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Calculate Orbital Angular Momentum

  • Thread starter PhDorBust
  • Start date
  • #1
143
0
Satellite of mass m is moving with velocity v in a circular orbit of radius r about mass M.

Find the orbital angular momentum.

Know

[tex]v = \sqrt{\frac{GM}{r}}[/tex]

Orbital angular momentum of a system is defined as the angular momentum of the center of mass of the system.

Let the origin be at mass M.

[tex]r_{cm} = \frac{m}{M + m} r[/tex]
[tex]v_{cm} = \frac{v}{r} \frac{m}{M + m} r = \frac{vm}{M+m}[/tex]

[tex]l = r_{cm} \times p_{cm} = (M + m) r_{cm} v_{cm} = \frac{m^2 rv}{M+m} = \frac{m^2}{m+M} \sqrt{GMr}[/tex]

Correct answer in text is [tex]m \sqrt{GMr}[/tex]
 

Answers and Replies

  • #2
993
13
I think it is being assumed that M is MUCH bigger than m.
 
  • #3
143
0
Ok thanks, just wanted to be sure.
 

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