When an object is in a circular orbit of radius r, its time period of revolution about the earth is T and orbital velocity is v when its orbit is r+Δr. Find the change in time period ΔT and orbital velocity Δv.
v0=√GMr,v0−Δv=√GMr+Δr
=√GMr(1+Δrr)−1/2orΔv=√GMrΔr2r
=v0Δr2r
=2πrTΔr2r=πΔrT
T=2πr3/2√GM, and T′=2π(r+Δr)3/2√GM
=2πr3/2√GM(1+Δrr)3/2
or T′=T(1+32Δrr)
ΔT=3TΔr2r=32(2πr)vΔrr=3πΔrv