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The tangential velocity component ‘V’ of a spacecraft, which is in a circular orbit of radius ‘R’ around a spherical Earth (µ = GM → gravitational parameter of Earth) is given by the following expression.
  • a)
  • b)
  • c)
  • d)
Correct answer is option 'B'. Can you explain this answer?
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The tangential velocity component ‘V’ of a spacecraft, which is in a circular orbit of radius ‘R’ around a spherical Earth (µ = GM → gravitational parameter of Earth) is given by the following expression.a)b)c)d)Correct answer is option 'B'. Can you explain this answer?
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