Hey, I've sort of challenged myself to figure this out, and I've been working on it for about an hour to no avail, Google didn't help either. I'm not even sure if it is remotely possible but I thought I would at least try!
Me = Mass of Earth, 5.97*10^24m
Mo = Mass of object, let's say, a space shuttle
re = Radius of Earth, 6.38*10^6m
I'm not really sure of the coefficient symbol for altitude so let's go with Ax, Ax = 400km
Gravity at altitude = 8.68m/s/s
G = 6.67*10^-11
And the formula I have been using are as follows:
Mo*g = G*(Me * Mo)/re^2
F = Mo*g
Mo*g = G*(Me * Mo)/(re^2 * Ax)
Is it possible? I really hope it is
Much love to anyone who can help~
Me = Mass of Earth, 5.97*10^24m
Mo = Mass of object, let's say, a space shuttle
re = Radius of Earth, 6.38*10^6m
I'm not really sure of the coefficient symbol for altitude so let's go with Ax, Ax = 400km
Gravity at altitude = 8.68m/s/s
G = 6.67*10^-11
And the formula I have been using are as follows:
Mo*g = G*(Me * Mo)/re^2
F = Mo*g
Mo*g = G*(Me * Mo)/(re^2 * Ax)
Is it possible? I really hope it is
Much love to anyone who can help~