Q1 - Derive a formula for ‘Critical Velocity’ for the launching of a
space craft in outer space, using the Newton’s law of gravitation.
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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 is r=R+h.
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Derive a formula for ‘Critical Velocity’ for the launching of a
space craft in outer space, using the Newton’s law of gravitation.
Explanation:
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