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Angular momentum and eccentricities question?

  1. Nov 6, 2007 #1
    An asteroid is on a circular orbit around the sun with an orbital radius of 3AU. It splits into two fragments, which initially move aparty along the direction of the original orbit. One fragment has a speed of 0.65 of the original speed, the other has a speed of 1.35 times the original speed.


    Original Orbital speed is 2pi/(root3) AU per year.

    1) Calculate the angular momentum per unit mass l, of the original asteroid and of each of the two fragments in units of AU^2 per year.

    In these units l can be related to the semi-major axis a i (in AU) and eccentricity e of the orbit by the formula l = 2pi[a(1-e^2)]^0.5

    2) Calculate the eccentricities of the two new orbits.

    3) Calculate the orbital periods of the original astroid and the two fragments (in years).



    I am very stuck on this and any assistance would be really be appretiated.
     
  2. jcsd
  3. Nov 6, 2007 #2

    Astronuc

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    Staff: Mentor

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