Consider the design of a multi$-$jet Pelton wheel with parameters and operating conditions as given below:

Head: H $=200$m

Flow rate: Q $=4$ m$^3/$s

Nozzle velocity coefficient: K $=0\mathrm{.}98$

Wheel diameter: D $=1\mathrm{.}47$ m

Mechanical efficiency: n $=88\%$ Calculate the power output capacity of the turbine.