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Orbital Period of Binary Star System Relative to Earth

Two stellar bodies with masses 3MS3M_S and 6MS6M_S are separated by a distance 9R9R. Here, RR represents the average distance between the centers of Earth and the Sun, while MSM_S denotes the mass of the Sun. If these two stars rotate around their mutual center of mass along circular paths with an orbital period of nTnT (where TT signifies the orbital period of Earth around the Sun), find the value of nn.

Official Numerical Answer9

Step-by-Step Solution

To find the value of nn, we analyze both the Earth-Sun system and the binary star system using Newton's law of gravitation and circular motion.

1. Earth-Sun System

Assuming the mass of the Earth is negligible compared to the mass of the Sun (MSM_S), the centripetal force required for Earth to maintain a circular orbit of radius RR is provided by the gravitational force between Earth and the Sun: GMSMER2=MEωE2R=ME(2πT)2R\frac{G M_S M_E}{R^2} = M_E \omega_E^2 R = M_E \left(\frac{2\pi}{T}\right)^2 R

Solving for the orbital period TT of the Earth around the Sun: T=2πR3GMST = 2\pi \sqrt{\frac{R^3}{G M_S}}


2. Binary Star System

Let the two stellar bodies have masses m1=3MSm_1 = 3M_S and m2=6MSm_2 = 6M_S, and let their separation distance be d=9Rd = 9R.

The total mass of the binary system is: Mtotal=m1+m2=3MS+6MS=9MSM_{\text{total}} = m_1 + m_2 = 3M_S + 6M_S = 9M_S

The center of mass of the two stars serves as the center of their circular orbits. The distance of star m1m_1 from the center of mass is given by: r1=(m2m1+m2)dr_1 = \left(\frac{m_2}{m_1 + m_2}\right) d

The gravitational force of attraction between the two stars provides the necessary centripetal force for m1m_1 to revolve in a circular path of radius r1r_1 with angular speed ω\omega: Gm1m2d2=m1ω2r1\frac{G m_1 m_2}{d^2} = m_1 \omega^2 r_1

Substituting r1=m2dm1+m2r_1 = \frac{m_2 d}{m_1 + m_2}: Gm1m2d2=m1ω2(m2dm1+m2)\frac{G m_1 m_2}{d^2} = m_1 \omega^2 \left(\frac{m_2 d}{m_1 + m_2}\right)

Canceling m1m2m_1 m_2 from both sides, we get: ω2=G(m1+m2)d3\omega^2 = \frac{G(m_1 + m_2)}{d^3}

The orbital period TbinaryT_{\text{binary}} of the binary system is: Tbinary=2πω=2πd3G(m1+m2)T_{\text{binary}} = \frac{2\pi}{\omega} = 2\pi \sqrt{\frac{d^3}{G(m_1 + m_2)}}


3. Relation Between TbinaryT_{\text{binary}} and TT

Substitute d=9Rd = 9R and m1+m2=9MSm_1 + m_2 = 9M_S into the formula for TbinaryT_{\text{binary}}: Tbinary=2π(9R)3G(9MS)=2π729R39GMS=2π81⋅R3GMS=9⋅(2πR3GMS)T_{\text{binary}} = 2\pi \sqrt{\frac{(9R)^3}{G(9M_S)}} = 2\pi \sqrt{\frac{729 R^3}{9 G M_S}} = 2\pi \sqrt{81 \cdot \frac{R^3}{G M_S}} = 9 \cdot \left(2\pi \sqrt{\frac{R^3}{G M_S}}\right)

Since T=2πR3GMST = 2\pi \sqrt{\frac{R^3}{G M_S}}, we have: Tbinary=9TT_{\text{binary}} = 9T

Given that the orbital period is nTnT, comparing Tbinary=9TT_{\text{binary}} = 9T with nTnT gives: n=9n = 9