Can You Solve the Keplerian Two-Body Problem in Physics?

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SUMMARY

The discussion focuses on solving the Keplerian two-body problem, specifically deriving the total energy equation for a particle in an attractive potential defined by V(r) = -GM/r. The derived energy equation is E = (1/2)(dr/dt)^2 + (1/2)(J^2/r^2) - (GM)/r, where J represents the angular momentum per unit mass. Additionally, the conversation explores the conditions under which a particle can reach r = 0 or r = infinity based on its energy state, emphasizing the significance of energy values E < 0 and E > 0 in determining the particle's trajectory.

PREREQUISITES
  • Understanding of Keplerian potential and gravitational forces
  • Familiarity with angular momentum concepts in physics
  • Knowledge of kinetic and potential energy relationships
  • Basic proficiency in calculus for analyzing motion equations
NEXT STEPS
  • Study the derivation of energy equations in gravitational systems
  • Learn about the implications of angular momentum in orbital mechanics
  • Explore the graphical representation of energy states in orbital dynamics
  • Investigate the conditions for escape velocity in gravitational fields
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Students and professionals in physics, particularly those focusing on orbital mechanics, astrophysics, and gravitational dynamics, will benefit from this discussion.

GaleForce
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Alright I'm really stuck on this question. I was wondering if anyone could help:

(a) Show that the total energy (per unit mass) of a particle orbiting in an attractive Keplerian potential V(r) = -GM/r is

E = (1/2)(dr/dt)^2 + (1/2)(J^2/r^2)-(GM)/r

where J = |r x v| is the particle's angular momentum (per unit mass).

(b) If the particle in part (a) has J =\= 0 and finite energy, is it possible for the particle to reach r = 0? Can the particle reach r = infinity if E < 0? If E > 0? If may help to sketch a graph of 1/2(dr/dt)^2 as a function of r for both E < 0 and E > 0. I have no idea how to even approach the problem. It really doesn't fit in with the rest of the work we've been doing so I'm completely clueless. Thanks if anyone can help out.
 
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a) dr/dt is only the radial part of the velocity vector [itex]\vec v[/itex]. Since -GM/r is the potential energy (per unit mass), (1/2)(J^2/r^2) must be the contribution of the tangential component of the velocity to the kinetic energy p.u.m. [itex]\frac{1}{2}\vec v\cdot \vec v[/itex].

So the first thing to do is to separate the vector [itex]\vec r,\vec v[/itex] into their radial and tangential components.

b) What are your thoughts on this one? What can you say if r=0?
 

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