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Orbit around an asteroid.

  1. Mar 27, 2012 #1
    The problem statement, all variables and given/known data
    The problem deals with a sports player being able to hit a golf ball at a speed of 92 m/s. The first part says to find the size of an asteroid that would have that speed as an escape velocity.

    The second part says that if he hits the ball at 80 m/s, what will the eccentricity be as well as the semi major axis a.
    So I did the following..

    [tex]v_{esc}=\sqrt{\frac{2GM}{R}}[/tex]
    and
    [tex]M=\frac{4}{3} \pi R^3 \rho[/tex]

    Where ρ=2.5g/cm
    Converted rho and plugged everything in and got a value of R to be 77144.5m.

    So since the player hits the ball at less than the escape velocity it goes into an elliptic orbit. The position of the ball when it first gets hit is right in the position of closest approach.(Right at the perihelion.)

    So that means, from geometry [itex]R=a(1-e)[/itex].

    The tangential velocity of the orbit is..
    [tex]v=\sqrt{\frac{M}{P}}(1+ecos( \theta))[/tex]
    Plugging in for P from geometry and taking theta to be zero...

    [tex]v=\sqrt{\frac{m(1+e)}{a(1-e)}}[/tex]

    This gives me two equations with two unknowns. When I solve, I get a negative eccentricity! I do not know where I am going wrong :\
     
  2. jcsd
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