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Problems in escape velocity​

User Begemoth
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Answer:

when u say problem do u mean question.

if u do here are some question:

  1. calculate the velocity of an artificial satellite orbiting the earth in a circular orbit at an altitude of 150 miles above the earth surface.

  2. solution \\ given \: r = (3960 + 150) * 5280 \\ r = 21 \: 700 \: 800ft \\ \\ v = sqrt( (gm)/(r) ) \\ v = sqrt( (1.408 * 10^( - 16) )/(21 \: 700 \: 800) \\ v = 25 \: 470 (ft)/(s)
User RomeNYRR
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