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Orbital Period Error in a Two-Body System

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Two satellites with masses m1m_1 and m2m_2 orbit a star of mass MM, where m1+m2≪Mm_1 + m_2 \ll M. What is the approximate percentage error in the orbital period that results from assuming the star is stationary?

A

Approximately (m1+m2)2/M2×100%(m_1 + m_2)^2/M^2 \times 100\%

B

Exactly 0%

C

Approximately (m1+m2)/(2M)×100%(m_1 + m_2)/(2M) \times 100\%

D

Approximately (m1+m2)/M×100%\sqrt{(m_1 + m_2)/M} \times 100\%

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