Posted by Steve on Wednesday, March 19, 2008 at 4:32pm.
Escape velocity is Ve = sqrt(2µ/r) where µ = the gravitational constant of the earth = 3.9863x10^14m^3/sec.^2 and r = the radius of the earth = 3963 miles = 6.377519x10^6 meters.
The earth's surface velocity at the equator is [3963(5280)2(3.1416)/3.281]/[86,400sec. = .0463m/s.
The vertical escape velocity is therefore 1.1180m/s.
Launching eastward, the escape velocity for the rockets 1.1180 - .0463 = 1.0707m/s.
Launchung westward, the escape velocity is 1.1180 + .0463 = 1.1643m/s.
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