Calculating Orbital Velocities in a Binary Star System

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In a binary star system with unequal masses, both stars share the same orbital period around their center of mass due to the conservation of momentum. The center of mass remains stationary, and the distance between the two bodies varies as they orbit. To calculate the orbital period, Kepler's third law can be applied, using the average distance between the two stars and the combined mass. The radial acceleration towards the center of mass can be expressed in terms of gravitational force and reduced mass. The derived formula for orbital velocity is accurate, allowing for the determination of velocities based on the gravitational interaction between the bodies.
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I just have a quick question about a binary star system consisting of 2 starts of unequal masses. Is the period of rotation of the 2 masses about their centre of mass equal? Do they both take the same amount of time to complete 1 revolution about the centre of mass?
 
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Yup. The two-body system's center of mass cannot move because there are no external forces, so the line between the two bodies must always pass through the center of mass. Imagine a bar connecting the two bodies; the bar's rotating, expanding, and contracting, but not bending or moving. You can imagine that the two bodies will have the same orbital period.
 
Thanks! :) That makes sense.
So how do I determine this period of orbit of the 2 bodies around the centre of mass? What if, for example, I was considering a planet orbiting around a star. Would I use the general version of Kepler's 3rd law? [ P^2 = (4pi^2*a^3)/ (G(m1 + m2)) ] with a being the average distance between the 2 bodies (since, as you said, this distance will contract and expand as they orbit) (I'll assume circular orbits for simplicity)? Or would I calculate the period in some other way?
 
Have a look at http://en.wikipedia.org/wiki/Reduced_mass"
 
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So , the radial acceleration the 2 bodies would experience towards each other (and therefore toward the centre of mass) is F/mreduced = G*m1*m1/(distance between objects)^2 /mreduced ?
and the radial acceleration (assuming circular orbit) is equal to v^2 / (distance of body to centre of mass), so I can calculate the orbital velocities of the 2 bodies as:

velocity = square root [ (G*m1*m1/(distance between objects)^2 ) * (distance of body to centre of mass)/(mreduced) ]

is this correct?
 
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