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JEE Main 2002 (AIEEE) · Satellite Energy & Weightlessness

Satellite Energy & Weightlessness question from JEE Main 2002 (AIEEE)

Q36JEE Main 2002 · AIEEEMedium

Satellite Energy & Weightlessness

Energy required to move a body of mass mm from an orbit of radius 2R2R to 3R3R is

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Answer: (d)

  1. Total energy in a circular orbit: E=−GMm2rE = -\frac{GMm}{2r}.
  2. E2R=−GMm4RE_{2R} = -\frac{GMm}{4R}, E3R=−GMm6RE_{3R} = -\frac{GMm}{6R}.
  3. Energy required =E3R−E2R=GMm4R−GMm6R=GMm12R= E_{3R} - E_{2R} = \frac{GMm}{4R} - \frac{GMm}{6R} = \frac{GMm}{12R}.
  4. So the answer is GMm12R\frac{GMm}{12R}, which is option (a) with the misprinted R2R^2 read as RR.
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