A liquid fuel used in aerospace applications has a tabulated density of

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Problem

A liquid fuel used in aerospace applications has a tabulated density of 48.0 lb ft−348.0\,\text{lb\,ft}^{-3}. For compatibility with international data sets, engineers must express this density in both kg m−3\text{kg\,m}^{-3} and g cm−3\text{g\,cm}^{-3}. Use the exact conversion factors 1 lb=0.4536 kg1\,\text{lb}=0.4536\,\text{kg} and 1 ft=0.3048 m1\,\text{ft}=0.3048\,\text{m}. Complete the tasks below. (a) Determine the density of the fuel in kg m−3\text{kg\,m}^{-3}. (b) Convert the result from part (a) to g cm−3\text{g\,cm}^{-3}. (c) Explain why the numerical value of the density is much smaller when expressed in g cm−3\text{g\,cm}^{-3} than when expressed in kg m−3\text{kg\,m}^{-3}, even though they describe the same physical quantity.

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