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Rocket and orbital problem

  1. Dec 12, 2005 #1
    A rocket is 1.00x10^10m from a moving star moving at a speed of 1.00x10^5 m/s with a total energy of -1.67x10^17 J when it experiences a gravitational force magnitude of 6.67x10^7 N. It turns on its thrusters and its speed as well its distance to the star doubles by the time the thrusters are turned off.

    Find the rocket's mass, the star's mass
    Prove the fist trajectory is elliptical and not circular.
    If a=1.11x10^10 m for the first trajectory, find the period.
    Find the work done by the thrusters in changing trajectories.

    How would I star this problem? It is the first part of physics ( Mech)

    I know r'= 2r and v'=2v
    would I use the orbtial formulas to find the mass or something else. Any hints or anything will be helpful thank you.
  2. jcsd
  3. Dec 13, 2005 #2


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    What's the expression for the total energy of an object in orbit about a central mass? What's the expression for the gravitational force between two objects?

    What's the velocity of an object in a circular orbit at this distance? How does it compare to the rocket's velocity?

    What is Kepler's Third Law?

    What is the energy of the new orbit? Where did this energy come from?
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