Escape Velocity for Moon: Is the Equation Wrong?

AI Thread Summary
The discussion centers on the calculation of escape velocity for the Moon, highlighting a potential error in the equation presented on a specific page. The correct formula for escape velocity is v,escape = (2*mu/r)^(1/2), where mu = G*M. It is noted that the page incorrectly calculates the escape velocity by using the formula for orbital speed just above the Moon's surface. To find the escape speed, one must multiply the orbital speed by the square root of two. The clarification resolves the confusion regarding the calculations.
eurekameh
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v,escape = (2*mu/r)^(1/2), where mu = G*M. What I'm asking is if this page is wrong about calculating the escape velocity for the moon. They seem to have the equation wrong (missing 2 in front of mu = G*M,moon).

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If you study the text closely you'll see that they're calculating the orbital speed for a circular orbit just above the Moon's surface, not the escape speed. Multiply by root two to get the escape speed.
 
Ah, somehow missed it. Thanks.
 
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