Gravitational Force of a rocket

AI Thread Summary
To determine how high a rocket must ascend for its weight to be half that on Earth's surface, the gravitational force equation F=GMeMr/r^2 is utilized. By setting up a ratio of the forces at different distances from Earth's center, it is derived that r = Re * sqrt(2), where Re is Earth's radius. The calculated distance from Earth's center must then be adjusted to find the altitude above the surface by subtracting Earth's radius. The correct altitude is found to be approximately 2642.68 km when using the Earth's radius in kilometers. Attention to units and problem specifics is crucial for accurate calculations.
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Homework Statement



How high does a rocket have to go above Earth's surfae before its weight is half what it would be on earth

Homework Equations



F=GMeMr/r^2, however there are too many variables here to use

The Attempt at a Solution



F/2=GMeMr/((sq root 2)r))^2, but I don;t know if this is right or how to use it without numbers
 
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skins266 said:

Homework Statement



How high does a rocket have to go above Earth's surfae before its weight is half what it would be on earth

Homework Equations



F=GMeMr/r^2, however there are too many variables here to use

The Attempt at a Solution



F/2=GMeMr/((sq root 2)r))^2, but I don;t know if this is right or how to use it without numbers

You can deal with this without numbers by using a comparison ratio. The weight of the rocket on the Earth's surface is

W = GMeMr/(Re^2) ,

where Re is the Earth's radius (that's how far the Earth's surface is from its center, which is the r we need in order to apply Newton's gravitation law here.

At the position we're interested in,

(1/2)W = GMeMr/(r^2) ,

where r is the distance from Earth's center that we need to solve for.

What happens when you divide the second equation by the first one? Can you solve the result for r? How do you apply this result to the original question?
 
So I will get 1/Re^2 = 2/r^2 and then r = Re - x where x is the distance to the rocket? But then I get lost on applying it to the question.
 
skins266 said:
So I will get 1/Re^2 = 2/r^2 and then r = Re - x where x is the distance to the rocket? But then I get lost on applying it to the question.

So this tells you that r^2 = 2 · (Re^2) or r = (Re) · sqrt(2). So the rocket must be about 1.414 times the Earth's radius from the Earth's center. How far does that put it above the Earth's surface? That is the altitude the problem asks for.
 
so r = Re(sqrt2) so r = 6.38E6*sqrt2. Which then equals 9022682.528, but when I punch that number into WebAssign it is wrong, so is it not in km, or what
 
skins266 said:
so r = Re(sqrt2) so r = 6.38E6*sqrt2. Which then equals 9022682.528, but when I punch that number into WebAssign it is wrong, so is it not in km, or what

First off, this is the distance from the center of Earth; the problem asks for the distance above Earth's surface, so you have to subtract Re. This will give you

x = Re · [ sqrt(2) - 1 ] .

Secondly, you are using the radius of Earth in meters. You didn't mention it in your original posting, but what units does the problem ask for?
 
Oh yeah, my bad. It is in km and so my radius would be 6.38E3 and then the answer would be 2642.68 ... which is right. Thanks for your help.
 
skins266 said:
Oh yeah, my bad. It is in km and so my radius would be 6.38E3 and then the answer would be 2642.68 ... which is right. Thanks for your help.

Great! Be sure to read these kinds of questions carefully. There is often a homework or exam problem which asks for altitude or gives information in terms of the altitude, rather than the distance to the center of the Earth.
 
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