Slowing down of space cehicle. A space vehicle has mass $200 \mathrm{~kg}$ and eross-sectional area $2 \times 10^{4} \mathrm{~cm}^{2} .$ It travels in a region without appreciable gravitational field through a rarefied atmosphere whose mass density is $2 \times 10^{-15} \mathrm{~g} / \mathrm{ce}$ with initial speed $7.6 \times 10^{5} \mathrm{em} / \mathrm{s}$. (These would be approximate values for a satellite $500 \mathrm{~km}$ above the surface of the earth.) Assume that the conditions of the example on page 183 apply, that all the gas the space vehicle encounters sticks to it.
(a) Work out the value of $c$. Consider the mass of gas picked up in $1 \mathrm{~s}$. Ans. $c=4 \times 10^{-11} \mathrm{~g} / \mathrm{cm}$.
(b) Using the conservation of momentum $M v=M_{0} v_{0}$, find the differential equation for $v$ in terms of $t$ and constants. $\mathrm{Ans}, d v / d t=-c v^{3} / M_{0} v_{0^{-}}$
(c) Solve for $v$ and find the time required for the satellite to slow down to $0.9$ of its initial speed.