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Question: A satellite is launched into a circular orbit of radius R around the earth. A second satellite is la...

A satellite is launched into a circular orbit of radius R around the earth. A second satellite is launched into an orbit of radius (1.01)R. The period of the second satellite is large than that of the first one by approximately

A

0.5%

B

1.0%

C

1.5%

D

3.0%

Answer

1.5%

Explanation

Solution

Kepler's Third Law states that T2R3T^2 \propto R^3, which means TR3/2T \propto R^{3/2}. For the two satellites, we have: T2T1=(R2R1)3/2\frac{T_2}{T_1} = \left(\frac{R_2}{R_1}\right)^{3/2} Given R1=RR_1 = R and R2=1.01RR_2 = 1.01R. T2T1=(1.01RR)3/2=(1.01)3/2\frac{T_2}{T_1} = \left(\frac{1.01R}{R}\right)^{3/2} = (1.01)^{3/2} Using the binomial approximation (1+x)n1+nx(1+x)^n \approx 1 + nx for small xx: (1.01)3/21+32×0.01=1+1.5×0.01=1+0.015=1.015(1.01)^{3/2} \approx 1 + \frac{3}{2} \times 0.01 = 1 + 1.5 \times 0.01 = 1 + 0.015 = 1.015 The percentage increase is: (T2T11)×100%(1.0151)×100%=0.015×100%=1.5%\left(\frac{T_2}{T_1} - 1\right) \times 100\% \approx (1.015 - 1) \times 100\% = 0.015 \times 100\% = 1.5\%