A satellite is moving very close to a planet of density \(\rho.\) The time period of the satellite is:
1. \(\sqrt{\frac{3 \pi}{ρG}}\)
2. \(\left(\frac{3 \pi}{ρG}\right)^{3 / 2}\)
3. \(\sqrt{\frac{3 \pi}{2 ρG}}\)
4. \(\left(\frac{3 \pi}{2 ρG}\right)^{3 / 2}\)
1. | \(T\) is conserved |
2. | \(V\) is always positive |
3. | \(E\) is always negative |
4. | the magnitude of \(L\) is conserved but its direction changes continuously |
Magnitude of potential energy (\(U\)) and time period \((T)\) of a satellite are related to each other as:
1. \(T^2\propto \frac{1}{U^{3}}\)
2. \(T\propto \frac{1}{U^{3}}\)
3. \(T^2\propto U^3\)
4. \(T^2\propto \frac{1}{U^{2}}\)
Weightlessness experienced while orbiting the earth in a space-ship is the result of:
1. Inertia
2. Acceleration
3. Zero gravity
4. Freefall towards the earth
The time period of a simple pendulum on a freely moving artificial satellite is
1. Zero
2. 2 sec
3. 3 sec
4. Infinite
The centripetal force acting on a satellite orbiting round the earth and the gravitational
force of earth acting on the satellite both equal F. The net force on the satellite is
1. Zero
2. F
3.
4. 2 F
Reason of weightlessness in a satellite is:
1. Zero gravity
2. Centre of mass
3. Zero reaction force by satellite surface
4. None
If r represents the radius of the orbit of a satellite of mass m moving around a planet of
mass M, the velocity of the satellite is given by:
1.
2.
3.
4.
A satellite which is geostationary in a particular orbit is taken to another orbit. Its
distance from the centre of earth in new orbit is 2 times that of the earlier orbit. The time
period in the second orbit is:
1. 4.8 hours
2. hours
3. 24 hours
4. hours
An astronaut orbiting the earth in a circular orbit 120 km above the surface of earth, gently drops a spoon out of space-ship. The spoon will
1. Fall vertically down to the earth
2. Move towards the moon
3. Will move along with space-ship
4. Will move in an irregular way then fall down