The $200-kg$ satellite has a radius of gyration about the centroidal $z$ axis of $k_z=1\mathrm{.}15m.$ Initially it is rotating with a constant angular velocity of ${}_0=\{1400k\}re\frac{v}{m}in$ as

Part A shown in $($Figure $1).$

If the two jets A and $B,$ both in the $x-y$ plane, are fired simultaneously and produce a thrust of $T=(5e^{-0\mathrm{.}1t})kN,$ where $t$ is in seconds, determine the angular velocity of the satellite, five seconds after firing.

Enter the $x,y,$ and $z$ components of the angular velocity in radians per second to three significant figures separated by commas.

Figure

$1$ of $1$