1.

i)Derive an expression for critical velocityof satellite.

Answer»

Consider a satellite of mass m revolving round the Earth at a, height 'h' above the surface of the Earth.

Let M be the mass and R be the radius of the Earth.

The satellite is moving with velocity V and the radius of the circular orbit isr=R+hr=R+h. Centripetal force = Gravitational force

∴Mv2cr=GMmr2∴Mvc2r=GMmr2

∴v2c=GMr∴vc2=GMr

∴vc=√GMR+h∴vc=GMR+h

This is the expression for critical velocity of a satellite moving in a circular orbit around the Earth,

We know that,

gh=GM(R+h)2gh=GM(R+h)2

GM=gh(R+h)2GM=gh(R+h)2

Substituting in equation (1), we get

∴vc=√gh(R+h)2R+h∴vc=gh(R+h)2R+h

∴vc=√gh(R+h)∴vc=gh(R+h)

whereghghis the acceleration due to gravity at a height above the surface of the Earth.



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