Answer:
The ratio of the mass of oxygen inhaled for each breath at this high altitude compared to that at sea level is 64.7 %
Step-by-step explanation:
Mass of air at sea level is given by;
![m_o = \rho_o V_o](https://img.qammunity.org/2021/formulas/engineering/college/aznpg8f7op6ua6a2s4awfsgqd2bwc43oqp.png)
Mass of air at 14,200 ft altitude is given by;
![m_(14.2) = \rho _(14.2) V_(14.2)](https://img.qammunity.org/2021/formulas/engineering/college/iw5nlgu4th5c1fz8rwj39yqqxpqetw9ei1.png)
The ratio of the mass of oxygen at high altitude to that at sea level is given by;
![(m_(14.2))/(m_o) = (\rho _(14.2) V_(14.2))/(\rho _oV_(o))\\\\ Assume \ that \ the \ air \ composition \ (V_(14.2) = V_o)\\\\(m_(14.2))/(m_o) = (\rho _(14.2) )/(\rho _o)\\\\](https://img.qammunity.org/2021/formulas/engineering/college/fh24npdbns929h8sk8jcbn78ywsp2ytkuj.png)
density of air at sea level,
![\rho _o = 0.002378 \ slug/ft^3](https://img.qammunity.org/2021/formulas/engineering/college/wawv9vi7h16jm1nmny1k3p6pgso8rgug9d.png)
density of air at 10,000 ft = 0.001756 slug/ft³
density of air at 14,200 ft = x
density of air at 15,000 ft, = 0.001496 slug/ft³
Interpolate between 10,000 ft and 15,000 ft
![(14,200 - 10,000)/(15,000-10,000) = (X - 0.001756)/(0.001496 -0.001756)\\\\ 0.84(-0.00026) = X - 0.001756\\\\-0.0002184 = X - 0.001756\\\\X = 0.001756 - 0.0002184\\\\ X = 0.001538 \ slug/ft^3](https://img.qammunity.org/2021/formulas/engineering/college/2fgmuin5k14f2nswdt6cx8lkt3q1smssdn.png)
The ratio of the mass of oxygen at 14,200 ft to that at sea level is given by;
![(m_(14.2))/(m_o) = (\rho _(14.2))/(\rho_o) \\\\(m_(14.2))/(m_o) =(0.001538)/(0.002378) = 0.647 = 64.7 \%](https://img.qammunity.org/2021/formulas/engineering/college/kw94ytljubtavhraj5c2c1fh8x3706phty.png)
Therefore, the ratio of the mass of oxygen inhaled for each breath at this high altitude compared to that at sea level is 64.7 %