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NEET PHYSICSGRAVITATIONMedium

Question

The additional kinetic energy to be provided to a satellite of mass m revolving around a planet of mass M, to transfer it from a circular orbit of radius R₁ to another of radius R₂ (R₂ > R₁) is

A

GmM(1/R₁² - 1/R₂²)

B

GmM(1/R₁ - 1/R₂)

C

2GmM(1/R₁ - 1/R₂)

D

1/2 GmM(1/R₁ - 1/R₂)

Step-by-Step Solution

The total mechanical energy (EE) of a satellite of mass mm revolving in a circular orbit of radius rr around a planet of mass MM is given by E=GMm2rE = -\frac{GMm}{2r}.

  1. Initial Energy: In the orbit of radius R1R_1, the total energy is E1=GMm2R1E_1 = -\frac{GMm}{2R_1}.
  2. Final Energy: In the orbit of radius R2R_2, the total energy is E2=GMm2R2E_2 = -\frac{GMm}{2R_2}.
  3. Energy Supplied: The additional energy required to transfer the satellite is the difference between the final and initial total energies: ΔE=E2E1=(GMm2R2)(GMm2R1)\Delta E = E_2 - E_1 = \left( -\frac{GMm}{2R_2} \right) - \left( -\frac{GMm}{2R_1} \right) ΔE=GMm2R1GMm2R2=12GMm(1R11R2)\Delta E = \frac{GMm}{2R_1} - \frac{GMm}{2R_2} = \frac{1}{2}GMm \left( \frac{1}{R_1} - \frac{1}{R_2} \right).

Exam Context & Concepts Covered

This question aligns with the NEET PHYSICS syllabus, specifically targeting concepts from GRAVITATION. Mastering this topic is crucial for scoring well in the upcoming medical entrance examinations. Solving conceptually related problems will help you understand the nuances of these concepts and improve your problem-solving speed.

PHYSICSGRAVITATIONadditionalkineticenergyprovidedsatellite

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