Launched Rocket (Energy problem)

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A rocket launched vertically from Earth's surface at a velocity of 3.4 km/s can be analyzed using energy conservation principles, equating kinetic energy and gravitational potential energy. The equation 1/2mv² = -GMm/r helps determine the maximum height reached, with the negative sign indicating gravitational potential energy's reference point at infinity. The negative values in the gravitational potential energy equation cancel out when calculating the difference between two radii, making them manageable in the context of the problem. To find the rocket's distance from Earth's surface, the Earth's radius should be subtracted from the calculated distance from Earth's center. This approach clarifies the relationship between kinetic and potential energy in the context of the rocket's launch.
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Homework Statement



15. (4) A rocket is launched vertically from Earth's surface with a velocity of 3.4 km/s. How high does it go from Earth's centre?


Homework Equations



Ek = 1/2mv^2
Eg = -GMm/r

The Attempt at a Solution



1/2mv^2 = -GMm/r
1/2(3400)^2 = 6.673*10^-11*5.978*10^24/r
r = -6.9*10^11 m

How do i get rid of the negative?

Thanks for your time
 
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Remember Eg is the energy needed to move the mass to infinity, so the change in Eg is the change in ke.

The change in PE is positive, and the change in KE is 0.5mv2

So you will have 0.5mv2= GMm/r
 
rock.freak667 said:
Remember Eg is the energy needed to move the mass to infinity, so the change in Eg is the change in ke.

The change in PE is positive, and the change in KE is 0.5mv2

So you will have 0.5mv2= GMm/r

Thanks! so I just ignore the negative sign?
 
I Like Pi said:
Thanks! so I just ignore the negative sign?

Well you don't really ignore is as it cancels out. But in essence, yes you can ignore it.
 
rock.freak667 said:
Well you don't really ignore is as it cancels out. But in essence, yes you can ignore it.

How does it cancel out?

thanks for your help!
 
I think it is a little more complicated. Notice that -GMm/r is zero at r = infinity (as someone already wrote) and that it gets larger as r increases. So, quite a large negative value at the surface. A smaller negative value a few km up. It really only has meaning when you take the difference for two different radii. You'll need something like this:
0.5mv² = -GMm/r - (-GMm/r)
where one of the r's is the Earth's radius and the other the radius you are looking for.
 
Delphi51 said:
I think it is a little more complicated. Notice that -GMm/r is zero at r = infinity (as someone already wrote) and that it gets larger as r increases. So, quite a large negative value at the surface. A smaller negative value a few km up. It really only has meaning when you take the difference for two different radii. You'll need something like this:
0.5mv² = -GMm/r - (-GMm/r)
where one of the r's is the Earth's radius and the other the radius you are looking for.

Thank you :smile:! Makes sense. Now if i want to find the rocket's distance from EARTH'S SURFACE, would I just subtract the radius of the Earth from the answer i get above?

Thanks again!
 
Last edited:
Right on the subtraction.
Most welcome and good luck on the next one.
 
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