How to find the L1 (First Langrangian Point) between the Earth and the Moon?

In summary, the point at which the force of gravity on an object from the moon is equal and opposite to the force of gravity on the earth is when the distance between the Earth and moon is 3.84x10^5 km.
  • #1
ootz0rz
3
0
Hi everyone :) I'm new to the forums, need some help with a homework question I just can't seem to be able to get...

The question as described in my book is as follows:

The mass of the moon is 7.35x10^22 kg. At some point between Earth and the Moon, the force of Earth's gravitational attraction on an object is canceled by the Moon's force of gravitational attraction. If the distance between the Earth and the moon (center to center) is 3.84x10^5 km, calculate where this will occur, relative to the Earth.

Earlier in the book, I am given the mass of the Earth as 5.98x10^24 kg and I am supposed to use that.

What I've got so far (not sure if any of this is correct at all... :frown:):

[tex]F_g = \frac{GMm}{r^2}[/tex]

Where...
[tex]G = 6.67x10^{-11} \frac{Nm^2}{kg^2}[/tex]
M = The larger mass
m = the smaller mass
r = radius

Problem is, we are not given an object being at the L1 point (which I will refer to as X), so it can't be used for that. It can be used however to find the force of gravity from Earth that is acting on the moon at that radius. But anyways, I needed a way to remove the m variable, so I replaced Fg with an equivalent equation:

[tex]\frac{mv^2}{r} = \frac{GMm}{r^2}[/tex]

m and one r cancels out and we get

[tex]\frac{GM}{r} = v^2[/tex]

this however introduces a new unknown variable into, v - being the velocity
However, v can be expressed as

[tex]v = \frac{2 \pi r}{T}[/tex]
therefore [tex]v^2 \Rightarrow v^2 = \frac{4 \pi^2 r^2}{T^2}[/tex]

T is the period it takes to complete one revolution, yet another fun unknown...

at this point we have
[tex]\frac{GM}{r} = \frac{4 \pi^2 r^2}{T^2}[/tex]

Then if we bring r^2 to the left side...

[tex]\frac{GM}{r^3} = \frac{4 \pi^2}{T^2}[/tex]

I could further juggle the equation so it would solve for r...however...I'm not sure what to do with the T variable

That's about as far as I was able to get :/ Any help would be greatly appreciated.
Thank you :)
 
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  • #2
ootz0rz said:
The mass of the moon is 7.35x10^22 kg. At some point between Earth and the Moon, the force of Earth's gravitational attraction on an object is canceled by the Moon's force of gravitational attraction. If the distance between the Earth and the moon (center to center) is 3.84x10^5 km, calculate where this will occur, relative to the Earth.

Earlier in the book, I am given the mass of the Earth as 5.98x10^24 kg and I am supposed to use that...
Welcome to PF!

You just have to find the point at which the force of gravity on an object from the moon is equal and opposite to the force of gravity on the earth. Take the distance between the Earth and moon as d. So [itex]r_e = d - r_m[/itex]

AM
 
  • #3
I just tried doing this another way, as follows (and was able to successfully solve for "r" using this method). Can someone please look it over? :)

We assume an object is at the L1 point (the point where the gravitational fields of the two objects cancels out). We will call this object X

r is the radius between the Earth and the Moon
We will call [tex]r_1[/tex] the point from the center of the Earth to x and [tex]r_2[/tex] the point from x to the center of the moon
Therefore
(1)[tex]r = r_1 + r_2[/tex]

Using this assumption of the object X we get..

[tex]F_g = \frac{G m_1 x}{r^2_1}[/tex] where [tex]m_1[/tex] is the mass of the earth, and x is the mass of object X
[tex]F_g = \frac{G m_2 x}{r^2_2}[/tex] where [tex]m_2[/tex] is the mass of the moon, and x is the mass of object X

Since we know that, at the point where the object X is situated, the gravitiational pull from both the Earth and the Moon will be equal, we can equate the above two equations getting the following:
(2)[tex]\frac{G m_1 x}{r_1^2} = \frac{G m_2 x}{r_2^2}[/tex]

Now, we obtain a ratio between [tex]m_1[/tex] and [tex]m_2[/tex] so we can express [tex]m_1[/tex] in terms of [tex]m_2[/tex]

[tex]\frac{m_1}{m_2} = 81[/tex] (Note: I rounded to 81 just to make typing it up here easier...)
Therefore, [tex]m_1 = 81m_2[/tex]

Now, going back to equation (2), G and x will cancel out and we replace [tex]r_1[/tex] with [tex]r-r_2[/tex] (from equation (1)) leaving us with:
[tex]\frac{81m_2}{(r-r_2)^2} = \frac{m_2}{r_2^2}[/tex]

[tex]m_2[/tex] will cancel out:
[tex]\frac{81}{(r - r_2)^2} = \frac{1}{r_2^2}[/tex]

[tex]81 = \frac{(r - r_2)^2}{r_2^2}[/tex]

i take the square root of both sides, and put the denominator on the left side
[tex]9 r_2 = r - r_2[/tex]

[tex]10 r_2 = r[/tex]

[tex]r_2 = r / 10[/tex]

[tex]r_2 = 3.84*10^{4}[/tex]

Since [tex]r_1 = r - r_2[/tex]

[tex]r_1 = 3.84*10^{5} - 3.84*10^{4}[/tex]

[tex]r_1 = 3.456*10^{5}[/tex]

my actual answer is a little bit different since i rounded differently for posting on here...but i'd like to know if the method is correct?
Thanks again in advance.
 
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  • #4
Andrew Mason said:
Welcome to PF!
Thank you :)
Andrew Mason said:
You just have to find the point at which the force of gravity on an object from the moon is equal and opposite to the force of gravity on the earth. Take the distance between the Earth and moon as d. So [itex]r_e = d - r_m[/itex]
I thought of doing something similar, and my results are posted above. I was writing the post up as you replied :)
 

FAQ: How to find the L1 (First Langrangian Point) between the Earth and the Moon?

How far is the L1 point from the Earth and Moon?

The distance to the L1 point between the Earth and Moon varies depending on the position of the Moon in its orbit, but on average it is approximately 326,000 km or 202,000 miles from the Earth and 56,000 km or 35,000 miles from the Moon.

How is the L1 point calculated?

The L1 point is calculated using a mathematical model that takes into account the gravitational forces between the Earth and Moon, as well as their orbital velocities and positions. This model is often referred to as the three-body problem.

Why is the L1 point important?

The L1 point is important because it is a point of gravitational equilibrium between the Earth and Moon. Objects placed at this point will experience equal gravitational pull from both bodies, making it an ideal location for spacecraft and satellites to orbit.

Can the L1 point be reached by spacecraft?

Yes, the L1 point can be reached by spacecraft, although it requires precise calculations and maneuvers to maintain a stable orbit at this point. Several missions, such as the Solar and Heliospheric Observatory (SOHO) and the Deep Space Climate Observatory (DSCOVR), have successfully orbited the L1 point.

How is the L1 point used in space exploration?

The L1 point is used in space exploration for a variety of purposes, including monitoring solar activity, studying the Earth's climate, and testing new technologies for future missions. It also serves as a gateway to other regions of space, such as the Lagrange points between the Earth and Sun.

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