# How High the Moon

## A paper for G4G9

### by Colin Wright

It's surprising, sometimes, how a large collection of apparently unconnected facts can sometimes be woven into whole cloth. Some months ago as I was drifting off to sleep I thought I saw how a bunch of stuff I knew all tied up together into a neat bundle.

Then I woke up, but surprisingly, it looked like it all still worked! Even more surprisingly, when I investigated further, it did, and here are the results.

As implausible as it may seem, we're going to compute the distance to the Moon using a few well-known facts, a few simple observations, a pendulum, and a stopwatch. Pretty much everything here was known to Isaac Newton in the late 1600's, and it's even been suggested that he performed pretty much exactly these calculations.
 Maybe, maybe not. Let's just see what we can do with some really elementary reasoning. We'll warm up with a well-known (in some circles!) question: How far is the horizon? We'll pretend things are simple. We'll pretend the Earth is a sphere, and suppose we're at the top of a tall mountain, say, 5 metres high. (Yes - I know that's not very tall really, but bear with me ...) We can create a right-angled triangle with one corner at the centre of the Earth, one corner at our position, and one where our line-of-sight tangents the Earth's surface. http://blogs.discovermagazine.com/badastronomy/files/2008/08/horizon_diagram.jpg

Our good friend Pythagoras now steps up and says that we have that $R^2+H^2=(R+5)^2,$ which can be expanded and simplified and we get $H^2\approx{}10\times{}R.$

• By the way, I'll keep the equations in the main text fairly simple and expand on them in the boxes on the right side of the page. Feel free to ignore them if you just want the main ideas, or if you want the challenge of working out the details yourself.
 $R^2+H^2=(R+5)^2$ $R^2+H^2=R^2+2\times{}5\times{}R+5^2$ $R^2+H^2=R^2+10\times{}R+25$ so $H^2=10\times{}R+25$ $H^2\approx{}10\times{}R$

Now, the original definition of the metre was "One ten-millionth of the distance from the North Pole to the Equator through Paris," which means the circumference of the Earth is 40 million metres, so the radius is roughly 6.4 million metres. Substituting this we get

$H^2\approx{}64\times{}10^6,$ and so $H\approx\sqrt{64\times{}10^6}=8000m$

So from a height of 5 metres, the distance to the horizon is about 8000 metres, or 8km.

 Now let's turn it around. Suppose we're at sea level and 8000m from the top of a 5m high mountain. If we fire a projectile line-of-sight at the peak, ignore air resistance, and it gets there in 1 second (unlikely, I know). In one second it will fall about 5m, because acceleration due to gravity is about $10m/s^2,$ so by the time it gets there, it will still be at sea-level. In other words, it will be grazing the Earth's (perfectly spherical) surface. It's in orbit. So we've just shown that subject to all our approximations, orbital velocity at grazing altitude is 8 km/s. Quite astonishing how our good friend Pythagoras is, in some sense, "Rocket Science." Diagram of cannon firing at 8km/s

So now let's be a little more general. Instead of being exactly 5m high, let's pick an acceleration a and an amount of time t and suppose we are $at^2/2$ high.

Our Pythagorean triangle equation is now

• $H^2+R^2=(R+at^2/2)^2$
We simplify, divide through by $t^2,$ throw away the irrelevant small part, and then remember that distance over time is velocity. That means we get

• $v^2=aR$
 That seems arbitrary, I know, but distance fallen in time t under acceleration a is given by $d=at^2/2$ so we're at a height such that something will fall that distance in time t.

 $H^2+R^2=(R+at^2/2)^2$ $H^2+R^2=R^2+2\times{}R\times{}at^2/2+(at^2/2)^2)$ $H^2=2\times{}R\times{}at^2/2$ (ignoring the last term) $H^2=R\times{}a\times{}t^2$ $(H/t)^2=R\times{}a$ $v^2=R\times{}a$

or equivalently,

• $a=v^2/R$
Suddenly we have the formula for acceleration in a circle.

Which is nice.

What does this have to do with the Moon?

 You may ask why something moving in a circle is accelerating? Well, its speed may not be changing, but its direction is. If left alone its direction wouldn't change, so something must be pushing on it, changing its direction. That comes out in the wash as meaning it's accelerating. I've also been a little cavalier about ignoring small quantities and so forth. In truth there are some details about limits and such like, and that's where the serious calculus should be done.

If we suppose the Moon to be moving in a circular orbit, and supposing the radius of that orbit to be M, we can now say that its acceleration in orbit is $v^2/M.$ So if only we knew how far away it was, and its velocity, we would know its acceleration.

But if we know its distance then we do know its velocity, because we know it takes 29.53 days from full moon to full moon. Correcting for sidereal time, that means it takes 27.32 days to make a complete circuit of the Earth. Call that time P. Therefore the Moon's velocity in orbit is $(2\pi{}M)/P.$

 When the Moon goes around the Earth, the Earth is also going around the Sun. In the 365.25 days it takes for a year the Moon goes around the Earth - apparently - some 365.25/29.53 times. However ... The orbit of the Earth itself adds another complete rotation. From the point of view of the stars the Moon hasn't gone around 12.37 times, it's gone around 13.37 times, and that means that each orbit, from the point of view of the stars, takes 365.25/13.37 days, or 27.32 days. Thus the sidereal orbital period of the Moon is 27.32 days.
So we have the formula for acceleration in a circle that needs the distance and velocity, but we now know both of those, so we can say that the Moon's acceleration is this:

• $a=(\frac{2\pi}{P})^2M$
Is that of any use?

Well, we know that acceleration due to gravity is what holds the Moon in orbit, so if only we knew how hard the Earth is pulling the Moon, then we would know that.

But we do.

 $a=v^2/M$ $\quad=[(2\pi{}M)/P]^2/M$ $\quad=(2\pi)^2M/P^2$ $\quad=(2\pi/P)^2M$

 We know that acceleration at the Earth's surface is g, and that it falls off as an inverse square. Hence the acceleration due to gravity at any distance, say M, is given by: $a=g.(R/M)^2$ where R is the Earth's radius.
But the Earth's radius is $40\times{}10^6/(2\pi),$ so putting it all together we get:

 $(2\pi/P)^2M=g.(R/M)^2$ $M^3=g(\frac{RP}{2\pi})^2$

Therefore

$M^3=g\left(\frac{RP}{2\pi}\right)^2$

And we know everything on the right hand side, except g.

But we can find g with a pendulum and a stopwatch. (I knew you'd be wondering where they came in.)

We know that the time taken for a complete swing of a pendulum is given by the formula:

• $T=2\pi\sqrt{L/g}$
Rearranging this we get:

• $g=L.(2\pi/T)^2$
We can substitute that into our earlier formula and we get

• $M^3=L.(RP/T)^2$
And now we know everything !!

Of course we have to go away and construct a pendulum, and then we have to measure how long it takes to swing. Typically we measure 10 swings, both back and forth, and then divide the total time by 10. We should also do that several times to make sure we get error bars on the result, because each one will vary slightly. There's lots to do here.

So what do we get?

so

$M=383\times{}10^6m$