Escape Velocity for Moon: Is the Equation Wrong?

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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).

Table 8.2: Approximate Astrometric Data for the Planets, listing body, symbol, average radius in km, and mu in km^3/sec^2 for Sun, Mercury, Venus, Earth, Moon, Mars, Jupiter, Saturn, Uranus, Neptune and Pluto, followed by escape velocity and circular orbit formulas for the Moon.
 
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.