I'm doing research for a movie. If you were in a space elevator/tower at an altitude of 250 miles, how much gravity would you experience? (I've heard various estimates of .9Gz and .65Gz)
How about if you were at an altitude of 22,236 miles?
I'm doing research for a movie. If you were in a space elevator/tower at an altitude of 250 miles, how much gravity would you experience? (I've heard various estimates of .9Gz and .65Gz)
How about if you were at an altitude of 22,236 miles?
Organic Marble gives a good answer. Hohmannfan gives a better answer if you want the net acceleration someone at that point of the elevator would feel.
Using both gravity and the so called centrifugal force, someone would feel .88 g's 250 miles up the elevator.
At 22237 miles altitude I get -7.23 millionths of a g which is darn near zero. Just a slight tug upward so that altitude is just a tad higher than geosynchronous orbit.
Here is a spreadsheet NetAccelOnElevator.xls. User inputs altitude in miles to the colored cell at the top. Below will appear the net acceleration in g's.
If you want to consider the centripetal force too, you can do that by just adding a little more to the equation already suggested by Organic Marble:
$$g_h=g_0 \left(\frac{r_e}{r_e + h}\right)^2 - \frac{4\pi^2 (r_e+h)}{t^2}$$
Where $h$ = height above sea level, $r_e$ = radius of Earth, $g_0$ = sea level gravity and the additional $t$ is the length of the Earth's rotational period.
The acceleration profile looks like this:
For the two values you have chosen, the acceleration is 0.88g for 250 miles, and 0g for 22236 miles, usually known as the geostationary altitude,
I could calculate it for you, but using the "Teach a Man to Fish" principle, here's a simple equation (lifted from Wikipedia)
$$ g_h = g_0 \left( \frac{r_e}{r_e + h} \right) ^2 $$
where:
$h$ = height above sea level
$r_e$ = radius of Earth
$g_0$ = sea level gravity
Use the units of your choice.
Note: this accounts for altitude effects only and not centripetal force.