A body is projected vertically upwards from the surface of a planet of radius \(R\) with a velocity equal to half the escape velocity for that planet. The maximum height attained by the body is:
1. \(\frac{R}{3}\)
2. \(\frac{R}{2}\)
3. \(\frac{R}{4}\)
4. \(\frac{R}{5}\)
A satellite is launched into a circular orbit of radius \(R\) around the Earth while a second satellite is launched into an orbit of radius \(1.02~\text{R}\). The percentage difference in the time periods of the two satellites is:
1. | \(0.7\) | 2. | \(1.0\) |
3. | \(1.5\) | 4. | \(3\) |
Distance of geostationary satellite from the center of the Earth in terms of is-
(1)
(2)
(3)
(4)
Energy required to move a body of mass m from an orbit of radius 2R to 3R is
(1)
(2)
(3)
(4)
If the radius of the earth contracts by 2% and its mass remains the same, then weight of the body at the earth surface :
(1) Will decrease
(2) Will increase
(3) Will remain the same
(4) None of these
The kinetic energy needed to project a body of mass m from the earth surface (radius R) to infinity is -
(1) mgR/2
(2) 2 mgR
(3) mgR
(4) mgR/4
A satellite is to revolve round the earth in a circle of radius 8000 km. The speed at which this satellite be projected into an orbit, will be
(1)
(2) 16 km/s
(3) 7.15 km/s
(4) 8 km/s
If the mass of a body is M on the earth surface, then the mass of the same body on the moon surface is:
(1) M/6
(2) Zero
(3) M (4) None of these
Radius of orbit of satellite of earth is R. Its kinetic energy is proportional to -
1.
2.
3. R
4.
A particle falls towards earth from infinity. It’s velocity on reaching the earth would be -
(1) Infinity
(2)
(3)
(4) Zero