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Homework Help: Orbit radius of 2 collided satellites

  1. Mar 10, 2010 #1
    1. The problem statement, all variables and given/known data
    Two satellites have mistakenly been put in identical Earth orbits of radius R. Satellite A with mass "m" is orbiting clockwise while satellite B with mass "2m" is orbiting counterclocwise. The two satellites have a head on collision and move as one body after the collision. In terms on the given quantities, what orbit radius would the collided objects have to possess in order to move in a circular path?


    2. Relevant equations/Attempt
    I believe that since the satellites are orbiting at the same radius, the are orbiting at the same speed so
    Va = - Vb

    I can get a quarter of it but I'm not even sure if it's right:

    (3m)(vf)²/(Rf) = ?

    using the collision formula to get vf
    mVa + 2mVb = 3m Vf
    Vf = (Va - 2Vb)/3

    so (3m)[(Va - Vb)/3]/Rf = ?

    I'm very stuck. Help!
     
  2. jcsd
  3. Mar 10, 2010 #2
    Ok, do you know these formulas?
    [tex] K_{s}=\frac{mv^{2}}{2}= \frac{GMm}{2r}[/tex]
     
  4. Mar 10, 2010 #3
    The formulas that I learned were mv^2/r = GMm/r^2
     
  5. Mar 10, 2010 #4
    Well, they are the same thing. Since you think the satellites before they collide have the same speed, use your formula to check it.
     
  6. Mar 10, 2010 #5
    but how? the masses of the satellites cancel out and the radius of orbit is unkown.
     
  7. Mar 10, 2010 #6
    Exactly, the masses cancel out. The speed is not dependent on the mass. Therefore, their speeds are the same.
     
  8. Mar 10, 2010 #7
    Ah ok. But now I have to find the orbit radius but in terms of the quantities given to me in the problem, which were just m & 2m.
     
  9. Mar 10, 2010 #8
    Before you go on with the orbit radius, why don't you plug in the speed since you know they are the same?
     
  10. Mar 10, 2010 #9
    By plugging the speed in do you just mean putting in the variable and manipulating the formula so the radius is isolated? Because the speed itself is unknown even though I know the speeds are the same.
     
  11. Mar 10, 2010 #10
    Sorry, should have been more clear. According to your formula, if we want to find r, we have to first find V. Now we know [tex]v_{a}=v_{b}[/tex], go back to the Conservation of Momentum formula or the collision formula and find V.
     
  12. Mar 10, 2010 #11
    a friend of mine came up with this as the answer. i'm not sure if it's right though.

    Va = - Vb
    so let's just write Vi as V

    V²/R = GM/R²
    V = √(GM/R)

    now using the formula for an inelastic equation to find Vf

    mV - 2mV = 3mVf
    Vf = -V/3

    replace v with √(GM/Ri)
    Vf = -[√(GM/Ri)]/3

    Then move on the the new mass, AB, the combined satellites, with a mass of 3m:

    (3m)Vf²/Rf = (3m) GM/Rf²
    Vf²/Rf = GM/Rf²

    replace Vf with what you found above

    [-(√(GM/Ri))/3]²/Rf = GM/Rf²

    simplify

    [(GM/Ri)/9]/Rf = GM/Rf²

    simplify more

    (GM/9Ri)/Rf = GM/Rf²

    and more

    (GM)(Rf²) = (GM)(9Ri)(Rf)

    cancel out the Gmp's and then divide each side by Rf and so you get to

    Rf = 9Ri
     
  13. Mar 10, 2010 #12
    Looks good for me.
     
  14. Mar 10, 2010 #13
    alright. thank you so much for the help :)
     
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