The turbine for a new jet engine was designed for entrance conditions of 160 psia and $1700^{\circ} \mathrm{F}$, ingesting $500 \mathrm{lbm} / \mathrm{s}$ at a speed of $500 \mathrm{rpm},$ and exit conditions of 80 psia and $1350^{\circ} \mathrm{F}$. If the altitude and fueling for the engine were changed such that the entrance conditions were now 140 psia and $1600^{\circ} \mathrm{F}$, calculate the new operating speed, mass flow rate, and exit conditions for similar operation, i.e. equal efficiency.