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Gravitational question

  1. Jul 22, 2016 #1
    1. The problem statement, all variables and given/known data
    The problem is attached

    2. Relevant equations
    Energy, gravitational formulas

    3. The attempt at a solution
    For part b, the answer is 2km s^-1
    If it can escape, KE-PE(energy travelled from infinity to R)=0
    KE = PE
    mv^2 /2 = GMm/R
    v^2/2=GM/R..(1)

    I tried to find GM by using the information provided
    mv^2 /R = GMm /R^2
    v^2/2 = GM/2R....(2)

    which combining (1) and (2) I get v^2/2 = v^2 which is impossible.
    Please tell me whats wrong and the correct method to solve the question
     

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  3. Jul 22, 2016 #2

    ehild

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    Homework Helper
    Gold Member

    It is not true if the spacecraft has kinetic energy at infinity .

    How do you intend to determine the mass of the planet? You have to define what R and v are. It seems you try to use the formula valid for a circular orbit, but this spacecraft is leaving the planet instead of orbiting around it.
     
  4. Jul 22, 2016 #3
    then what formula should I use?
     
  5. Jul 22, 2016 #4

    cnh1995

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    Homework Helper

    I'm not sure this will work but here's what I think..
    You can first plot the graph of v vs r on a graph paper. Draw a smooth curve. At (r=1, v=6.635), draw a tangent to that curve whose slope will be dv/dr.
    Now,
    deceleration=dv/dt=(dv/dr)*(dr/dt)=v*dv/dr..
    You can know v, r and dv/dr at every point on the graph.
    You can equate the deceleration obtained from graph to GM/r2 and get M.
     
    Last edited: Jul 22, 2016
  6. Jul 22, 2016 #5
    Hello,

    I have searched a little bit about the topic of escape velocity and I figured the solution
    I will give you an example
    If you have a road that is 8 meters tall and you know that a section from the end to a point in that road is 5 meters tall. How far is the point from the starting point of the road? You just have to do subtraction.

    Okay so If G M m /r gives you potential from a point to infinity and you take another (r value) above the first one you took and substract the two what do you get?

    Now use energy conservation using velocities and find out GM.

    Once you find that out we can continue.
     
  7. Jul 22, 2016 #6

    gneill

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    Staff: Mentor

    Look at energy conservation. The total specific mechanical energy (that is, the energy per unit mass of the object in orbit) is the sum of the specific kinetic and potential energy at any instant. For a body in a free-fall trajectory of any kind (such as this spacecraft is) this value is a constant.

    In particular: ##\xi = \frac{v^2}{2} - \frac{GM}{r}## is a constant over the whole trajectory.

    You should be able to use this along with the given data to solve for both ##\xi## and GM.
     
  8. Jul 22, 2016 #7
    Thanks, I can find the answer of part a by using both methods.
    The answer of part c is 6 x 10^23 kg, but when I use U^2/2 - GM/R =V^2/2, I found out 3 x 10^23 kg
     
  9. Jul 22, 2016 #8

    gneill

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    Staff: Mentor

    Your answer (3.0 x 10^23 kg) looks good to me. Perhaps there's an error in the given answer key.
     
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