Escape Velocity of the Milky Way

Click For Summary
SUMMARY

The discussion focuses on deriving the escape velocity from the Milky Way galaxy, specifically proving that the escape velocity from any radius r PREREQUISITES

  • Understanding of gravitational potential energy and kinetic energy concepts
  • Familiarity with circular motion and orbital velocity equations
  • Knowledge of logarithmic functions and their properties
  • Basic calculus skills for evaluating integrals
NEXT STEPS
  • Study the derivation of gravitational potential energy in astrophysical contexts
  • Learn about the implications of flat rotation curves in galaxies
  • Explore the concept of mass density profiles in astrophysics
  • Investigate the role of escape velocity in celestial mechanics
USEFUL FOR

Astronomy students, astrophysicists, and anyone interested in understanding the dynamics of galaxies and escape velocity calculations.

J.Welder12
Messages
5
Reaction score
0

Homework Statement



In the Solar neighborhood, the Milky Way has a flat rotation curve, with V(r)= Vc where Vc is a constant, implying a mass desnity profile ρ(r) ~ r^-2

Assume there is a cutoff radius R beyond where the mass density is zero. Prove that the velocity of escape from the galaxy from any radius r<R is:

Ve^2= 2Vc^2(1+ln R/r)


Homework Equations



Integral needs to be done in two parts


The Attempt at a Solution



The 1/2 mv^2 provides the energy needed to do the work of moving the mass m against the force of gravity from a radius r to infinity.
I believe the integral needs to be evaluated at both r and R, however, I do not know what equation to integrate because integrating 1/2 mv^2 doesn't seem like it will yield the above equation.
 
Physics news on Phys.org
A body orbiting a central mass M in a circular orbit at radial distance r has orbital velocity
[tex]V_c = \sqrt{\frac{G M}{r}}[/tex]
For the galaxy then, if the velocity profile is flat then Vc is a constant from r to R, and you can obtain an effective mass w.r.t. radius by solving the above for M and calling it M(r).

With M(r) you are in a position to determine the change in PE for an object taken from r to R.

Next, consider that at distance R the circular orbital velocity is still Vc, and that since all the effective mass is "below" R, it will behave as a point mass at the center and the escape velocity there must be [itex]\sqrt{2}V_c[/itex]. That gives you the required KE at radius R.

For escape, the starting KE will be the required final KE plus the loss in PE. Find the escape velocity from the starting KE.
 

Similar threads

  • · Replies 7 ·
Replies
7
Views
1K
  • · Replies 15 ·
Replies
15
Views
2K
  • · Replies 7 ·
Replies
7
Views
2K
  • · Replies 5 ·
Replies
5
Views
3K
Replies
6
Views
2K
  • · Replies 39 ·
2
Replies
39
Views
4K
Replies
335
Views
17K
  • · Replies 5 ·
Replies
5
Views
2K
  • · Replies 5 ·
Replies
5
Views
2K