Question:

The ratio of escape velocity and orbital velocity of satellite revolving near the earth:

Updated On: Jul 28, 2022
  • $ \sqrt{2} $
  • 2
  • 3
  • 4
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The Correct Option is A

Solution and Explanation

$v_{e}=\sqrt{2} v_{o} \,\,$ $ v_{e}=$ escape velocity $ \frac{v_{e}}{v_{o}}=\sqrt{2} \,\,$ $ v_{0}=$ orbital velocity
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Concepts Used:

Gravitation

In mechanics, the universal force of attraction acting between all matter is known as Gravity, also called gravitation, . It is the weakest known force in nature.

Newton’s Law of Gravitation

According to Newton’s law of gravitation, “Every particle in the universe attracts every other particle with a force whose magnitude is,

  • F ∝ (M1M2) . . . . (1)
  • (F ∝ 1/r2) . . . . (2)

On combining equations (1) and (2) we get,

F ∝ M1M2/r2

F = G × [M1M2]/r2 . . . . (7)

Or, f(r) = GM1M2/r2

The dimension formula of G is [M-1L3T-2].