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All questions of Gravitation for Class 11 Exam

Two bodies with same mass “m” separated by a distance “r” exert a gravitational force of F on each other. Suppose the distance between them is doubled and the force becomes F’. The ratio of two forces is
  • a)
    1:4
  • b)
    4:1
  • c)
    1:2
  • d)
    2:1
Correct answer is 'B'. Can you explain this answer?

Niharika Nair answered
We know that the force of gravitation is inversely proportional to square of the distance between the two bodies,
i.e. F∝ r-2
Hence, when the distance between them will be doubled, the force will be reduced by 4 times
So, the ratio will be 4:1

 Which is untrue about orbital velocity?
  • a)
    increases with the increase in height of satellite
  • b)
    depends on mass and radius of planet around which it revolves
  • c)
    it is independent of mass of satellite
  • d)
    decreases with an increase in radius of orbit
Correct answer is option 'A'. Can you explain this answer?

Om Desai answered
The untrue statement about orbital velocity is:

1. increases with the increase in height of satellite

Explanation: Orbital velocity is the speed at which an object revolves around a planet or other celestial body in a stable orbit. According to the equation for orbital velocity, v = √(GM/r+h), where G is the gravitational constant, M is the mass of the planet, and r is the radius of the orbit.

As the height of the satellite increases (meaning it gets far to the planet), its h increase , so reasulting in decrease in velocity .

The other statements are true:

2. depends on mass and radius of planet around which it revolves: As mentioned in the equation, orbital velocity depends on both the mass (M) of the planet and the radius (r) of the orbit.

3. it is independent of mass of satellite: The mass of the satellite does not appear in the equation for orbital velocity, so it does not affect the speed at which the satellite orbits the planet.

4. decreases with an increase in radius of orbit: From the equation, we can see that as the radius of the orbit (r) increases, the orbital velocity (v) decreases.

Assuming the earth to be a sphere of uniform density the acceleration due to gravity
  • a)
    At a point outside the earth is inversely proportional to the square of its distance from the center
  • b)
     At a point outside the earth is inversely proportional to its distance from the centre
  • c)
    At a point inside is zero
  • d)
    At a point inside is proportional to its distance from the centre
Correct answer is option 'A,D'. Can you explain this answer?

Krishna Iyer answered
As g is inversely proportional to (R+h)2 when we go away from earth's surface g is inversely proportional to square of the distance and g is directly proportional to (R-d) when we go inside the surface of Earth therefore g is directly proportional to distance travelled inside the Earth
g=Gmr/a3=r for r<R
g=Gm/a2 for r<R

The escape velocity for the moon is nearly
  • a)
    11.2km/s
  • b)
    2.4km/s
  • c)
    24km/s
  • d)
    10km/s
Correct answer is option 'B'. Can you explain this answer?

Rohit Shah answered
About 11.2 km/s
In common usage, the initial point is on the surface of a planet or moon. On the surface of the Earth, the escape velocity is about 11.2 km/s, which is approximately 33 times the speed of sound (Mach 33) and several times the muzzle velocity of a rifle bullet (up to 1.7 km/s).

A satellite which appears to be at a fixed position at a definite height to an observer is called:
  • a)
    Geostationary satellite and geosynchronous satellite
  • b)
    Polar satellite
  • c)
    Geostationary satellite
  • d)
    Geosynchronous satellite
Correct answer is option 'A'. Can you explain this answer?

Neha Joshi answered
As the relative velocity of the satellite with respect to the earth is zero, it appears stationary from the Earth surface and therefore it is called is geostationary satellite or geosynchronous satellite.

The gravitational potential due to the gravitational force on the earth is defined as the
  • a)
    potential energy multiplied by the mass of the object
  • b)
    potential energy of the mass placed at that point
  • c)
    numerically equal to the potential energy
  • d)
    potential energy of a unit mass at that point.
Correct answer is option 'D'. Can you explain this answer?

Nandini Patel answered
Gravitational Potential
Gravitational Potential is dened as the potential energy of a particle of unit mass at that point due to the gravitational force exerted byearth. Gravitational potential energy of a unit mass is known as gravitational potential.

What could be the maximum value for gravitational potential energy?
  • a)
    1
  • b)
    zero
  • c)
    infinity
  • d)
    1000
Correct answer is option 'B'. Can you explain this answer?

Riya Banerjee answered
As, U=−Gm1m2/r, 
it can be used to describe the potential energy in a system of point charges (or radially symmetric spheres) as a function of their separation distance r, then the maximum value is zero at infinite separation.
Hence, its maximum value is zero at infinity.
 

When a satellite moves in a circular orbit, the _______acceleration is provided by the gravitational attraction of the earth
  • a)
    tangential
  • b)
    centrifugal
  • c)
    centripetal
  • d)
    fictitious
Correct answer is option 'C'. Can you explain this answer?

Hansa Sharma answered
When any body or particle moves in circular orbit centripetal force acts on it and to move the object centripetal acceleration is necessary. So, when a satellite moves in circular orbit the centripetal acceleration is provided by the gravitational attraction of the earth.

Kepler’s second law states that the straight line joining the planet to the sun sweeps out equal areas in equal time. The statement is equivalent to saying that:
  • a)
    longitudnal acceleration is zero
  • b)
    total acceleration is zero
  • c)
    transverse acceleration is zero
  • d)
    radial acceleration is zero
Correct answer is option 'C'. Can you explain this answer?

Suresh Reddy answered
According to the second law the orbital radius and angular velocity of the planet in the elliptical orbit will vary. The planet travels faster when closer to the Sun, then slower when farther from the Sun. Hence we can say that the transverse acceleration is zero while radial and longitudinal accelerations are not zero.

Velocity of geostationary satellite with respect to earth is
  • a)
    10 ms-1
  • b)
    15 ms-1
  • c)
    zero
  • d)
    1 ms-1
Correct answer is option 'C'. Can you explain this answer?

Neha Joshi answered
Because geostationary satellite ( completes it's rotation in about 24hrs).and it's rotation cycle is same as that of Earth .thus it's velocity is zero with respect to earth

 The mass and diameter of a planet are twice those of earth. What will be the period of oscillation of a pendulum on this planet if it is a seconds pendulum on earth ?
  • a)
      second
  • b)
      seconds
  • c)
     second
  • d)
    second
Correct answer is option 'B'. Can you explain this answer?

Pooja Shah answered
As Mp​=2Me​ and Dp​=2De
or Rp​=2Re​
Hence, gp​= GMp/(Rp​)2 ​​=G(2Me​)/(2Re​)2 ​= GMe/2Re2​ ​​=ge/2​​
Time period of pendulum on the planet  Tp​=2π√ l/gp​
Tp​=2π√​2l/ge​​=√2​×2π√l/ge​=√2​×Te
Tp​=√2​×2=2√2​s

An earth satellite is moved from one stable circular orbit to a farther stable circular orbit. which one of following quantity increases
  • a)
    gravitational potential energy
  • b)
    centripetal acceleration
  • c)
    gravitationl force
  • d)
    linear orbital speed
Correct answer is option 'A'. Can you explain this answer?

Neha Joshi answered
We know that gravitational potential is negative in sign and its magnitude decreases when distance from the massive attracting object increases, hence when considered with sign we can say that gravitational potential increases with increases in distance.

If a satellite orbits as close to the earth's surface as possible,
  • a)
     Its speed is maximum
  • b)
    Time period of its rotation is minimum
  • c)
    The total energy of the `earth plus satellite' system is minimum
  • d)
    The total energy of the `earth plus satellite' system is maximum
Correct answer is option 'A,B,C'. Can you explain this answer?

Hansa Sharma answered
The velocity of satellite V=√GM​/R​⇒V∝1/√R​​. 
The time period of satellite is given by  T=2π√ R3/GM​​⇒T∝R1.5
The total energy is given by  T.E.=−GMm/2R​⇒T.E.∝−1/M​ 
Here, G is constant, R is orbital radius, M is mass of earth and m is mass of satellite.
Near the earth surface, R has the least value and therefore time period and total energy are minimum while velocity is maximum. So, options A, B, C are correct.
 

Satellites A and B are orbiting around the earth in orbits of ratio R and 4R respectively. The ratio of their areal velocities is
  • a)
    1 : 2
  • b)
    1 : 4
  • c)
    1 : 8
  • d)
    1 : 16
Correct answer is option 'A'. Can you explain this answer?

Gaurav Kumar answered
Answer :- a
Solution :- L = mvr
⇒L=m√GMr/r 
L = m√GMr−−−−.....(1)
L = 2mdA/dt....(2)
From (1) and (2)
dA/dt ∝ (r)^1/2
= √(dA/dt)1/(dA/dt)2
= √4/1 = 2/1

Gravitational Potential is:
  • a)
    negative, scalar quantity , unit JKg-1
  • b)
    positive, vector quantity , unit JKg-1
  • c)
    positive, scalar quantity , unit JKg-1
  • d)
    negative, vector quantity , unit JKg-1
Correct answer is option 'A'. Can you explain this answer?

Ayush Joshi answered
Gravitational potential (radial fields) at a point in a radial field is the work done per unit mass against the field, in bringing a small mass from infinite distance to the point. Since gravitational fields are attractive and the potential at infinite distance is zero, all points within the field have negative values of potential. Gravitational potential is a scalar quantity with SI unit J kg^-1. The symbol used is mostly V but sometimes or Vr or V(r). A radial gravitational field is one in which the field strength has the same magnitude at all points at a given distance from the center. 

The energy required to be spent by a satellite of mass m and speed v and orbital radius r in completing a circular orbit once round the earth of mass M is
  • a)
    GMm/r
  • b)
    2GMm/r
  • c)
    GMm/2r
  • d)
    zero
Correct answer is 'D'. Can you explain this answer?

Suresh Iyer answered
As the satellite is bounded by earth's gravitational field and has some velocity, it would completely revolve around the circular orbit without any external energy required.

If a tunnel is cut at any orientation through earth, then a ball released from one end will reach the other end in time (neglect earth rotation)
  • a)
    84.6 minutes 
  • b)
    42.3 minutes
  • c)
    8 minutes 
  • d)
    Depends on orientation
Correct answer is option 'B'. Can you explain this answer?

Neha Joshi answered
Total time period will be 84.6 min when ball released from one end and it come backs to same point as in oscillation.
When ball is released from one end then time taken to reach other end will be half of total time period then that will be 42.3 min.
 

 When a satellite in a circular orbit around the earth enters the atmospheric region, it encounters small air resistance to its motion. Then
  • a)
     Its kinetic energy increases
  • b)
    Its kinetic energy decreases
  • c)
    Its angular momentum about the earth decreases
  • d)
    Its period of revolution around the earth increases
Correct answer is option 'A'. Can you explain this answer?

Hansa Sharma answered
Due to air drag some mechanical energy of satellite will converted into heat energy, there will be loss of ME of satellite, so radius of orbit will decrease and satellite will follow a spiral path towards earth. 
If r is decreases,
P.E.=−GMm​/r, P.E. is also decreases.
K.E=GMm​/2r K.E increasing, increased speed in spite of decrease in M.E. But rate of P.E decreases is more than the rate at which M.E decreases.
Angular momentum L=mrv=mr√GM​r=m√GMr​⇒L∝√r​.
So, angular momentum decreases as r decreases.

The height at which the acceleration due to gravity becomes g/9 (where g = the acceleration due to gravity on the surface of the earth) in terms of R, the radius of the earth, is
  • a)
     R/2
  • b)
    2R
  • c)
    R/3
  • d)
    3R
Correct answer is option 'B'. Can you explain this answer?

Bhargavi Sen answered
To find the height at which the acceleration due to gravity becomes g/9, let's analyze the gravitational force equation.

Gravitational force (F) between two objects is given by:
F = (G * m1 * m2) / r^2

where G is the gravitational constant, m1 and m2 are the masses of the two objects, and r is the distance between their centers.

The acceleration due to gravity (g) is the force experienced by an object of mass m due to the gravitational attraction of the Earth. It is given by:
g = (G * M) / R^2

where M is the mass of the Earth and R is the radius of the Earth.

Since the acceleration due to gravity is directly proportional to the mass of the Earth and inversely proportional to the square of the radius, we can write:
g' = (G * M') / (R')^2

where g' is the new acceleration due to gravity, M' is the new mass of the Earth, and R' is the new radius of the Earth.

We are given that g' = g/9. Substituting this into the equation above, we get:
g/9 = (G * M') / (R')^2

Simplifying, we find:
(R')^2 = (9 * M' * R^2) / (G * M)

To find the height at which the acceleration due to gravity becomes g/9, we need to find the difference between the new radius (R') and the original radius (R). Let's call this difference ΔR.

ΔR = R' - R

Now, let's substitute the expression for (R')^2 into the equation for ΔR:

ΔR = sqrt((9 * M' * R^2) / (G * M)) - R

Since the new mass M' is the same as the original mass M (since we are still considering the Earth), we can simplify further:

ΔR = sqrt((9 * R^2) / G) - R

To find the height, we need to multiply ΔR by the radius of the Earth, R:

Height = R * ΔR

Substituting the expression for ΔR, we get:

Height = R * (sqrt((9 * R^2) / G) - R)

Simplifying further, we find:

Height = R * (3R / sqrt(G) - R)

Since G is a constant, the height can be written as:

Height = 3R - R^2 / sqrt(G)

Therefore, the height at which the acceleration due to gravity becomes g/9 is given by 3R - R^2 / sqrt(G), which is equivalent to option B, 2R.

A satellite of mass 5M orbits the earth in a circular orbit. At one point in its orbit, the satellite explodes into two pieces, one of mass M and the other of mass 4M. After the explosion the mass M ends up travelling in the same circular orbit, but in opposite direction. After explosion the mass 4M is in
  • a)
    Bound orbit 
  • b)
    Unbound orbit
  • c)
    Partially bound orbit
  • d)
    Data is insufficient to determine the nature of the orbit
Correct answer is option 'B'. Can you explain this answer?

Suresh Reddy answered
Applying the conservation of momentum, we get:
V = velocity of 5M, V1 = velocity of 4M, V2 = velocity of M and ATQ V2 = -V
5MV = 4MV1 + M(-V)
6MV = 4MV1
V1 = 3/2 V
Now, Vo = orbital velocity and Ve = escape velocity
Ve = √2 Vo 
In a bound orbit the object is gravitationally bound to the body that is the source of gravity (like the Earth is bound to the Sun, or the Moon to the Earth). An unbound orbit is typically hyperbolic, and the object will escape from the source of gravity
 

A satellite S is moving in an elliptical orbit around the earth. The mass of the satellite is very small compared to the mass of the earth
  • a)
    The acceleration of S is always directed towards the centre of the earth
  • b)
    The angular momentum of S about the centre of the earth changes in direction, but its magnitude remains constant
  • c)
    The total mechanical energy of S varies periodically with time
  • d)
    The linear momentum of S remains constant in magnitude
Correct answer is option 'A'. Can you explain this answer?

Bhavana Tiwari answered
As the gravitational force on satellites due to earth acts always towards the centre of earth, thus acceleration of S is always directed towards the centre of the earth.
Also, as there is no external force so according to conservation of energy, total mechanical energy of S is constant always.
Also, as in the absence of external torque L is constant in magnitude and direction.
Thus, mrv=constant ⟹v varies as r changes
Hence, p=mv is not constant.

The earth's gravitational force at someplace in space causes an acceleration of 7m/s2 in a 1kg mass.What will be the acceleration of a 5kg mass at the same place?
  • a)
    7m/s2
  • b)
    35m/s2
  • c)
    1.4m/s2
  • d)
    3.5m/s2
Correct answer is option 'A'. Can you explain this answer?

Hansa Sharma answered
The acceleration due to gravity does not vary with the change in the mass of the object as it is a dimensionless quantity representing the amount of matter in a particle or object.
Therefore, the acceleration of a 5 kg mass at the same place is 7m/s2.

The orbit of a planet P round the sun S. AB and CD are the minor and major axes of the ellipse.
              
 If t1 is the time taken by the planet to travel along ACB and t2 the time along BDA, then
  • a)
     t1 = t2
  • b)
    t1 > t2
  • c)
     t1 < t2
  • d)
    Nothing can be concluded
Correct answer is option 'B'. Can you explain this answer?

Pooja Shah answered
Here, the angular momentum is conserved i.e. mvr is constant. Where r is the distance from centre of the sun to centre of the planet.
Now, consider one point each from both the mentioned paths. (Shown in fig.)
Applying conservation of angular momentum for these points we get 
mv1​r1​=mv2​r2​. Simplifying this, v1/​v2​​=r2​/r1​​<1
Time period are given by 
t1​=L/ v1​, t2​= L​/ v2
Comparing them by taking the ratio 
t1/t2​​=(L​/ v1)×(v2/L)
So, t1/t2=v2​/v1​​>1.Thus t1​>t2

 In side a hollow spherical shell
  • a)
    Everywhere gravitational potential is zero 
  • b)
    Everywhere gravitational field is zero
  • c)
     Everywhere gravitational potential is same
  • d)
    Everywhere gravitational field is same
Correct answer is option 'B,C,D'. Can you explain this answer?

Lavanya Menon answered
The gravitational field inside a uniform spherical shell is 0 from gauss law for gravitation since no mass is enclosed in any Gaussian surface.
Since gravitational potential is given by φ=−∫ gdr, hence, φ=constant since g=0.
Since the gravitational field is 0 everywhere, it is apparently the same everywhere.
Answer is B,C,D.

The earth attracts the moon with a gravitational force of 1020 N. Then the moon attracts the earth with the gravitational force of  
  • a)
    10-20 N
  • b)
    10-2 N
  • c)
    1020 N
  • d)
    None of the above
Correct answer is option 'C'. Can you explain this answer?

The universal law of gravitation:
  • Sir Isaac Newton put forward the universal law of gravitation in 1687 and used it to explain the observed motions of the planets and moons.
  • The law states that every particle attracts every other particle in the universe with force directly proportional to the product of the masses and inversely proportional to the square of the distance between them.
  • Formula, Gravitational force,  where, F is the gravitational force between bodies, m1, and m2 are the masses of the bodies, d is the distance between the centers of two bodies, and G is the universal gravitational constant.
  • Here, universal gravitational constant, G = 6.67 × 10-11 Nm/kg2
  • The Universal Gravitational Law can explain almost anything, right from how an apple falls from a tree to why the moon revolves around the Earth.
Newton's third law of motion
  • It states that for every action, there is an equal and opposite reaction.
  • Action and reaction always act on two different bodies.
Explanation:
By Newton's Third Law and Newton's Law of Universal gravitation, the gravitational force the Earth exerts on the Moon is exactly the same as the force the Moon exerts on the Earth. 
F(Earth) = F(Moon)
Therefore, the moon attracts the earth with a gravitational force of 1020N.

What is gravitational potential?
  • a)
    It is defined as the work done in taking a unit mass from one point to that point
  • b)
    It is defined as the work done in taking a unit mass from infinity to that point
  • c)
    It is defined as the energy spent in taking a unit mass from infinity to that point.
  • d)
    none
Correct answer is option 'B'. Can you explain this answer?

Sanjana Bajaj answered
Understanding Gravitational Potential
Gravitational potential is a fundamental concept in physics, particularly in the study of gravitation and fields. It provides insight into how gravity influences mass in a gravitational field.

Definition of Gravitational Potential
- Gravitational potential at a point in a gravitational field is defined as:
- **The work done in bringing a unit mass from infinity to that point.**
This definition emphasizes that gravitational potential is concerned with the energy required to move an object within a gravitational field.

Why Option B is Correct
- The reason option 'B' is correct can be broken down as follows:
- **Reference Point:** The choice of infinity as a reference point is crucial because at infinity, the gravitational force is effectively zero. This allows us to measure the potential energy relative to a point where gravitational effects can be ignored.
- **Work Done:** The work done against gravitational attraction as an object is brought from infinity to a specified point quantifies the gravitational potential at that point. This work is converted into gravitational potential energy.

Other Options Explained
- **Option A:** Incorrect because it does not specify the reference point (infinity), which is essential for defining gravitational potential.
- **Option C:** While it mentions energy, it inaccurately describes the nature of work done. Gravitational potential is specifically about work done on a unit mass.
- **Option D:** Incorrect as option 'B' is indeed the correct answer.

Conclusion
Understanding gravitational potential is vital for grasping concepts in classical mechanics, as it helps predict the behavior of objects under the influence of gravity.

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