A multicylinder gasoline engine in an airplane, operating at $2.50 \times 10^{3}$ rev $/$ min, takes in energy $7.89 \times 10^{3} \mathrm{J}$ and exhausts $4.58 \times 10^{3} \mathrm{J}$ for each revolution of the crankshaft.
(a) How many liters of fuel does it consume in $1.00 \mathrm{h}$ of operation if the heat of combustion of the fuel is equal to $4.03 \times 10^{7} \mathrm{J} / \mathrm{L} ?(\mathrm{b})$ What is the mechanical power output of the engine? Ignore friction and express the answer in horsepower. (c) What is the torque exerted by the crankshaft on the load? (d) What power must the exhaust and cooling system transfer out of the engine?