Ban air-conditioner to cool the air injected into the cabin
b
(b)
Compression of a gas in a compressor is nearly an adiabatic process.
So, by using $p_{\text {in }}^{1-\gamma} \cdot T_{\text {in }}^\gamma=p_{\text {out }}^{1-\gamma} \cdot T_{\text {out }}^\gamma$
We get, $(0.28)^{1-\gamma}(233)^\gamma=(1)^{1-\gamma}(T)^\gamma$
Here, for air, $\gamma=14=\frac{7}{5}$
Hence, $T=(233)(0.28)^{-2 / 7}=\frac{233}{(0.28)^{2 / 7}}$
This temperature is much higher than $298 \,K$ or $25^{\circ} C$.
So, an air-conditioner is needed to cool the air coming out of compressor.