Posted by Anonymous on Monday, February 21, 2011 at 11:33am.
I find the hints confusing. Here is the formula you need.
M*g = (1/2)*rho*A*Cd*V^2
Solve for the limiting velocity, V
*Cd is the dimensionless "drag coefficient", which is about 1.5 for a hemispherical parachute shape.
*rho is the density of air
*A is the projected area of the parachute (pi R^2), (not the surface area)
*g is the acceleration of gravity
* M is the mass
For more about the formula, see
http://my.execpc.com/~culp/rockets/descent.html
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