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**MULTIPLE CHOICE QUESTION I**

**Q.1. The earth is an approximate sphere. If the interior contained matter which is not of the same density everywhere, then on the surface of the earth, the acceleration due to gravity(a) Will be directed towards the centre but not the same everywhere.(b) Will have the same value everywhere but not directed towards the centre.(c) Will be same everywhere in magnitude directed towards the centre.(d) Cannot be zero at any point.Ans.** (d)

If the density of the earth is non-uniform then ‘g’ at different point on the surface of the earth will be different.

If we substitute any value of density, g ≠ 0 at any point.

(a) Be similarly true.

(b) Not be true because the force between earth and mercury is not inverse square law.

(c) Not be true because the major gravitational force on mercury is due to sun.

(d) Not be true because mercury is influenced by forces other than gravitational forces.

Ans.

Force of attraction between any two objects obeys the inverse square law as its universal law. The relative motion between Earth, Mercury as observed from Earth will not be circular as the force on Mercury due to the sun is very large than due to Earth and due to the relative motion of Sun and Earth with Mercury.

For a rigid body, we know that if various forces act at various points in it, the resultant motion is as if a net force acts on the c.m. (centre of mass) causing translation and a net torque at the c.m. causing rotation around an axis through the c.m.

For the earth-sun system (approximating the earth as a uniform density sphere)

(a) The torque is zero.

(b) The torque causes the earth to spin.

(c) The rigid body result is not applicable since the earth is not even approximately a rigid body.

(d) The torque causes the earth to move around the sun.

Ans.

The torque on earth due to gravitational attractive force on earth is zero, because the direction of force (F) (gravitational) and the line joining, the point of application of force (which also is at c.m. of earth) is along the same direction, so angle between is zero or

(a) The solar cells and batteries in satellites run out.

(b) The laws of gravitation predict a trajectory spiralling inwards.

(c) Of viscous forces causing the speed of satellite and hence height to gradually decrease.

(d) Of collisions with other satellites.

Ans.

We know that the total energy of the earth satellite of radius R bounded system is negative

(-GM\ 2 R)

where M is mass of the earth. –

Due to the atmospheric friction (viscous force) acting on satellite, energy decreases continuously, radius of the orbit or height decreases gradually and the satellite spirals down with increasing speed till it bums in the denser layers of the atmosphere.

**Q.5. Both earth and moon are subject to the gravitational force of the sun. As observed from the sun, the orbit of the moon(a) Will be elliptical.(b) Will not be strictly elliptical because the total gravitational force on it is not central.(c) Is not elliptical but will necessarily be a closed curve.(d) Deviates considerably from being elliptical due to influence of planets other than earth.Ans.** (b)

Moon revolves around the earth in a nearly circular orbit. When it is observed from the sun, two types of forces are acting on the moon one is due to gravitational attraction between the sun and the moon and the other is due to gravitational attraction between the earth and the moon. So moon is moving under the combined gravitational pull acting on it due to the earth and the sun. Hence, total force on the moon is not central.

(a) Will not move around the sun since they have very small masses compared to sun.

(b) Will move in an irregular way because of their small masses and will drift away into outer space.

(c) Will move around the sun in closed orbits but not obey Kepler’s laws.

(d) Will move in orbits like planets and obey Kepler’s laws.

Ans.

Like any other planet, asteroids also follow Kepler’s law and move in elliptical orbits around planet due to the central gravitational force acting on them.

small mass of asteroid does not escape the gravitational force due to sun because of large mass of sun and hence, (a) is incorrect. Since gravitational force follow inverse square law, the asteroid will move in circular or elliptical orbits and (b) is incorrect option

(a) Inertial mass is a measure of difficulty of accelerating a body by an external force whereas the gravitational mass is relevant in determining the gravitational force on it by an external mass.

(b) That the gravitational mass and inertial mass are equal is an experimental result.

(c) That the acceleration due to gravity on earth is the same for all bodies is due to the equality of gravitational mass and inertial mass.

(d) Gravitational mass of a particle like proton can depend on the presence of neighbouring heavy objects but the inertial mass cannot.

Ans.

The mass of an object A can be defined as the mass of the object obtained by measuring their accelerations under equal forces taking mass of B to be 1kg. This is known as inertial mass.

The gravitational force exerted by a massive body on an object is proportional to the mass of the object. If F

Thus

If B is a standard unit mass, by measuring gravitational Force we can obtain the mass of object A which is known as gravitational mass.

By several experiments, it has been concluded that the inertial and gravitational mass are identical.

At subsequent times before any collision takes place:

(a) m will remain at rest

(b) m will move towards M

(c) m will move towards 2M

(d) m will have oscillatory motion

Ans.

Let F

Suppose AB = x, then

Substituting the values of AB and BC in the above equations (1) and (2)

As F

**MULTIPLE CHOICE QUESTIONS II**

**Q.9 Which of the following options are correct? (a) Acceleration due to gravity decreases with increasing altitude. (b) Acceleration due to gravity increases with increasing depth (assume the earth to be a sphere of uniform density). (c) Acceleration due to gravity increases with increasing latitude. (d) Acceleration due to gravity is independent of the mass of the earthAns.** (a, c)

increasing height (h) decreases the value of gh. option (a) is correct.

Increasing depth (d) decreases the value of gd. Option (b) is incorrect.

As value of cos λ decrease from 0º to 90º ( from 1 to 0). The acceleration due to gravity increases from equator (λ = 0º) to pole (λ = 90º). Option (c) is correct.

So g on earth depends on mass of earth. Option (d) is incorrect.

(a) planets will not have elliptic orbits.

(b) circular orbits of planets is not possible.

(c) projectile motion of a stone thrown by hand on the surface of the earth will be approximately parabolic.

(d) there will be no gravitational force inside a spherical shell of uniform density.

Ans.

If the law of gravitation becomes an inverse cube law instead of inverse square law, then for a planet of mass m revolving around the sun of mass M, we can write

(where R is the radius of orbiting planet)

⇒ Orbital Speed

Time period of revolution of a planet

⇒ T

Hence, orbit will not be elliptical.

[for elliptical orbit T

The circular orbits of the planets is not possible according to new law of gravitation.

As force

where,

As g' acceleration due to gravity is constant, hence path followed by a projectile will be approximately parabolic, (as T ∝ R

Also, gravitational force inside a spherical shell of uniform density will have some value. So, only option (d) is incorrect.

(a) Walking on ground would became more difficult.

(b) The acceleration due to gravity on earth will not change.

(c) Raindrops will fall much faster.

(d) Airplanes will have to travel much faster

Ans.

According to the problem

G'

From the adjacent diagram

Gravitational field due to the earth

Weight of person = mg' = m x 10 g = 10 mg

force on the man due to the sun

As r »R (radius of the earth)

⇒ F will be very small.

So, the effect of the sun will be neglected.

Due to this reason gravity pull on the person will increase. Due to it, walking on ground would become more difficult.

Critical velocity, vc is proportional to g, i.e., v

As, g’ > g => v

Hence, rain drops will fall much faster.

To overcome the increased gravitational force of the earth, the aeroplanes will have to travel much faster.

(a) All three of Kepler’s laws would still be valid

(b) Only the third law will be valid

(c) The second law will not change

(d) The first law will still be valid

Ans.

Coulomb’s electric force or Electrostatic force of attraction will produce due to opposite charges.

If the sun and the planets carries huge amount of opposite charges, then electrostatic force of attraction will be large. Gravitational force is also attractive in nature have both forces will be added and both are radial in nature.

Both the forces obey inverse square law and are central forces. As both the forces are of same nature, hence all the three Kepler’s laws will be valid.

(a) Nothing will change

(b) We will become hotter after billions of years

(c) We will be going around but not strictly in closed orbits

(d) After sufficiently long time we will leave the solar system

Ans.

F

Where M

This provides the necessary centripetal force for the circular orbit of the earth around the sun. As G decreases with time, the gravitational force F

Hence, after long time the earth will leave the solar system.

(a) The acceleration due to gravity on earth will be different for different objects

(b) None of the three laws of Kepler will be valid

(c) Only the third law will become invalid

(d) For n negative, an object lighter than water will sink in water

Ans.

Where M

For calculating acceleration due to gravity let

M

M

r

Then magnitude of force between the object and earth is given by

Which can be said as

Where K is a constant

Therefore, acceleration due to gravity can be calculated as

Which depends on mass and hence different for different objects

Therefore (a) is the correct option

since this force follows inverse square law, hence Kepler’s first two are valid but since g is no longer constant, therefore Kepler’s third law (Law of periods) does not remain valid therefore (c) is the correct option

when n is negative than force is given by

Where a = - n

Therefore, force is inversely proportional to mass of body, hence an object lighter than water will experience more force than water and therefore will sink in water

Therefore (a), (c) and (d) are the correct options

(a) A polar satellite goes around the earth’s pole in north south direction

(b) A geostationary satellite goes around the earth in east-west direction

(c) A geostationary satellite goes around the earth in west-east direction

(d) A polar satellite goes around the earth in east-west direction

Ans.

(a) Are always at the same point for any size of the body

(b) Are always at the same point only for spherical bodies

(c) Can never be at the same point

(d) Is close to each other for objects, say of sizes less than 100 m

(e) Both can change if the object is taken deep inside the earth

Ans.

The center of gravity is based on weight, whereas the center of mass is based on mass. So, when the gravitational field across an object is uniform, the two are identical. However, when the object enters a spatially-varying gravitational field, the COG will move closer to regions of the object in a stronger field, whereas the COM is unmoved.

More practically, the COG is the point over which the object can be perfectly balanced; the net torque due to gravity about that point is zero. In contrast, the COM is the average location of the mass distribution or it is the point where whole mass of the body is supposed to be concentrated. If the object were given some angular momentum, it would spin about the COM.

For small objects, say of sizes less than 100 m placed in uniform gravitational field then centre of mass is very close with the centre of gravity of the body. But when the size of object increases, its weight changes and its CM and CG become far from each other. Like in the case of spherical ball, the CM and the CG are the same, but in case of Mount Everest, its CM lies a bit above its CG.

**VERY SHORT ANSWER TYPE QUESTIONS**

**Q.1. Molecules in air in the atmosphere are attracted by gravitational force of the earth. Explain why all of them do not fall into the earth just like an apple falling from a tree.Ans.** Air molecules in the atmosphere are attracted by gravitational force of the earth but they do not fall into earth due to the reason that the molecules in air has some random motion due to temperature, so their resultant motion is not exactly in the vertical downward direction.

But in case of apple, only vertical motion dominates because of being heavier than air molecules. But due to gravity, the density of air is more near to the earth than the density as we go up.

**Q.2. Give one example each of central force and non-central force.Ans.**

(i) Gravitational force due to point mass.

(ii) Electrostatic force on the point charge.

(i) Nuclear force which depends upon the spin of particles.

(ii) Magnetic systems acting between two current carrying loops

**Q.3. Draw areal velocity versus time graph for mars.Ans.** Areal velocity of Mars revolving around the Sun does not change with time according to Kepler’s law, i.e. it is constant with time. Then graph of a real velocity versus time is a straight line parallel to time axis.

**Q.4. What is the direction of areal velocity of the earth around the sun?Ans.** Areal velocity of the earth around the sun is given by

where, L is the angular momentum and M is the mass of the earth.

But angular momentum

Therefore we get,

∴

Therefore, the direction of a real velocity is in the direction of

i.e., perpendicular to the plane containing r and v and directed as given by right hand rule. So, areal velocity is normal to the plane containing Earth and Sun as shown in the figure

**Q.5. How is the gravitational force between two point masses affected when they are dipped in water keeping the separation between them the same?Ans.** Gravitational force acting between two point masses m

F = G m

It does not depend upon the medium separating the two point masses. Therefore, gravitational force acting between two point masses will remain unaffected when they are dipped in water keeping the separation between them same. Only their apparent weights change, there is no effect on masses.

**Q.6. Is it possible for a body to have inertia but no weight?Ans. **Yes, a body can have inertia but no weight. Inertia of a body is related to mass. Where as weight of body is defined as

W = mg

Where

M = mass of body

g = acceleration due to gravity

therefore, weight of the object can be zero when the acceleration due to gravity becomes zero.

Since we know that at the centre of earth, the value of acceleration due to gravity is zero and hence the weight of the object is zero at the centre, but it remains mass(inertia) remains constant.

Ans.

Ans.

Ans.

Given:

Radius of hollow shell = R

Distance of point mass from centre of hollow shell = r

Let the mass of the spherical shell be M and the point mass be m. Then the force between the shell and the point mass is given by,

When point mass is positioned such that it is inside the hollow sphere i.e. 0<r<R, the force is zero as the mass of the hollow sphere is distributed on its surface. When the mass is positioned such that r≤R, the force will be,

Therefore, the graph will be as follows

Ans.

mr

Where m is the mass of the earth, r

∴ r

Since r

(a) Polar satellite?

(b) Geostationary satellite?

Ans.

(a) For a polar satellite, the satellite revolves from north to south and therefore its orbital plane is at 90° to the equatorial plane

(b) For a geostationary satellite whose position with respect to a place on earth is constant i.e. it revolves in the direction of the rotation of earth, the orbital plane is at 0° to the equatorial plane.

**SHORT ANSWER TYPE QUESTIONS**

**Q.1. Mean solar day is the time interval between two successive noon when sun passes through zenith point (meridian).Sidereal day is the time interval between two successive transit of a distant star through the zenith point (meridian).By drawing appropriate diagram showing earth’s spin and orbital motion, show that mean solar day is four minutes longer than the sidereal day. In other words, distant stars would rise 4 minutes early every successive day.(Hint: you may assume circular orbit for the earth).Ans.**

A day on earth is measured in terms of rotation of earth on its axis with respect to the sun called the mean solar day. When the day is measured with respect to a distant sun, it is called a sidereal day.

Let us look at the given figure, let the sun and distant star’s location be pointed by the long arrow at day 1, where they are directly in line with zenith of the observer on earth. When the earth rotates by 360° the arrow of the distant star points in the same direction along the zenith. However, the sun’s arrow is at an angle from the zenith. Thus, for the sun to be at the zenith in line with the observer, the earth needs to rotate an additional angle. Since the earth moves by 1° around the sun in a day, this additional angle is 1°. Now 360° is equal to 24 hours on earth or 1440 minutes, therefore

Therefore, the distant star will always rise 4 minutes earlier than the sun.

**Q.2. Two identical heavy spheres are separated by a distance 10 times their radius. Will an object placed at the mid point of the line joining their centres be in stable equilibrium or unstable equilibrium? Give reason for your answer.Ans.**

Given:

Distance between centres of spheres = 10 x radius

Let the mass of the two spheres be M and their radii be R. Then, the distance between the two will be 10R. let an object of mass m be placed at the midpoint of the line joining the centres of the spheres. Then the force acting on the object due to the two spheres F

Therefore, the forces are equal and in opposite directions and therefore the mass is in stable equilibrium.

However, if the mass were to be displaced by say a distance x from the midpoint towards the sphere 2, the forces acting on the object would be

Therefore, F

**Q.3. Show the nature of the following graph for a satellite orbiting the earth.(a) KE vs orbital radius R(b) PE vs orbital radius R(c) TE vs orbital radius RAns**

Given

Radius of satellite’s orbit = R

(a) Let the mass of earth be M and the mass of the satellite be m. Then the orbital velocity of the satellite will be

then, the kinetic energy of the satellite will be

(b) the potential energy of the satellite is given by

(c) the total energy of the satellite is given by

Therefore, the curves are as follows**Q.4. Shown are several curves (Figure). Explain with reason, which ones amongst them can be possible trajectories traced by a projectile (neglect air friction).Ans. **The trajectory or the path followed by a projectile under gravitational force of the earth instead of parabolic will be a conic section (for motion outside the earth) with the centre of the earth as a focus. Only the diagram in option (c) will fulfill the requirements.

Ans.

Given:

Mass of the object = m

Radius of earth = R

Initial height of the object from earth’s centre = R

Final height of the object from earth’s centre = 2R

Let the mass of earth be M. We know that the gravitational potential energy of an object is given by,

Where r is the distance between the object and centre of earth. When the object is at its initial position it is at a distance of R from the centre of the earth. Then its potential energy,

When the object is raised to a height 2R, then the potential energy is given by,

Now the gain in gravitational potential energy is given by

If the mass is removed further away such that OP becomes 2h, by what factor the force of gravitation will decrease, if h = r?

Ans.

Given:

Mass of the ring = M

Layout of the ring = r

Mass of the object = m

Initial distance of the object h = r

Final distance of the object 2h = 2r

To find the gravitational force on the object of mass m due to the ring let us consider an elemental mass on the ring of mass dM. The force due to this elemental mass is then,

where x is the distance of the object from the elemental mass m and

Now at the point P the force dF can be resolved into a vertical component and a horizontal component. If we consider two elemental masses diametrically opposite to each other, then the vertical component due to the two forces cancel each other as they are equal and opposite and the horizontal forces add up. Therefore, we only need to consider the horizontal component of the forces, therefore the net force on the object,

Now from the triangle OPA in the figure we have,

therefore,

When h = r

When h = 2h = 2r

Therefore, the force decreases by a factor of

**LONG ANSWER TYPE QUESTIONS**

**Q.1. A star like the sun has several bodies moving around it at different distances. Consider that all of them are moving in circular orbits. Let r be the distance of the body from the centre of the star and let its linear velocity be v, angular velocity ω, kinetic energy K, gravitational potential energy U, total energy E and angular momentum l. As the radius r of the orbit increases, determine which of the above quantities increase and which ones decrease.Ans. **

Given:

Radius of the orbit of planets = r

Let the mass of the sun be M and the planet be m.

Therefore, linear velocity v is inversely proportional to square root of r and hence when r increases, v decreases.

Therefore, when r increases, ω decreases.

Therefore, as r increases, K decreases.

Therefore, as r increases U becomes less negative or increases.

Therefore, as r increases E becomes less negative or increases.

Therefore, as r increases, L increases.

Ans.

Given

Side of hexagon = l

The force on the masses will be the resultant of the forces of all the other masses. Let the masses be m each. Now the distance AC is given by the parallelogram law i.e.

Due to symmetry we have AC = AE = 1√3

Now, for AD we have

Now the force on mass at A due to b is

Also

F

The force on mass A due to C is

Also due to symmetry, we have

F

The force on mass at A due to mass at D is

Now, the forces F

Similarly, F

Therefore, the net force on mass at A will be

F = F

(a) Calculate height of such a satellite.

(b) Find out the minimum number of satellites that are needed to cover entire earth so that at least one satellites is visible from any point on the equator.

[M = 6 × 10

Ans.

Where r is the radius of the orbit of the satellite and ω is its angular velocity

ω = 2π/T

where T is the time period of revolution, then

Now the height h of the satellite from the surface of the earth,

h = r - R

where R is the radius of earth.

For a geostationary satellite, the time period is 24 hours or 86400 seconds,

Now from the figure we have

θ = cos

Now 2θ = 162.58, therefore to cover the earth with such satellites so that from any point on the equator a satellite can be seen,

360/162.58 = 2.21 ≈ 3

Ans.

Given

The eccentricity of earth’s orbit e = 0.0167

Let the earth - sun distance at the aphelion and perihelion be r

Now, from the ellipse we have

r

Where a is the semi - major axis of the ellipse

Since e = 0.0167

⇒ ω_{a}/ω_{p }= 1.069

And since the mean angular velocity is the geometric mean of the two, we have

Now we know that the mean solar day corresponds to 1° on the orbit of earth. A mean solar day has 24 h for which the earth rotates 361°. Thus for aphelion the earth rotates 361.034° and hence the time for the day is 24 hours and 8.1 seconds, and the for the perihelion the earth rotates 359.96° and the time is 23 hours and 52 seconds. Thus the longest day is 8.1 seconds long and the shortest day is 8 seconds shorter. However, the variation of length of day in the year is not explained by this phenomenon as the total time of the day still remains around 24 hours, while the amount of time the sun is visible changes.**Q.5. A satellite is in an elliptic orbit around the earth with aphelion of 6R and perihelion of 2 R where R= 6400 km is the radius of the earth. Find eccentricity of the orbit. Find the velocity of the satellite at apogee and perigee. What should be done if this satellite has to be transferred to a circular orbit of radius 6R ?****[G = 6.67 × 10 ^{–11} SI units and M = 6 × 10^{24} kg]**

Ans.

Given

Radius of earth = R = 6400 km

Aphelion earth - satellite distance r

Perihelion earth - satellite distance r

We know for an ellipse

r

Where e is the eccentricity of the ellipse, and the semi major axis.

Now, the angular momentum of the satellite is conserved we then, we have

mr_{p}v_{p}=mr_{a}v_{a}

Where m is the mass of satellite and v_{p} and v_{a} are the velocities at the perigee and apogee respectively

Now from conservation of energy at the apogee and perigee

K_{P} + U_{P} = K_{a} + U_{a}

Where K and U are the kinetic and gravitational potential energy of the satellite

Where M is the mass of earth. Using the relation between v_{p} and v_{a} above we have

Putting the values of r_{p} and r_{a} we have

∴ v_{a} = v_{P}/3_{ }= 2.29 km/s

To transfer the satellite to a circular orbit of radius 6R the satellite’s velocity has to be maintained at a value of

** **

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