The parachute in the chapter-opener photo is, of course, meant to decelerate the payload on Mars. The wind tunnel test gave a drag coefficient of about $1.1,$ based upon the projected area of the parachute. Suppose it was falling on earth and, at an altitude of $1000 \mathrm{m},$ showed a steady descent rate of about $18 \mathrm{mi} / \mathrm{h}$. Estimate the weight of the payload.