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Exercise · Q15

Q.Define escape velocity and orbital velocity. For a satellite in a circular orbit very close to a planet's surface, derive the relation ve=2 vov_e = \sqrt{2}\,v_o connecting the two.

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Escape velocity (vev_e) is the minimum launch speed needed for an object to reach infinity with, at the limit, zero speed left over -- found from energy conservation, 12mve2=GMm/R\tfrac{1}{2}mv_e^2 = GMm/R, giving ve=2GM/Rv_e = \sqrt{2GM/R}.\n\nOrbital velocity (vov_o) is the (generally much smaller) speed needed for the SAME object to instead move in a stable circular orbit exactly at the surface, found by equating gravity to the required centripetal force, GMm/R2=mvo2/RGMm/R^2 = mv_o^2/R, giving vo=GM/Rv_o = \sqrt{GM/R}.\n\nDividing the two expressions,

vevo=2GM/RGM/R=2\frac{v_e}{v_o} = \frac{\sqrt{2GM/R}}{\sqrt{GM/R}} = \sqrt{2} …

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