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Keep $A=\beta G{M}_{\star }/c$ constant. A circular circumstellar orbit stays circular in the secular drag approximation, and $da/dt=-2A/a$ integrates to $a^2=a_p^2-4At$. The inspiral time under Poynting–Robertson drag to the stellar surface isThe final expression treats the star as a point, or assumes $R_{\star }\ll a_p$.

For the coplanar circumplanetary orbit used in the preceding result, $da/dt=-3Aa/a_p^2$, so $a=a_0\exp (-3At/a_p^2)$. The inspiral time of circumplanetary dust to the planet's surface, for $a_0>R_p$, isThus the timescales have the same dependence on stellar flux and $\beta$, but planetary arrival contains a logarithm of the initial planetocentric radius. It is not always shorter: for a point star, $t_{\mathrm{cp}}<t_{\mathrm{cs}}$ only if $a_0/R_p<e^{3/4}$. A constant tilted-orbit average replaces three by its appropriate orientation coefficient. Sublimation or other removal can terminate the evolution before either idealized arrival time.