The difference in temperatures is
\(D(t) = T(\v{r}_1(t)) - T(\v{r}_2(t))\text{.}\) The rate of change is
\(D'(t) = \frac{d}{dt}T(\v{r}_1(t)) - \frac{d}{dt}T(\v{r}_2(t))\text{.}\) By the Chain Rule,
\(\frac{d}{dt}T(\v{r}(t)) = \nabla T(\v{r}(t)) \cdot \v{r}'(t)\text{.}\)
First, calculate the gradient of \(T\text{:}\)
\begin{equation*}
\nabla T = \la 2xy(1-z), x^2(1-z), -x^2y \ra
\end{equation*}
Spacecraft 1: Evaluate path and velocity at \(t = \pi\text{:}\)
\begin{align*}
\v{r}_1(\pi) \amp= \la \sin(\pi), \pi, \pi^2 \ra = \la 0, \pi, \pi^2 \ra \\
\v{r}_1'(t) \amp= \la \cos(t), 1, 2t \ra \implies \v{r}_1'(\pi) = \la -1, 1, 2\pi \ra
\end{align*}
Evaluate gradient at \(\v{r}_1(\pi)\text{:}\)
\begin{equation*}
\nabla T(0, \pi, \pi^2) = \la 2(0)(\pi)(1-\pi^2), (0)^2(1-\pi^2), -(0)^2(\pi) \ra = \la 0, 0, 0 \ra
\end{equation*}
Rate of change for spacecraft 1:
\begin{equation*}
\frac{d}{dt}T(\v{r}_1(\pi)) = \la 0, 0, 0 \ra \cdot \la -1, 1, 2\pi \ra = 0
\end{equation*}
Spacecraft 2: Evaluate path and velocity at \(t = \pi\text{:}\)
\begin{align*}
\v{r}_2(\pi) \amp= \la \cos(\pi), 1-\pi, \pi^3 \ra = \la -1, 1-\pi, \pi^3 \ra \\
\v{r}_2'(t) \amp= \la -\sin(t), -1, 3t^2 \ra \implies \v{r}_2'(\pi) = \la 0, -1, 3\pi^2 \ra
\end{align*}
Evaluate gradient at \(\v{r}_2(\pi)\text{:}\)
\begin{align*}
\nabla T(-1, 1-\pi, \pi^3) \amp= \la 2(-1)(1-\pi)(1-\pi^3), (-1)^2(1-\pi^3), -(-1)^2(1-\pi) \ra \\
\amp= \la -2(1-\pi)(1-\pi^3), 1-\pi^3, -(1-\pi) \ra \\
\amp= \la 2(\pi-1)(1-\pi^3), 1-\pi^3, \pi-1 \ra
\end{align*}
Rate of change for spacecraft 2:
\begin{align*}
\frac{d}{dt}T(\v{r}_2(\pi)) \amp= \la 2(\pi-1)(1-\pi^3), 1-\pi^3, \pi-1 \ra \cdot \la 0, -1, 3\pi^2 \ra \\
\amp= 0 - (1-\pi^3) + 3\pi^2(\pi-1) \\
\amp= \pi^3 - 1 + 3\pi^3 - 3\pi^2 = 4\pi^3 - 3\pi^2 - 1
\end{align*}
Finally, calculate the rate of change of the difference:
\begin{align*}
D'(\pi) \amp= \frac{d}{dt}T(\v{r}_1(\pi)) - \frac{d}{dt}T(\v{r}_2(\pi)) \\
\amp= 0 - (4\pi^3 - 3\pi^2 - 1) \\
\amp= -4\pi^3 + 3\pi^2 + 1
\end{align*}