Home
Class 11
PHYSICS
Two small satellies move in a circular o...

Two small satellies move in a circular orbits around the earth, at disatnce `r` and `(r + dr)` from the centre of the earth. Their time periods of rotation ate `T` and `T + dT (Delta r lt lt b r, DeltaT lt lt T)`. Then

A

`DeltaT = (3)/(2)T (Delta r)/(r )`

B

`DeltaT = (-3)/(2)T (Delta r)/(r )`

C

`DeltaT = (2)/(3)T (Delta r)/(r )`

D

`DeltaT = T (Delta r)/(r )`

Text Solution

Verified by Experts

The correct Answer is:
A

As `T^(2) prop r^(3)` or `T^(2) = Kr^(3)` ..(i)
Differentating it, we have
`2T Delta T = 3Kr^(2) Delta r` ..(ii)
Dividing (ii) by (i), we have
`(2T DeltaT)/(T^(2)) = (3kr^(2)Delta r)/(Kr^(3))` or `DeltaT = (3)/(2)T (Delta r)/(r )`
Promotional Banner

Similar Questions

Explore conceptually related problems

Two small satellites are moving in circular orbits around the earth at a distance R and R + Delta R from the centre of the earth. If their time period of rotation are T and T + Delta T respectively, then

Two satellite A and B are travelling in the same plane and same sense in circular orbit around the earth at an atitude r_(A) and r_(B) from the centre of the earth respectively. If at time t=0 the satellite are aligned as shown in the figure, knowing that the radius of the earth R . Determine the time at which again the satellite will be aligned as they were at t=0

The time period of a satellite in a circular orbit around the earth is T . The kinetic energy of the satellite is proportional to T^(-n) . Then, n is equal to :

A satellite of mass is in a stable circular orbit around the earth at an altitude of about 100 km. If M is the mass of the earth, R its radius and g the acceleration due to gravity, then the time period T of the revolution of the satellite is

A geostationary satellite is orbiting the earth at a height of 6R above the surface oof earth where R is the radius of the earth .The time period of another satellite at a distance of 3.5R from the centre of the earth is ….. hours.

A satellite is revolving round the earth in an orbit of radius r with time period T. If the satellite is revolving round the earth in an orbit of radius r + Deltar(Deltar lt lt r) with time period T + DeltaT(DeltaT lt lt T) then.

The acceleration due to gravity is g at a point distant r from the centre of earth of radius R . If r lt R , then

The time period of a satellite in a circular orbit of radius R is T. The radius of the orbit in which time period is 8 T is