Question #39911

Obtain an expression for the time period of a satelite orbiting the earth. A space shuttle is in a circular orbit at a height of 250km from the earth's surface, where the acceleration due to earth's gravity is 0.93g. calculate the period of its orbit. Take g=9.8m/s-2 and the radius of the earth R=6370000m.

Expert's answer

Answer on Question#39911, Physics, Mechanics

Question:

Obtain an expression for the time period of a satellite orbiting the earth. A space shuttle is in a circular orbit at a height of 250km from the earth's surface, where the acceleration due to earth's gravity is 0.93g. calculate the period of its orbit. Take g=9.8m/s-2 and the radius of the earth R=6370000m.

Answer:

Newton's second law of motion:


mv2R+h=0.93mg\frac{m v^{2}}{R + h} = 0.93mg


where v2R+h\frac{v^{2}}{R + h} is centripetal acceleration, 0.93mg0.93mg is gravitational force.

Therefore, speed of motion equals:


v=0.93g(R+h)v = \sqrt{0.93g (R + h)}


Period equals:


T=2π(R+h)v=2πR+h0.93g5400sT = \frac{2\pi (R + h)}{v} = 2\pi \sqrt{\frac{R + h}{0.93g}} \cong 5400\,s


Answer: 5400 s

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