12th Grade > Physics
GRAVITATION THE LAW OF FALLING MCQs
Total Questions : 30
| Page 2 of 3 pages
Answer: Option C. -> 2 Eo
:
C
Potential energy =2 × (Total energy)=2Eo
Becuase we know =U=−GMmr and Eo=−GMm2r
:
C
Potential energy =2 × (Total energy)=2Eo
Becuase we know =U=−GMmr and Eo=−GMm2r
Answer: Option B. -> The earth's angular momentum remains constant
:
B
Kinetic and potential energies varies with position of earth w.r.t. sun. Angular momentum remains constant every where.
:
B
Kinetic and potential energies varies with position of earth w.r.t. sun. Angular momentum remains constant every where.
Answer: Option A. -> 2√Gd(M1+M2)
:
A
Gravitational potential at mid point
V=−GM1d2+−GM2d2
Now, PE=m×V=frac−2Gmd(M1+M2)
[m = mass of particle]
So, for projecting particle from mid point to infinity
KE=|PE|
⇒12mv2=2GMd(M1+M2)⇒v=2√G(M1+M2)d
:
A
Gravitational potential at mid point
V=−GM1d2+−GM2d2
Now, PE=m×V=frac−2Gmd(M1+M2)
[m = mass of particle]
So, for projecting particle from mid point to infinity
KE=|PE|
⇒12mv2=2GMd(M1+M2)⇒v=2√G(M1+M2)d
Answer: Option A. -> −5000J
:
A
Given, escape velocity, ve=100ms−1, mass of the body, m=1kg
We know universal gravitational constant, G=6.67×10−11Nm2kg−2.
Let M be the mass of the planet and R be the radius of the planet and U be the gravitational potential energy.
We know, ve=√2GMR=100
⇒10000=2GMR⇒GMR=5000
Potential energy, U=−GMmR=5000×1=−5000J
:
A
Given, escape velocity, ve=100ms−1, mass of the body, m=1kg
We know universal gravitational constant, G=6.67×10−11Nm2kg−2.
Let M be the mass of the planet and R be the radius of the planet and U be the gravitational potential energy.
We know, ve=√2GMR=100
⇒10000=2GMR⇒GMR=5000
Potential energy, U=−GMmR=5000×1=−5000J
Answer: Option A. -> The acceleration of S is always directed towards the centre of the earth
:
A
The satellite revolves around the earth due to gravitational force that acts towards the centre of the earth. And according to the Kepler's laws the angular momentum of the satellite reamains constant but not the linear momentum
:
A
The satellite revolves around the earth due to gravitational force that acts towards the centre of the earth. And according to the Kepler's laws the angular momentum of the satellite reamains constant but not the linear momentum
Answer: Option C. -> R
:
C
v=v0=ve√2 (orbital speed v0 of a satellit near the earth's surface is equal to 1√2 times the escape velocity of a particle on earth's surface)
Now from conservetion of mechanical energy:
Decrease in kinetic energy = increase in potential energy
or 12mv2e2=mgh(1+hR)
or 12m(2gR2)=mgh(1+hR)
or h = R
:
C
v=v0=ve√2 (orbital speed v0 of a satellit near the earth's surface is equal to 1√2 times the escape velocity of a particle on earth's surface)
Now from conservetion of mechanical energy:
Decrease in kinetic energy = increase in potential energy
or 12mv2e2=mgh(1+hR)
or 12m(2gR2)=mgh(1+hR)
or h = R
Answer: Option B. -> P will run faster than S
:
B
g=43πρGR. If density is same then g∝R According to problem Rp=2Re∴gp=2ge
For clock P (based on pendulum motion) T=2π√lg
Time period decreases on planet so it will run faster because gp>ge
For clock S (based on oscillation of spring) T=2π√mk
So it does not change.
:
B
g=43πρGR. If density is same then g∝R According to problem Rp=2Re∴gp=2ge
For clock P (based on pendulum motion) T=2π√lg
Time period decreases on planet so it will run faster because gp>ge
For clock S (based on oscillation of spring) T=2π√mk
So it does not change.
Answer: Option A. -> T
:
A
Time period of satellite which is very near to planet
T=2π√R3GM=2π√R3G43πR3ρ∴T∝√1ρ
i.e. time period of nearest satellite does not depends upon the radius of planet, it only depends upon the density of the planet. In the problem, density is same so time period will be same.
:
A
Time period of satellite which is very near to planet
T=2π√R3GM=2π√R3G43πR3ρ∴T∝√1ρ
i.e. time period of nearest satellite does not depends upon the radius of planet, it only depends upon the density of the planet. In the problem, density is same so time period will be same.
Answer: Option B. -> x=2h
:
B
The value of g at the height h from the surface of earth
g′=g(1−2hR)
The value of g at depth x below the surface of earth
g′=g(1−xR)
These two are given equal, hence g′=g(1−2hR)=g′=g(1−xR)
On solving, we get x=2h
:
B
The value of g at the height h from the surface of earth
g′=g(1−2hR)
The value of g at depth x below the surface of earth
g′=g(1−xR)
These two are given equal, hence g′=g(1−2hR)=g′=g(1−xR)
On solving, we get x=2h
Answer: Option D. -> R2
:
D
g=43πρGR⇒RpRe=(gpge)(ρeρp)=(1)×(12)⇒Rp=Re2=R2
:
D
g=43πρGR⇒RpRe=(gpge)(ρeρp)=(1)×(12)⇒Rp=Re2=R2