What is the Period of Revolution for a Triple Star System?

  • Thread starter Thread starter chaose
  • Start date Start date
  • Tags Tags
    Gravitation Weird
Click For Summary
SUMMARY

The period of revolution for a triple star system, consisting of two stars each with mass m orbiting a central star of mass M, is derived using gravitational principles. The correct expression for the period T is T² = (16π² * r³) / (G * (4M + m)), where G is the universal gravitational constant and r is the radius of the orbit. The gravitational forces from the two orbiting stars do not cancel each other out; instead, they contribute to the net centripetal force acting on the system.

PREREQUISITES
  • Understanding of Newton's Law of Universal Gravitation
  • Familiarity with Kepler's Laws of Planetary Motion
  • Basic knowledge of centripetal force concepts
  • Mathematical proficiency in algebra and calculus
NEXT STEPS
  • Study the derivation of Kepler's Third Law in detail
  • Explore the dynamics of multi-body gravitational systems
  • Learn about the implications of gravitational interactions in astrophysics
  • Investigate the mathematical modeling of orbital mechanics
USEFUL FOR

Astronomy students, astrophysicists, and anyone interested in the dynamics of multi-star systems will benefit from this discussion.

chaose
Messages
10
Reaction score
0
A triple star system consists of two stars each of mass m revoling in the same circular orbit of radius r around a central star of mass M. The two orbiting stars are always at opposite ends of a diameter of the orbit. Derive an expression for the period of the revolution of the stars.

I don't understand this problem that well. Any hints?

I thought that if the two stars are at opposite ends of the orbit, won't the gravitational forces from one cancel out the forces from the other star?
Then won't the period just be Kepler's Third law?

T^2 = (r^3)*(4pi^2)/(GM), G = universal gravitational constant, M = mass of central star, T = period of revolution, r = radius of the orbit, pi = 3.14159...
 
Physics news on Phys.org
The force on each orbiting star is the sum of the forces from the other two stars. The net force on the central star will be zero, so it is stationary at the center of the motion of the other two stars. You can do this as a basic centripetal force problem if you get the forces right.
 
thanks, I believe I got it now.

My end result was
T^2 = (16pi^2 * r^3)/(G*(4M+m))
 

Similar threads

  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 12 ·
Replies
12
Views
4K
  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 1 ·
Replies
1
Views
5K
  • · Replies 7 ·
Replies
7
Views
3K
  • · Replies 13 ·
Replies
13
Views
8K
  • · Replies 8 ·
Replies
8
Views
3K
  • · Replies 3 ·
Replies
3
Views
1K
Replies
1
Views
2K
  • · Replies 4 ·
Replies
4
Views
2K