First off, in short, I'm thinking what you want to know about is escape velocity..which has little to do with altitude.
See...There is a way to travel along a path that isn't straight, but looks straight compared to, say, elliptical orbits. That is a hyperbolic escape trajectory, which depends on the mass of a planet to an extent, but also depends on the velocity of the space craft. A hyperbolic escape trajectory means that essentially, the space craft is on a path that will allow it, or has allowed it to escape the influence of the planet's gravity for all intensive purposes. The equation for the escape velocity is:
v >= sqrt(2GM/r), where r is the distance from the planet, G is the gravitational constant (which can be looked up), M is the mass of the planet.
For earth, a space craft has to be traveling at about 11 km/s to eventually escape, REGARDLESS of its altitude. If it continued at that speed, and the Earth was the ONLY body in the universe, eventually you would be able to just keep going forever. HOWEVER because there are other bodies in the universe, they exert influence on the space shuttle and so the shuttle's path will eventually be perturbed if it continues at this speed.
Now if that answer was completely irrelevant to you, I'm guessing what you mean is "what orbital altitude would the shuttle have to be at in order for gravity to be negligible...aka. At what orbital altitude can you consider the shuttle to be in a 'zero-gravity' environment?"
As the others have said, earth's gravitational influence extends to infinity. You might be wondering then about the earth's sphere of influence, which extends until the sun's influence takes over. In order for the ship to be affected negligibly by earth, the sun, or the solar system, you would have to travel deep into interstellar space, at least 2 light years away from the sun, between the sun and its closest neighboring star. That is the closest you could get to 0 g because it's the location where both gravitational fields of the sun and the star have minimal influence on the shuttle. If that's not good enough, the shuttle would have to venture into intergalactic space, somewhere between the milky way and its nearest galaxy neighbor. And even then, there would still be a bit of gravitational influence on the shuttle. So in short, for all gravity to be negligible, at least for a short period of time, you'd have to travel pretty far.
However, on a simpler note, you can approximate the altitude at which Earth's gravitational acceleration in particular exerts a certain amount of influence. There is a simple equation you can use to estimate the gravitational acceleration at a particular altitude.
g = g0 (re / (re + h) )^2
re = radius of earth (I typically use 6378 km) h = orbital altitude g0 = acceleration due to gravity at earth's surface (aka. 9.81 m/s^2)
The smaller g is, the less of an influence Earth's gravity will have on someone jumping out of the shuttle. You could try solving the equation for h for some really small g...like 0.00000000001 percent of g0 and see what you get. Keep in mind though, that if the earth's sphere of influence still dominates at that altitude, if you jump off the shuttle, you will still float back into earth orbit. For comparison, the international space station orbits between 280 and 460 km. Gravitational acceleration there is an average of 90% what it is on earth's surface. In contrast, g = 2.5 x 10^(-7) m/s^2 about halfway between the sun-centered orbits of earth and mars. That's really small.
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