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MHT CET 2023 (10 May, Shift 1) · Satellites - Orbital Velocity & Period

Satellites - Orbital Velocity & Period question from MHT CET 2023 (10 May, Shift 1)

Q28MHT CET 2023 · 10 MAY · SHIFT 1Easy

Satellites - Orbital Velocity & Period

A satellite moves in a stable circular orbit round the earth if (where VH,VcV_H, V_c and VeV_e are the horizontal velocity, critical velocity and escape velocity respectively)

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Answer: (c)

  1. A stable circular orbit needs gravity to supply exactly the centripetal force: mVH2r=GMmr2\frac{mV_H^2}{r} = \frac{GMm}{r^2}.
  2. This gives VH=GMr=VcV_H = \sqrt{\frac{GM}{r}} = V_c, the critical velocity.
  3. If VH<VcV_H < V_c it falls back; if Vc<VH<VeV_c < V_H < V_e the orbit is elliptical; if VH≥VeV_H \ge V_e it escapes.
  4. So the answer is (c) VH=VcV_H = V_c.
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