The initial conditions at the inlet of a gas turbine compressor are 123 kPa and 385 K. The air is compressed until a pressure of 1275 kPa is reached. Expansion is carried out in two stages. In the first turbine, the conditions at the inlet are 1520 K and it expands to a pressure of 385 kPa and is reheated to 1495 K. The efficiency of the compressor is 87%, the efficiency of the two turbines are: the high turbine is 98% and the low turbine is 91%, with a regeneration efficiency of 87%. If the air flows through the cycle at a ratio of 69 kg/s, determine the cycle power, compressor work, and thermal efficiency. Consider constant specific heat.