface:
g = \[\frac {GM}{R^2}\]

If we assume Earth has uniform density ρρ, then:
M = \[\frac {4}{3}\]πR³ρ

Therefore:
g = \[\frac{G\times\frac{4}{3}\pi R^{3}\rho}{R^{2}}=\frac{4}{3}\pi RG\rho\]

At depth d, only the inner sphere of radius (R - d) matters:
M′ = \[\frac{4}{3}\pi(R-d)^3\rho\]

gd = \[\frac{G\times\frac{4}{3}\pi(R-d)^{3}\rho}{(R-d)^{2}}=\frac{4}{3}\pi(R-d)G\rho\]

Dividing the equation at depth d by the equation at the surface:
\[\frac{g_d}{g}=\frac{\frac{4}{3}\pi(R-d)G\rho}{\frac{4}{3}\pi RG\rho}=\frac{R-d}{R}=1-\frac{d}{R}\]

This gives us:
gd = g[1 − \[\frac {d}{R}\]]

Conclusion:

  • As depth increases, the value of gd decreases
  • The relationship is linear with respect to depth
  • At Earth's center (d = R): gd = g[1− 1] = 0 (no gravitational force)

Key Points

Key Points: Newton's Universal Law of Gravitation
  • Every object attracts every other with a gravitational force.
  • Force increases with mass — more mass means a stronger pull.
  • Force decreases with distance — doubling the distance halves the force.
  • A force acts along the line joining the centres (or centres of mass) of the two bodies.
Key Points: Variation in Acceleration due to Gravity
  • Due to Altitude: The acceleration due to gravity decreases with altitude as we move away from the surface of the Earth. As h↑, g↓.
  • Due to Depth: The acceleration due to gravity decreases as we move into the Earth's interior, i.e., with increasing depth. As d↑, g↓.
  • Due to Latitude: The acceleration due to gravity increases with latitude. At the poles (θ = 90°), g = gmax⁡​; at the equator (θ = 0°), g = gmin​.
  • Due to Shape of Earth: The equatorial radius of the Earth is greater than the polar radius. Since g ∝ \[\frac {1}{R^2}\], the acceleration due to gravity is greater at the poles compared to the equator, i.e., Requator > Rpole​ and gequator < gpole​.
Key Points: Gravitational Potential Energy
  • Gravitational P.E. per unit mass at a point is gravitational potential.
  • V = 0 (potential at infinity is zero).
  • It is independent of the mass of the object.
  • U = mgh
    Potential energy is a property of the entire system, not just a single object.
  • For an object near Earth's surface, U = mgh belongs to the system consisting of both the object and the Earth.
Key points: Potential and Potential Difference
  • Electric potential is a scalar quantity, and it is positive near a positive charge and negative near a negative charge.
  • Electric potential is taken as zero at infinity because the force between charges becomes zero at infinite separation.
  • The potential difference between two points is measured using a voltmeter, which is connected in parallel with the circuit, with its positive terminal at the higher-potential point.
Key Points: Critical Velocity or Projection of Satellite
  • In case of a revolving satellite, the centripetal acceleration is equal to the gravitational acceleration g — this is called the state of free fall; in free fall, the apparent weight of the body is zero.
  • The time taken by a satellite to complete one revolution around the Earth is its time period, where: Time period = \[\frac {\text {Circumference of the orbital}}{\text {Critical speed}}\]
  • The minimum energy required by a satellite to escape from Earth's gravitational influence is the binding energy of the satellite = +\[\frac {1}{2}\]\[\frac {GMm}{r}\]​.
  • Path of satellite depends on its velocity: vH < vc​ → Elliptical; vH = vc​ → Circular; vc < vH < ve​ → Elliptical (perigee at point of projection); vH = ve​ → Parabolic; vH > ve​ → Hyperbolic.
  • Energy of satellite: K.E. = \[\frac {1}{2}\]\[\frac {GMm}{r}\]​, P.E. = −\[\frac {GMm}{r}\]​, Total Energy = −\[\frac {1}{2}\]\[\frac {GMm}{r}\]​, Binding Energy = +\[\frac {1}{2}\]\[\frac {GMm}{r}\].
Key Points: Energy Associated with Satellite
  • K.E. and B.E. both decrease as orbital radius r increases; P.E. and T.E. both increase (become less negative) as r increases.
  • For a stationary object, K.E. = 0, so T.E. equals P.E. and B.E. = −T.E.
  • For a revolving satellite, K.E. is always half the magnitude of P.E., and B.E. is always equal to −T.E.
  • As orbital radius increases, the satellite has less kinetic energy but is harder to pull back (B.E. decreases), meaning it is less bound to Earth.
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