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Class- XI-CBSE-Physics Gravitation
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CBSE NCERT Solutions for Class 11 Physics Chapter 8
Back of Chapter Questions
8.1. (a) You can shield a charge from electrical forces by putting it inside a hollow
conductor.Can you shield a body from the gravitational influence of
nearby matter by putting it inside a hollow sphere or by some other
means?
(b) An astronaut inside a small space ship orbiting around the earth cannot
detect gravity. If the space station orbiting around the earth has a large
size, can he hope to detect gravity?
(c) If you compare the gravitational force on the earth due to the sun to that
due to the moon, you would find that the Sunβs pull is greater than the
moonβs pull.
(You can check this yourself using the data available in the succeeding exercises).
However, the tidal effect of the moonβs pull is greater than the tidal effect of sun.
Why?
Solution:
(a) No.There is no way to screen the gravitational influence of matter on
neighbouring objects. This is because, unlike electrical forces, the
gravitational force is independent of the material medium's nature. It is
also independent of the status of the object.
(b) Yes. If the size of the space station is sufficiently large, then the astronaut
will detect the change in Earthβs gravity (π).
(c) The tidal effect relies inversely upon the cube of the distance while the
gravitational force relies inversely on the square of the distance. Since the
distance between the Moon and the Earth is less than the distance between
the Sun and the Earth, the tidal effect Moon's pull's is greater than the tidal
effect Sun's pull.
8.2. Choose the correct alternative:
(a) Acceleration due to gravity increases/decreases with increasing altitude.
(b) Acceleration due to gravity increases/decreases with increasing depth.
(assume the earth to be a sphere of uniform density).
(c) Acceleration due to gravity is independent of mass of the earth/mass of the
body.
(d) The formula βπΊ ππ(1/π2 β 1/π1) is more/less accurate than the formula
ππ(π2 β π1) for the difference of potential energy between two points π2
and π1 distance away from the centre of the earth.
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Solution:
Explanation:
Decreases
The relation which gives acceleration due to gravity at depth h is given by :
(πβ) = (1 β2β
π π) π
Where,
π π = Radius of the Earth
π = Acceleration due to gravity on the surface of the Earth
It is clear from the given relation that with an increase in height, acceleration due
to gravity decreases.
Decreases
Acceleration due to gravity at depth d is given by the relation:
(ππ) = (1 βπ
π π) π
It is clear from the given relation that with an increase in depth, acceleration due
to gravity decreases.
Mass of the body.
Acceleration due to the gravity of the body of mass m is given by the relation:
π =πΊπ
π 2
Where,
πΊ = Universal gravitational constant
π = Mass of the Earth
π = Radius of the Earth
Therefore, acceleration due to gravity can be inferred independent of the body's
mass.
More
The gravitational potential energy of two points π2 and π1 distance away from the
centre of the Earth is respectively given by:
π(π1) = βπΊππ
π1
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π(π2) = βπΊππ
π2
β΄ The difference in potential energy, π = π(π2) β π(π1) = βπΊππ (1
π2β
1
π1)
Hence, this formula is more precise than the formula ππ(π2 β π1).
8.3. Suppose there existed a planet that went around the sun twice as fast as the earth.
What would be its orbital size as compared to that of the earth?
Solution:
Earth's time to complete a revolution around the Sun,
ππ = 1 year
The Earth's orbital radius in its orbit, π π = 1 π΄π
The Time taken by the planet to complete one revolution around the Sun,
ππ =1
2ππ =
1
2 year
The orbital radius of the planet = π π
From Keplerβs third law of planetary motion:
(π π
π π)
3
= (ππ
ππ)
2
π π
π π= (
ππ
ππ)
23
= (
121
)
23
= (0.5)23 = 0.63
Therefore, the planet's orbital radius will be 0.63 times lower than the Earth's.
8.4. πΌπ, one of the satellites of Jupiter, has an orbital period of 1.769 days and the
radius of the orbit is 4.22 Γ 108 m. Show that the mass of Jupiter is about one-
thousandth that of the sun.
Solution:
Orbital period of πΌ0, ππΌ0= 1.769 Γ 24 Γ 60 Γ 60 s
Orbital radius of πΌ0, π πΌ0= 4.22 Γ 108m
Satellite I0 is revolving around the Jupiter
The Mass of the latter is given by the relation:
ππ =4π2π Β±
3
πΊππΌ02 β¦β¦.(i)
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Where,
ππ = Mass of Jupiter
πΊ = Universal gravitational constant
The orbital period of the Earth,
ππ = 365.25 days = 365.25 Γ 24 Γ 60 Γ 60 s
The orbital radius of the Earth,
π π = 1 AU = 1.496 Γ 1011m
Mass of Sun is given as:
ππ =4π2π π
3
πΊππ2 β¦..(ii)
β΄ππ
ππ=
4π2π π3
πΊππ2
ΓπΊπ10
2
4π2π 103 =
π π3
π 103 Γ
π102
ππ2
= (1.769 Γ 24 Γ 60 Γ 60
365.25 Γ 24 Γ 60 Γ 60)
2
Γ (1.496 Γ 1011
4.22 Γ 108)
3
= 1045.04
β΄ππ
ππ½~1000
ππ~1000 Γ ππ
Therefore, It can be inferred that Jupiter's mass is about one-thousandth of the
Sun's mass.
8.5. Let us assume that our galaxy consists of 2.5 Γ 1011 stars each of one solar mass.
How long will a star at a distance of 50,000 ly from the galactic centre take to
complete one revolution? Take the diameter of the Milky Way to be 105 ly.
Solution:
The Mass of our galaxy Milky Way, π = 2.5 Γ 1011 solar mass
Solar mass = Mass of Sun = 2.0 Γ 1036 kg
Mass of our galaxy, π = 2.5 Γ 1011 Γ 2 Γ 1036 = 5 Γ 1041 kg
The diameter of Milky Way, d = 105 ππ¦
The radius of Milky Way, r = 5 Γ 104 ππ¦
1 ly = 9.46 Γ 1015 m β΄
π = 5 Γ 104 Γ 9.46 Γ 1015
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= 4.73 Γ 1020 m
Since a star revolves around the galactic centre of the Milky Way, its time period
is given by the relation:
π = (4π2π3
πΊπ)
12
= (4 Γ (3.14)2 Γ (4.73)3 Γ 1060
6.67 Γ 10β11 Γ 5 Γ 1041)
12
= (39.48 Γ 105.82 Γ 1030
33.35)
12
= (125.27 Γ 1030)12 = 1.12 Γ 1016 s
1 year = 365 Γ 324 Γ 60 Γ 60 s
1s =1
365Γ24Γ60Γ60 years
β΄ 1.12 Γ 1016s =1.12 Γ 1016
365 Γ 24 Γ 60 Γ 60
= 3.55 Γ 108 years
8.6. Choose the correct alternative:
(a) If the zero of potential energy is at infinity, the total energy of an orbiting
satellite is negative of its kinetic/potential energy.
(b) The energy required to launch an orbiting satellite out of earthβs
gravitational influence is more/less than the energy required to project a
stationary object at the same height (as the satellite) out of earthβs
influence.
Solution:
(a) Kinetic energy
A satellite's total mechanical energy is the sum of its kinetic energy
(always positive) and potential energy (may be negative). At infinity, the
satellite's gravitational potential is zero. The total energy of the satellite is
negative because the Earth-satellite system is a bound system.
Thus, an orbiting satellite's total energy at infinity is equivalent to the
negative of its kinetic energy.
(b) Less
An orbiting satellite gains a certain amount of energy that allows it to
revolve around the Earth. This energy is provided by its orbit. To move
out of the influence of the Earth's gravitational field, it needs relatively
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less energy than a stationary object on the Earth's surface that initially
contains no energy.
8.7. Does the escape speed of a body from the earth depend on
(a) the mass of the body
(b) the location from where it is projected
(c) the direction of projection
(d) the height of the location from where the body is launched?
Solution:
(a) No
(b) No
(c) No
(d) Yes
The escape velocity of a body from the Earth is given by the relation:
π£ππ π = β2ππ β¦β¦.(i)
π =Acceleration due to gravity
π = Radius of the Earth
It is clear from equation (i) that escape velocity π£ππ π is independent of the mass of
the body and the direction of its projection. However, at the point where the body
is launched, it depends on the gravitational potential. Because this potential
depends marginally on the height of the point, escape velocity also marginally
depends on these factors.
8.8. A comet orbits the Sun in a highly elliptical orbit. Does the comet have a constant
(a) linear speed
(b) angular speed
(c) angular momentum
(d) kinetic energy
(e) potential energy
(f) total energy throughout its orbit?
Neglect any mass loss of the comet when it comes very close to the Sun.
Solution:
(a) No
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(b) No
(c) Yes
(d) No
(e) No
(f) Yes
At all points of a comet's orbit moving in a highly elliptical orbit around the Sun,
angular momentum and total energy are constant. Its linear speed, angular speed,
kinetic and potential energy vary in the orbit from point to point.
8.9. Which of the following symptoms is likely to afflict an astronaut in space
(a) swollen feet
(b) swollen face
(c) headache
(d) orientational problem?
Solution: (b), (c), and (d)
(a) Due to gravitational pull, the legs hold the entire mass of a body in
standing position. In space, due to the absence of gravity, an astronaut
feels weightlessness. Hence, an astronaut's swollen feet do not affect
him/her in space.
(b) In general, a swollen face is caused by apparent weightlessness in space.
Sense organs like eyes, ears, nose, and mouth constitute a personβs face.
This symptom can affect an astronaut in space.
(c) Due to mental strain, headaches are triggered. It may influence an
astronaut's work in space.
(d) Space has different orientations. Therefore, the orientational problem can
affect an astronaut in space.
8.10. Choose the correct answer from among the given ones:
The gravitational intensity at the centre of a hemispherical shell of uniform mass
density has the direction indicated by the arrow (see Figure) (i) a, (ii) b, (iii) c,
(iv) O.
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Solution: (iii)
The Gravitational potential (V) is constant at all points in a spherical shell. Hence,
the gravitational potential gradient (dV
dr)is zero everywhere inside the spherical
shell. The gravitational potential gradient is equal to the negative of gravitational
intensity. Hence, the intensity is also zero at all points inside the spherical shell.
This indicates that gravitational forces acting at a point in a spherical shell are
symmetric.
If the upper half of a spherical shell is cut out (as shown in the figure in question),
then the net gravitational force acting on a particle in the centre O will be in the
downward direction.
Because at that stage, the gravitational intensity is described as the gravitational
force per unit mass, it will also act in the downward direction. The gravitational
intensity of the given hemispheric shell at centre O, therefore, has the direction
indicated by arrow c.
8.11. Choose the correct answer from among the given ones:
For the problem 8.10, the direction of the gravitational intensity at an arbitrary
point P is indicated by the arrow (i) d, (ii) e, (iii) f, (iv) g.
Solution: (ii)
The gravitational potential (π) is constant at all points in a spherical shell. Hence,
the gravitational potential gradient (ππ
ππ) is zero everywhere inside the spherical
shell. The gravitational potential gradient is equal to the negative of gravitational
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intensity. Therefore, the intensity within the spherical shell is also zero at all
points. This indicates symmetric gravitational forces at a point in a spherical shell.
If the upper half of a spherical shell is cut out (as shown in the figure), then the
net gravitational force at an arbitrary point P will be in the downward direction.
Because at that point, the gravitational intensity is defined as the gravitational
force per unit mass, it will also act in the downward direction. Consequently, the
gravitational intensity of the hemispheric shell at an arbitrary point P has the
direction indicated by arrow e.
8.12. A rocket is fired from the earth towards the sun. At what distance from the earthβs
centre is the gravitational force on the rocket zero?
Mass of the sun = 2 Γ 1030 kg, mass of the earth = 6 Γ 1024 kg. Neglect the
effect of other planets etc. (orbital radius = 1.5 Γ 1011m).
Solution:
Mass of the Sun, Ms = 2 Γ 1030 kg
Mass of the Earth, Me = 6 Γ 1024 kg
Orbital radius, r = 1.5 Γ 1011 m
Mass of the rocket = m
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Let x be the distance from the centre of the Earth where the gravitational force
acting on satellite P becomes zero.
From Newton's gravitational law, under the influence of the Sun and Earth, we
can equate gravitational forces acting on satellite P:
πΊπππ
(π β π₯)2= πΊπ
ππ
π₯2
(π β π₯
π₯)
2
=ππ
ππ
π β π₯
π₯= (
2 Γ 1030
60 Γ 1024)
12
= 577.35
1.5 Γ 1011 β x = 577.35 x
578.35x = 1.5 Γ 1011
x =1.5 Γ 1011
578.35= 2.59 Γ 108 m
8.13. How will you βweigh the sunβ, that is estimate its mass? The mean orbital radius
of the earth around the sun is 1.5 Γ 108 km.
Solution:
The orbital radius of the Earth around the Sun, π = 1.5 Γ 1011 m
Time taken by the Earth to complete a single revolution around the Sun,
π = 1 year = 365.25 days
= 365.25 Γ 24 Γ 60 Γ 60 s
Universal gravitational constant, G = 6.67 Γ 10β11 Nm2 kgβ2
Thus, the mass of the Sun can be calculated using the relation,
π =4Ο2r3
GT2
=4 Γ (3.14)2 Γ (1.5 Γ 1011)3
6.67 Γ (365.25 Γ 24 Γ 60 Γ 60)2
=133.24 Γ 10
6.64 Γ 104= 2.0 Γ 1030 kg
Hence, the mass of the Sun is 2 Γ 1030 kg
8.14. A Saturn year is 29.5 times the earth year. How far is the Saturn from the sun if
the earth is 1.50 Γ 108 km away from the sun?
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Solution:
Given:
The distance of the Earth from the Sun, re = 1.5 Γ 108 km = 1.5 Γ 1011 m
The time period of the Earth = ππ
The time period of Saturn, ππ = 29. 5 ππ
The distance of Saturn from the Sun = ππ
From Keplerβs third law of planetary motion:
π = (4π2π3
πΊπ)
12
For Saturn and Sun, we can write
ππ 3
ππ3 =
ππ 2
ππ2
ππ = ππ (ππ
ππ)
23
= 1.5 Γ 1011 (29.5ππ
ππ)
23
= 1.5 Γ 1011(29.5)23
= 1.5 Γ 1011 Γ 9.55
= 14.32 Γ 1011m
Hence, the distance between Saturn and the Sun is.1.43 Γ 1012 m.
8.15. A body weighs 63 N on the surface of the earth. What is the gravitational force on
it due to the earth at a height equal to half the radius of the earth?
Solution:
Weight of the body, π = 63 N
The relation for acceleration due to gravity at height h from the Earthβs surface:
πβ² =π
(1 + β
π π)
2
Where,
π = Acceleration due to gravity on the Earthβs surface
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π π = Radius of the Earth
For h =π π
2
πβ² =π
(1 +π π
2 Γ π π)
2 =π
(1 +12)
2 =4
9π
The weight of a body of mass m at height h is given as:
πβ² = ππβ²
= π Γ4
9π =
4
9Γ ππ
=4
9π
=4
9Γ 63 = 28 N
8.16. Assuming the earth to be a sphere of uniform mass density, how much would a
body weigh halfway down to the centre of the earth if it weighed 250 N on the
surface?
Solution:
Weight of a body of mass m at the Earthβs surface, W = mπ = 250 N
Body of mass m is located at depth, d =1
2π π
Where,
π π = Radius of the Earth
Acceleration due to gravity at depth g(d) is given by the relation:
πβ² = (1 βπ
π π) π
= (1 βπ π
2 Γ π π) π =
1
2π
Weight of the body at depth d,
Wβ² = mπβ²
= π Γ1
2π =
1
2ππ =
1
2π
=1
2Γ 250 = 125 N
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8.17. A rocket is fired vertically with a speed of 5 km sβ1 from the earthβs surface.
How far from the earth does the rocket go before returning to the earth? Mass of
the earth = 6.0 Γ 1024 kg; mean radius of the earth = 6.4 Γ 106 π; πΊ =6.67 Γ 10β11 N m2 kgβ2.
Solution:
The velocity of the rocket, π£ = 5 km/s = 5 Γ 103 m/s
Mass of the Earth, ππ = 6.0 Γ 1024 kg
The radius of the Earth, π π = 6.4 Γ 106 m
The height reached by rocket mass, π = β
At the surface of the Earth,
The total energy of the rocket = Kinetic energy + Potential energy
=1
2ππ£2 + (β
πΊπππ
π π)
At highest point h,
v = 0
And, Potential energy = βπΊπππ
π π+β
The total energy of the rocket = 0 + (βπΊπππ
π π+β) =
πΊπππ
π π+β
From the law of conservation of energy:
The total energy of the rocket at the Earthβs surface = Total energy at height h
1
2ππ£2 + (β
πΊπππ
π π) = β
πΊπππ
π π + β
1
2π£2 = πΊππ (
1
π πβ
1
π π + β)
1
2π£2 = πΊππ (
π π + β β π π
π π(π π + β))
1
2π£2 =
πΊππβ
π π(π π + β)Γ
π π
π π
1
2Γ π£2 =
ππ πβ
π π + β
Where π =πΊπ
π π2 = 9.8 m/s2 (Acceleration due to gravity on the Earthβs surface)
β΄ π£2(π π + β) = 2ππ πβ
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π£2π π = β = (2ππ π β π£2)
β =π ππ£2
2ππ π β π£2
=6.4 Γ 106 Γ (5 Γ 103)2
2 Γ 9.8 Γ 6.4 Γ 106 β (5 Γ 103)2
β =6.4 Γ 25 Γ 1012
100.44 Γ 106= 1.6 Γ 106m
The height of the rocket in relation to the Earth's center
= π π + β
= 6.4 Γ 106 + 1.6 Γ 106
= 8.0 Γ 106m
8.18. The escape speed of a projectile on the earthβs surface is 11.2 km sβ1. A body is
projected out with thrice this speed. What is the speed of the body far away from
the earth? Ignore the presence of the sun and other planets.
Solution:
The escape velocity of a projectile from the Earth, π£ππ π = 11.2 km/s
Projection velocity of the projectile, π£π = 3 π£ππ π
Mass of the projectile = m
The velocity of the projectile far away from the Earth = π£π
The total energy of the projectile on the Earth =1
2ππ£π
2 β1
2ππ£ππ π
2
The gravitational potential energy of the projectile far away from the Earth is
zero.
The total energy of the projectile far away from the Earth =1
2ππ£π
2
From the law of conservation of energy,
1
2ππ£π
21
2ππ£ππ π
2 =1
2ππ£π
2
π£π = βπ£π2 β π£ππ π
2
=β(3π£ππ π)2 β (π£ππ π)2
= β8 π£ππ π
= β8 Γ 11.2 = 31.68 km/s
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8.19. A satellite orbits the earth at a height of 400 km above the surface. How much
energy must be expended to rocket the satellite out of the earthβs gravitational
influence? Mass of the satellite = 200 kg; mass of the earth = 6.0 Γ 1024 kg;
radius of the earth = 6.4 Γ 106 m; G = 6.67 Γ 10β11 N m2 kgβ2.
Solution:
Mass of the Earth, π = 6.0 Γ 1024 kg
Mass of the satellite, π = 200 kg
The radius of the Earth, π π = 6.4 Γ 106 m
Universal gravitational constant, G = 6.67 Γ 10β11 Nm2 kgβ2
Height of the satellite, β = 400 km = 4 Γ 105 m = 0.4 Γ 106 m
The total energy of the satellite at height h =1
2mv2 + (β
πΊπππ
π π+β)
Orbital velocity of the satellite, v = βπΊππ
π π+β
The total energy of height, β =1
2π (
πΊππ
π π+β) β
πΊπππ
π π+β= β
1
2(
πΊππ
π π+β)
The negative sign indicates that the satellite is bound to the Earth. This is called
bound energy of the satellite.
The energy required to send the satellite out of its orbit = β (Bound energy)
=1
2
πΊπππ
(π π + β)
=1
2Γ
6.67 Γ 10β11 Γ 6.0 Γ 1024 Γ 200
(6.4 Γ 106 + 0.4 Γ 106)
=1
2Γ
6.67 Γ 6 Γ 2 Γ 10
6.8 Γ 106= 5.9 Γ 109J
8.20. Two stars each of one solar mass (= 2 Γ 1030 kg) are approaching each other for
a head-on collision. When they are a distance 109 km, their speeds are negligible.
What is the speed with which they collide? The radius of each star is 104 km.
Assume the stars to remain undistorted until they collide.
(Use the known value of G).
Solution:
Mass of each star, M = 2 Γ 1030 kg
The radius of each star, R = 104 km = 107 m
Distance between the stars, r = 109 km = 1012m
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For negligible speeds, v = 0 total energy of two stars separated at distance r
= βπΊππ
π+
1
2ππ£2
= βπΊππ
π+ 0 β¦..(i)
Now, consider the case when the stars are about to collide:
The velocity of the stars = π£
Distance between the centres of the stars = 2π
The total kinetic energy of both stars =1
2ππ£2 +
1
2ππ£2 = ππ£2
The total potential energy of both stars =βπΊππ
2π
The total energy of the two stars = ππ£2 βπΊππ
2π β¦β¦.(ii)
Using the law of conservation of energy:
ππ£2 βπΊππ
2π =
βπΊππ
π
π£2 =βπΊπ
π+
πΊπ
2π = πΊπ (β
1
π+
1
2π )
= 6.67 Γ 10β11 Γ 2 Γ 1030 [β1
1012+
1
2 Γ 107]
= 13.34 Γ 1019[β10β12 + 5 Γ 10β8]
~13.34 Γ 1019 Γ 5 Γ 10β8
~6.67 Γ 1012
v = β6.67 Γ 1012 = 2.58 Γ 106 m/s
8.21. Two heavy spheres each of mass 100 kg and radius 0.10 m are placed 1.0 m
apart on a horizontal table. What is the gravitational force and potential at the mid
point of the line joining the centres of the spheres? Is an object placed at that point
in equilibrium? If so, is the equilibrium stable or unstable?
Solution:
0;
β2.7 Γ 10β8 J/kg;
Yes;
Unstable
Explanation:
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The situation is represented in the given figure:
Mass of each sphere, M = 100 kg
The separation between the spheres, r = 1m
X is the midpoint between the spheres. Gravitational force at point X will be zero.
This is because the gravitational force exerted by each sphere will act in opposite
directions.
Gravitational potential at point X:
= βπΊπ
(π2)
βπΊπ
(π2)
= β4πΊπ
π
=4 Γ 6.67 Γ 10β11 Γ 100
1
= β2.67 Γ 10β8 J/kg
Any object placed at point X will be in an equilibrium state, but the equilibrium is
unstable. This is because any change in the position of the object will change the
effective force in that direction.
8.22. As you have learnt in the text, a geostationary satellite orbits the earth at a height
of nearly 36,000 km from the surface of the earth. What is the potential due to
earthβs gravity at the site of this satellite? (Take the potential energy at infinity to
be zero).
Mass of the earth = 6.0 Γ 1024 kg,
radius = 6400 km.
Solution:
Mass of the Earth, π = 6.0 Γ 1024 kg
The radius of the Earth, π = 6400 km = 6.4 Γ 106 m
A geostationary satellite's height from the earth's surface,
β = 36000 km = 3.6 Γ 107 m
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The gravitational potential energy due to Earthβs gravity at height β,
=βGM
(R + h)
= β6.67 Γ 10β11 Γ 6.0 Γ 1024
3.6 Γ 107 + 0.64 Γ 107
= β6.67 Γ 6
4.24Γ 1013β7
= β9.4 Γ 106 J kgβ
8.23. A star 2.5 times the mass of the sun and collapsed to a size of 12 km rotates with
a speed of 1.2 rev. per second. (Extremely compact stars of this kind are known
as neutron stars.Certain stellar objects called pulsars belong to this category). Will
an object placed on its equator remain stuck to its surface due to gravity? (Mass of
the sun = 2 Γ 1030 kg).
Solution:
Yes
A body gets stuck to the surface of a star if the inward gravitational force is
greater than the outward centrifugal force caused by the rotation of the star.
Gravitational force, ππ =πΊππ
π 2
Where,
π = Mass of the star = 2.5 Γ 2 Γ 1030 = 5 Γ 1030 kg
π = Mass of the body
π = Radius of the star = 12 km = 1.2 Γ 104 m
β΄ ππ =6.67 Γ 10β11 Γ 5 Γ 1030 Γ π
(1.2 Γ 104)2= 2.31 Γ 1011π π
Centrifugal force, ππ = πππ2
where,
π =Angular speed = 2ΟΞ½
Ξ½ = Angular frequency = 1.2 πππ£ π β1
ππ = ππ (2ΟΞ½)2
= m Γ (1.2 Γ 104) Γ 4 Γ (3.14)2 Γ (1.2)2 = 1.7 Γ 105mN
Since ππ > ππ, the body will remain stuck to the surface of the star.
Class- XI-CBSE-Physics Gravitation
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8.24. A spaceship is stationed on Mars. How much energy must be expended on the
spaceship to launch it out of the solar system? Mass of the space ship = 1000 kg;
mass of the Sun = 2 Γ 1030 kg; mass of mars = 6.4 Γ 1023 kg; radius of mars =3395 km; radius of the orbit of mars = 2.28 Γ 108kg; G = 6.67 Γ10β11m2kgβ2.
Solution:
Mass of the spaceship, ππ = 1000 ππ
Mass of the Sun, π = 2 Γ 1030 ππ
Mass of Mars, ππ = 6.4 Γ 1023 ππ
The orbital radius of Mars, π = 2.28 Γ 108ππ = 2.28 Γ 1011π
The radius of Mars, π = 3395 ππ = 3.395 Γ 106 π
Universal gravitational constant, πΊ = 6.67 Γ 10β11 π2ππβ2
The potential energy of the spaceship due to the gravitational attraction of the Sun
=βπΊπππ
π
The potential energy of the spaceship due to the gravitational attraction of Mars =βπΊππππ
π
Since the spaceship is stationed on Mars, its velocity and therefore its kinetic
energy will be zero
The total energy of the spaceship =βπΊπππ
π β
βπΊππ ππ
π
= βπΊππ (π
π +
ππ
π)
The negative sign indicates that the system is in bound state.
The energy required for launching the spaceship out of the solar system
= β (Total energy of the spaceship)
= πΊππ (π
π +
ππ
π)
= 6.67 Γ 10β11 Γ 103 Γ (2 Γ 1030
2.28 Γ 1011+
6.4 Γ 1023
3.395 Γ 106)
= 6.67 Γ 10β8 Γ (87.72 Γ 1017 + 1.88 Γ 1017)
= 6.67 Γ 10β8 Γ 89.50 Γ 1017
= 596.97 Γ 109
Class- XI-CBSE-Physics Gravitation
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= 6 Γ 1011J
8.25. A rocket is fired βverticallyβ from the surface of Mars with a speed of 2 km sβ1. If
20% of its initial energy is lost due to Martian atmospheric resistance, how far
will the rocket go from the surface of Mars before returning to it? Mass of mars =6.4 Γ 1023 ππ; radius of mars = 3395 km; G = 6.67 Γ 10β11 N m2 kgβ2.
Solution:
Initial velocity of the rocket, v = 2 km/s = 2 Γ 103 m/s
Mass of Mars, M = 6.4 Γ 1023 kg
The radius of Mars, R = 3395 km = 3.395 Γ 106 m
Universal gravitational constant, G = 6.67 Γ 10β11 N m2 kgβ2
Mass of the rocket = m
The initial kinetic energy of the rocket =1
2ππ£2
The initial potential energy of the rocket =βπΊππ
π
Total initial energy =1
2ππ£2 β
πΊππ
π
If 20% of the initial kinetic energy is lost because of Martian atmospheric
resistance, then only 80 % of its kinetic energy will help to reach a height.
Total initial energy available =80
100Γ
1
2ππ£2 β
πΊππ
π = 0.4 ππ£2 β
πΊππ
π
The maximum height reached by rocket = β
At this height, the velocity and therefore the rocket's kinetic energy will be zero.
The total energy of the rocket at height β =πΊππ
(π +β)
By applying the law of conservation of energy for the rocket, we can write:
0.4ππ£2 βπΊππ
π = β
βπΊππ
(π + β)
0.4π£2 =πΊπ
π β
πΊπ
π + β
0.4π£2 = πΊπ (1
π β
1
π + β)
0.4π£2 = πΊπ (π + β β π
π (π + β))
0.4π£2 =πΊπβ
π (π + β)
Class- XI-CBSE-Physics Gravitation
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π + β
β=
πΊπ
0.4π£2π
π
β+ 1 =
πΊπ
0.4π£2π
π
β=
πΊπ
0.4π2π β 1
β =π
πΊπ0.4π£2π
β 1
β =0.4π 2π£2
πΊπ β 0.42π
β =0.4 Γ (3.395 Γ 106)2 Γ (2 Γ 103)2
6.67 Γ 10β11 Γ 6.4 Γ 1023 β 0.4 Γ (2 Γ 103)2 Γ (3.395 Γ 106)
β =18.442 Γ 1018
42.688 Γ 10β12 β 5.432 Γ 1012=
18.442
37.256Γ 106
β = 495 Γ 103π = 495 km
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