$\bullet$ $\bullet$ When its $75-\mathrm{kW}(100-\mathrm{hp})$ engine is generating full power,
a small single-engine airplane with mass 700 $\mathrm{kg}$ gains altitude
at a rate of 2.5 $\mathrm{m} / \mathrm{s}(150 \mathrm{m} / \mathrm{min},$ or 500 $\mathrm{ft} / \mathrm{min}$ ). What frac-
tion of the engine power is being used to make the airplane
climb? (The remainder is used to overcome the effects of air
resistance and of inefficiencies in the propeller and engine.)