General Chemistry 202-SN1-RE • CEGEP, Montreal

Corrected exercises: gases and kinetic theory (202-SN1-RE)

The secondary school gas chapter stops at the ideal gas law. In General Chemistry, 202-SN1-RE (formerly 202-NYA), three questions are added, and they are the ones that make the exam: what happens when several gases share the same container (Dalton's law and partial pressures), how fast the molecules really move (kinetic theory, root-mean-square speed, the Maxwell-Boltzmann distribution, Graham's law), and when the ideal gas law stops being true (the van der Waals equation, the compressibility factor).

By the end of the set you can apply the combined gas law and its special cases, Boyle's, Charles's and Gay-Lussac's laws (exercise 1), calculate a root-mean-square speed (exercise 3), compare effusion rates up to uranium enrichment (exercise 4), correct a pressure with the van der Waals equation (exercise 5), identify a gas from its density (exercise 6), do the stoichiometry of an airbag and the pressure after a reaction in a rigid container (exercise 7), read the three Maxwell-Boltzmann speeds and atmospheric escape (exercise 8), and calculate a compressibility factor and the Boyle temperature (exercise 9).

Exercise 2, on collecting a gas over water, holds the most profitable trap of the chapter: a gas collected by displacement of water is always MOIST, and forgetting to subtract the water vapour pressure throws the result off by 2 to 3%, without ever giving an absurd value. The last exercise applies Dalton's law to scuba diving and Nitrox, where the result is frankly counterintuitive.

10 corrected exercises • 100 points • 150 minutes

This chapter is part of 202-SN1-RE, every chapter with its set and sheet Before you start Revision sheet: the traps and the method for this chapter

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Course recap

  • • Constants: R = 8.314 kPa·L/(mol·K); 101.3 kPa = 1 atm = 760 mm Hg; T(K) = T(°C) + 273. Molar volume 22.4 L/mol at STP (0 °C, 101.3 kPa).
  • • Combined gas law: for a closed amount of gas, P1V1T1=P2V2T2\dfrac{P_{1}V_{1}}{T_{1}}=\dfrac{P_{2}V_{2}}{T_{2}}. Boyle's law (TT constant), Charles's law (PP constant) and Gay-Lussac's law (VV constant) are only special cases of it. Temperatures are ALWAYS in kelvins, because these laws involve a ratio of temperatures.
  • • Ideal gas law: PV=nRTPV=nRT. Molar mass of a gas: M=mRTPVM=\dfrac{mRT}{PV}, and density ρ=PMRT\rho=\dfrac{PM}{RT}.
  • • Dalton's law: the total pressure is the sum of the partial pressures, Ptotal=∑PiP_{\text{total}}=\sum P_{i}. Each partial pressure is Pi=xiPtotalP_{i}=x_{i}P_{\text{total}}, where xix_{i} is the MOLE FRACTION.
  • • Collecting over water: the gas collected is saturated with water vapour, so Pgas=Patm−Pvap(T)P_{\text{gas}}=P_{atm}-P_{vap}(T). The vapour pressure depends ONLY on the temperature.
  • • Kinetic theory: the average kinetic energy depends only on the temperature, Ek‾=32RT\overline{E_{k}}=\frac{3}{2}RT per mole. Root-mean-square speed vrms=3RTMv_{rms}=\sqrt{\dfrac{3RT}{M}}, with R = 8.314 J/(mol·K) and M in kg/mol.
  • • Graham's law: at the same temperature, v1v2=M2M1\dfrac{v_{1}}{v_{2}}=\sqrt{\dfrac{M_{2}}{M_{1}}}. The LIGHT gas effuses fastest.
  • • Real gases, van der Waals equation: P=nRTV−nb−an2V2P=\dfrac{nRT}{V-nb}-\dfrac{an^{2}}{V^{2}}. The bb term corrects for the volume of the molecules themselves, the aa term corrects for the attractions.
  • • Gas stoichiometry: at fixed TT and PP, gas volumes are proportional to amounts of substance, so the coefficients of the equation can be read directly as volumes. In a rigid container, the pressure depends only on the TOTAL number of moles of gas, whatever their nature.
  • • Maxwell-Boltzmann distribution: vp=2RTM<vavg=8RTπM<vrms=3RTMv_{p}=\sqrt{\dfrac{2RT}{M}}<v_{avg}=\sqrt{\dfrac{8RT}{\pi M}}<v_{rms}=\sqrt{\dfrac{3RT}{M}}. Heating the gas or making it lighter shifts the curve to the right and flattens it; the area under the curve is always 1.
  • • Compressibility factor: Z=PVnRTZ=\dfrac{PV}{nRT}, equal to 1 for an ideal gas. Z<1Z<1 means the attractions dominate, Z>1Z>1 that the volume of the molecules themselves dominates. The first-order coefficient in PP vanishes at the Boyle temperature TB=aRbT_{B}=\dfrac{a}{Rb}.

Part A: Gas laws, partial pressures, kinetic theory and effusion (/50)

Exercise 1: The simple laws and the combined gas law

Before Dalton and before kinetic theory, the whole chapter rests on a single relation between two states of the same amount of gas: P1V1T1=P2V2T2\dfrac{P_{1}V_{1}}{T_{1}}=\dfrac{P_{2}V_{2}}{T_{2}}. Boyle's, Charles's and Gay-Lussac's laws are only special cases of it, obtained by freezing one of the three variables.

Take R=8.314R=8.314 kPa·L/(mol·K) and 1 atm = 101.3 kPa.

The diagram below shows the two situations.

rigid cylinderV = 12.0 L20,265 kPa at 20 °Cin the sun: 55 °CP = ?at ground level:25.0 m³ of helium101.3 kPa, 20 °Cat 20 km: 5.5 kPa, −50 °CV = ?flexible weather balloon
  • a) A rigid scuba cylinder of 12.0 L contains air at 20,265 kPa (200 atm) and 20 °C. Left in the sun, it reaches 55 °C. Calculate the new pressure. Which particular law did you apply, and why does the volume play no role?
  • b) A flexible weather balloon carries 25.0 m³ of helium at ground level, where the pressure is 101.3 kPa and the temperature 20 °C. At an altitude of 20 km, the pressure is only 5.5 kPa and the temperature −50-50 °C. Calculate the volume of the balloon at that altitude.
  • c) Check the result of b) by calculating the amount of helium at ground level and then at altitude with the ideal gas law. What should you find, and why?
  • d) A student redoes the calculation of a) keeping the temperatures in degrees Celsius. What pressure does the student get? Explain why the Celsius scale is unusable here, although it works perfectly well for a temperature difference.

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  • a) P2=22,686P_{2}=22{,}686 kPa, that is 224 atm: Gay-Lussac's law, the volume cancels
  • b) V2=350V_{2}=350 m³, which is 14 times the volume at ground level
  • c) 1040 mol in both cases: the balloon is closed
  • d) 55,729 kPa, that is 550 atm: a ratio of temperatures requires kelvins
a)

The container is rigid, so V1=V2V_{1}=V_{2} and the relation reduces to P1T1=P2T2\dfrac{P_{1}}{T_{1}}=\dfrac{P_{2}}{T_{2}}: this is Gay-Lussac's law. With T1=20+273=293T_{1}=20+273=293 K and T2=55+273=328T_{2}=55+273=328 K, we get P2=P1T2T1=20,265×328293=22,686P_{2}=P_{1}\dfrac{T_{2}}{T_{1}}=20{,}265\times\dfrac{328}{293}=22{,}686 kPa, that is 224 atm. The volume does not appear because it cancels on both sides: only its constancy matters, not its value. A rise of 35 °C therefore pushes the pressure up by 24 atmospheres, which is why a cylinder must never be left in the sun.

b)

Here all three quantities change, so we need the combined gas law: V2=V1P1P2×T2T1=25.0×101.35.5×223293=25.0×18.42×0.761=350V_{2}=V_{1}\dfrac{P_{1}}{P_{2}}\times\dfrac{T_{2}}{T_{1}}=25.0\times\dfrac{101.3}{5.5}\times\dfrac{223}{293}=25.0\times 18.42\times 0.761=350 m³. The balloon therefore swells by a factor of 14. The two effects work in opposite directions: the drop in pressure multiplies the volume by 18.4 while the cooling divides it by 1.31; the pressure wins by a wide margin. This is why a weather balloon is released half empty and ends up bursting at altitude.

c)

At ground level: n=PVRT=101.3×25,0008.314×293=1040n=\dfrac{PV}{RT}=\dfrac{101.3\times 25{,}000}{8.314\times 293}=1040 mol, after converting the 25.0 m³ to 25,000 L. At altitude: n=5.5×350,4508.314×223=1040n=\dfrac{5.5\times 350{,}450}{8.314\times 223}=1040 mol. We find exactly the same value, which is what we should get since the balloon is closed: the amount of substance is conserved. This is in fact the proof of the combined gas law, which is nothing but the statement of PVT=nR\dfrac{PV}{T}=nR at two instants for the same nn. This check through the amount of substance is the best way to verify a combined gas law exercise.

d)

With degrees Celsius, the student would get P2=20,265×5520=55,729P_{2}=20{,}265\times\dfrac{55}{20}=55{,}729 kPa, that is 550 atm: the cylinder would explode. The error is major because the ratio 5520=2.75\dfrac{55}{20}=2.75 has nothing to do with the true ratio 328293=1.12\dfrac{328}{293}=1.12. The reason is that the gas laws involve a RATIO of temperatures, and a ratio only makes sense on a scale whose zero is the true zero, that is, the kelvin. On the Celsius scale the zero is arbitrary: saying that it is twice as hot at 20 °C as at 10 °C has no physical meaning. A temperature DIFFERENCE, on the other hand, is the same on both scales, since the offset of 273 cancels: this is why a heat capacity can be written equally well in J/(g·°C) or J/(g·K).

2468101251015202530higher Tlower TV (L)P (kPa)

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Exercise 2: Dalton's law and gas collected over water

In a mixture, each gas behaves as if it were alone: it exerts the pressure it would have if it occupied the whole volume. The total pressure is simply the sum of these contributions, weighted by the mole fractions.

Molar masses: HeHe 4.003 g/mol; O2O_{2} 32.00 g/mol; H2H_{2} 2.016 g/mol.

The diagram below shows the mixture of a) and the setup of c).

a) 5.00 L, 25 °C2.00 g He8.00 g O₂HeO₂H₂(g)250 mL22 °CPatm = 101.3 kPac) H₂ produced
  • a) 2.00 g of helium and 8.00 g of oxygen gas are sealed in a 5.00 L flask at 25 °C. Calculate the two partial pressures and the total pressure.
  • b) Calculate the mole fraction of helium and check that it gives back its partial pressure.
  • c) Hydrogen gas is collected by displacement of water: 250 mL at 22 °C, under an atmospheric pressure of 101.3 kPa. The vapour pressure of water at 22 °C is 2.6 kPa. Calculate the mass of H2H_{2} collected.
  • d) What relative error does a student make by forgetting the water vapour correction? Why is this error hard to detect?

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  • a) n(He)=0.4996n(He)=0.4996 mol and n(O2)=0.2500n(O_{2})=0.2500 mol; 247.6 kPa, 123.9 kPa, total 371.5 kPa
  • b) x(He)=0.6665x(He)=0.6665, and 0.6665×371.5=247.60.6665\times 371.5=247.6 kPa
  • c) P(H2)=98.7P(H_{2})=98.7 kPa, n=1.006×10−2n=1.006\times 10^{-2} mol, that is 20.3 mg
  • d) +2.6%+2.6\%: a perfectly plausible error, hence an invisible one
a)

First convert: T=25+273=298T=25+273=298 K. Amounts of substance: n(He)=2.004.003=0.4996n(He)=\dfrac{2.00}{4.003}=0.4996 mol and n(O2)=8.0032.00=0.2500n\left(O_{2}\right)=\dfrac{8.00}{32.00}=0.2500 mol. Each gas alone occupies the 5.00 L: P(He)=0.4996×8.314×2985.00=247.6P(He)=\dfrac{0.4996\times 8.314\times 298}{5.00}=247.6 kPa and P(O2)=0.2500×8.314×2985.00=123.9P\left(O_{2}\right)=\dfrac{0.2500\times 8.314\times 298}{5.00}=123.9 kPa. The total pressure is their sum: Ptotal=371.5P_{\text{total}}=371.5 kPa. Note that helium, which has one quarter of the mass, gives twice the pressure: it is the amount of MATTER that counts, never the mass.

b)

x(He)=0.49960.4996+0.2500=0.49960.7496=0.6665x(He)=\dfrac{0.4996}{0.4996+0.2500}=\dfrac{0.4996}{0.7496}=0.6665. Then P(He)=x(He)×Ptotal=0.6665×371.5=247.6P(He)=x(He)\times P_{\text{total}}=0.6665\times 371.5=247.6 kPa: we do recover the value from a). The two routes are equivalent, and the second is faster when the composition is given in percentages.

c)

The gas collected over water is saturated with vapour: the pressure measured is that of the mixture. So P(H2)=101.3−2.6=98.7P\left(H_{2}\right)=101.3-2.6=98.7 kPa. With T=22+273=295T=22+273=295 K and V=0.250V=0.250 L: n=PVRT=98.7×0.2508.314×295=1.006×10−2n=\dfrac{PV}{RT}=\dfrac{98.7\times 0.250}{8.314\times 295}=1.006\times 10^{-2} mol. The mass is m=1.006×10−2×2.016=2.03×10−2m=1.006\times 10^{-2}\times 2.016=2.03\times 10^{-2} g, or about 20 mg.

d)

Without the correction, the student would use 101.3 kPa and find n=1.033×10−2n=1.033\times 10^{-2} mol, an error of +2.6+2.6%. The error is hard to detect because the result remains perfectly PLAUSIBLE: right order of magnitude, right units, no absurd value. Only a careful reading of the problem, which contains the words “collected over water” and a vapour pressure given for no apparent reason, can reveal it. RULE: if a water vapour pressure is supplied in the problem, it is there to be used.

N₂: 60 kPax = 0.60O₂: 28 kPax = 0.28H₂O: 12 kPax = 0.12total100 kPa

Exercise 3: Kinetic theory: how fast do molecules move?

The pressure of a gas comes from the collisions of its molecules with the walls. Kinetic theory links this microscopic picture to measurable quantities, and it gives a surprising result: the speed of air molecules is of the same order as the speed of sound.

Here R = 8.314 J/(mol·K) and the molar masses are in kg/mol.

The diagram below shows the two gases at the same temperature.

helium, 25 °Coxygen gas, 25 °Cmolecules colliding with the walls
  • a) Calculate the root-mean-square speed of helium and that of oxygen gas at 25 °C.
  • b) Check that the ratio of the two speeds depends only on the molar masses.
  • c) Calculate the average kinetic energy per mole at 25 °C. Is it the same for both gases? Justify your answer.
  • d) By what factor is the root-mean-square speed multiplied if the absolute temperature is doubled? And if the pressure is doubled at constant temperature?

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  • a) vrms(He)=1363v_{rms}(He)=1363 m/s and vrms(O2)=482v_{rms}(O_{2})=482 m/s
  • b) 2.83=32.00/4.0032.83=\sqrt{32.00/4.003}: the factor 3RT3RT cancels
  • c) Ek‾=3716\overline{E_{k}}=3716 J/mol, the SAME for every ideal gas at 298 K
  • d) 2≈1.41\sqrt{2}\approx 1.41 if TT doubles; nothing at all if PP doubles
a)

vrms=3RTMv_{rms}=\sqrt{\dfrac{3RT}{M}} with MM in kg/mol. For helium, M=4.003×10−3M=4.003\times 10^{-3} kg/mol: vrms=3×8.314×2984.003×10−3=1.857×106=1363v_{rms}=\sqrt{\dfrac{3\times 8.314\times 298}{4.003\times 10^{-3}}}=\sqrt{1.857\times 10^{6}}=1363 m/s. For oxygen gas, M=32.00×10−3M=32.00\times 10^{-3} kg/mol: vrms=74330.03200=482v_{rms}=\sqrt{\dfrac{7433}{0.03200}}=482 m/s. An O2O_{2} molecule therefore moves at nearly 1700 km/h at room temperature.

b)

v(He)v(O2)=1363482=2.83\dfrac{v(He)}{v\left(O_{2}\right)}=\dfrac{1363}{482}=2.83. On the other hand, M(O2)M(He)=32.004.003=7.99=2.83\sqrt{\dfrac{M\left(O_{2}\right)}{M(He)}}=\sqrt{\dfrac{32.00}{4.003}}=\sqrt{7.99}=2.83: the two coincide. Indeed, in the ratio 3RT/M1÷3RT/M2\sqrt{3RT/M_{1}}\div\sqrt{3RT/M_{2}}, the factor 3RT3RT cancels, and only the molar masses remain. This is exactly Graham's law.

c)

Ek‾=32RT=32×8.314×298=3716\overline{E_{k}}=\dfrac{3}{2}RT=\dfrac{3}{2}\times 8.314\times 298=3716 J/mol, or 3.72 kJ/mol. This value is the SAME for both gases, and for every ideal gas: the average kinetic energy depends only on the temperature. This is in fact the microscopic definition of temperature. Light molecules make up for their small mass with a higher speed, so that the product 12mv2\frac{1}{2}mv^{2} stays the same.

d)

Since vrms∝Tv_{rms}\propto\sqrt{T}, doubling the absolute temperature multiplies the speed by 2≈1.41\sqrt{2}\approx 1.41, not by 2: it would take QUADRUPLING TT to double the speed. Doubling the pressure at constant temperature changes NOTHING about the speed: vrmsv_{rms} depends only on TT and MM. Compressing a gas increases the FREQUENCY of the collisions, not their individual violence. This is the most common misconception of the chapter.

Exercise 4: Graham's law of effusion, from helium to uranium

Effusion is the passage of a gas through a tiny hole. Since the speed depends on the molar mass, light gases escape faster: it is the only process that separates isotopes without a chemical reaction.

Molar masses: HeHe 4.003; SF6SF_{6} 146.06; 235UF6^{235}UF_{6} 349.03; 238UF6^{238}UF_{6} 352.04 g/mol.

The diagram below shows the two gases, each in front of a tiny hole.

heliumsulfur hexafluoride SF₆tiny holesame temperature
  • a) How many times faster does helium effuse than sulfur hexafluoride at the same temperature?
  • b) A party balloon filled with helium deflates in a day, whereas a balloon filled with air lasts a week. Explain using this chapter.
  • c) An unknown gas effuses 2.92 times more SLOWLY than helium. Determine its molar mass and suggest what it is.
  • d) Calculate the ratio of the effusion rates of the two isotopes of UF6UF_{6}. Comment on the industrial difficulty of enriching uranium.

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  • a) Helium effuses 6.04 times faster than SF6SF_{6}
  • b) 2.69 times faster than air, and a small monatomic atom
  • c) M=34.1M=34.1 g/mol, that is hydrogen sulfide
  • d) 1.004301.00430, that is 0.43%0.43\% per pass: thousands of stages in a cascade
a)

v(He)v(SF6)=M(SF6)M(He)=146.064.003=36.49=6.04\dfrac{v(He)}{v\left(SF_{6}\right)}=\sqrt{\dfrac{M\left(SF_{6}\right)}{M(He)}}=\sqrt{\dfrac{146.06}{4.003}}=\sqrt{36.49}=6.04. Helium therefore effuses about six times faster.

b)

Two effects combine, but the main one is this: helium, with a molar mass of 4.003 g/mol, effuses 29.0/4.003=2.69\sqrt{29.0/4.003}=2.69 times faster than air, whose average molar mass is 29.0 g/mol. It therefore passes through the pores of the latex much more quickly. In addition, the helium atom is monatomic and very small, which makes its passage even easier. A helium balloon thus loses its lift in about a day.

c)

“Effusing 2.92 times more slowly” means v(He)v(X)=2.92\dfrac{v(He)}{v(X)}=2.92, so M(X)4.003=2.92\sqrt{\dfrac{M(X)}{4.003}}=2.92 and M(X)=4.003×2.922=4.003×8.53=34.1M(X)=4.003\times 2.92^{2}=4.003\times 8.53=34.1 g/mol. This mass matches hydrogen sulfide H2SH_{2}S, whose molar mass is 34.08 g/mol. Check: 34.08/4.003=2.92\sqrt{34.08/4.003}=2.92. Reading pitfall: “more slowly” puts the unknown mass in the NUMERATOR under the square root; inverting it would give M=0.47M=0.47 g/mol, an impossible value since it is smaller than that of hydrogen.

d)

v(235UF6)v(238UF6)=352.04349.03=1.00862=1.00430\dfrac{v\left(^{235}UF_{6}\right)}{v\left(^{238}UF_{6}\right)}=\sqrt{\dfrac{352.04}{349.03}}=\sqrt{1.00862}=1.00430. The difference is only 0.43% per pass. To enrich natural uranium, which contains 0.7% of 235U^{235}U, up to the 3 to 5% of nuclear fuel, THOUSANDS of effusion stages must therefore be chained in a cascade. This is what makes enrichment technically heavy, energy-hungry and easy to detect, a point with direct geopolitical consequences. Modern centrifuges exploit the same difference in mass, with a better yield per stage.

Exercise 5: Real gases and the van der Waals equation

The ideal gas law assumes point molecules with no interactions. Both assumptions fail under strong compression or on cooling: the van der Waals equation corrects each of them separately.

For CO2CO_{2}: a=364a=364 kPa·L²/mol² and b=0.0427b=0.0427 L/mol.

The diagram below shows the sample.

P = ?1.00 mol of CO₂V = 0.500 LT = 300 K
  • a) Calculate the pressure exerted by 1.00 mol of CO2CO_{2} in 0.500 L at 300 K, according to the ideal gas law.
  • b) Redo the calculation with the van der Waals equation, then give the relative difference.
  • c) Explain the physical role of each of the two correction terms, and say which one dominates here.
  • d) Under what conditions does the ideal gas law become an excellent approximation again? Justify from the equation.

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  • a) P=4988P=4988 kPa, nearly 49 atm
  • b) P=3998P=3998 kPa, that is −19.9%-19.9\%: the ideal gas law overestimates
  • c) +466+466 kPa for the molecular volume, −1456-1456 kPa for the attractions, which dominate
  • d) At low pressure and high temperature, the difference falls below 1%
a)

P=nRTV=1.00×8.314×3000.500=4988P=\dfrac{nRT}{V}=\dfrac{1.00\times 8.314\times 300}{0.500}=4988 kPa, nearly 49 atmospheres.

b)

P=nRTV−nb−an2V2=8.314×3000.500−0.0427−364×1.000.5002=24940.4573−1456=5454−1456=3998P=\dfrac{nRT}{V-nb}-\dfrac{an^{2}}{V^{2}}=\dfrac{8.314\times 300}{0.500-0.0427}-\dfrac{364\times 1.00}{0.500^{2}}=\dfrac{2494}{0.4573}-1456=5454-1456=3998 kPa. The relative difference is 3998−49884988=−19.9\dfrac{3998-4988}{4988}=-19.9%. The ideal gas law therefore OVERESTIMATES the pressure by nearly 20% under these conditions.

c)

The term nbnb subtracted from the volume represents the VOLUME OF THE MOLECULES THEMSELVES: the volume actually available for movement is smaller than the volume of the container, which INCREASES the pressure. The term an2V2\dfrac{an^{2}}{V^{2}} represents the ATTRACTIVE FORCES between molecules: a molecule about to hit the wall is held back by its neighbours, so it hits less hard, which DECREASES the pressure. Here the two corrections are +466+466 kPa and −1456-1456 kPa respectively: the attractive term clearly dominates, which makes sense for CO2CO_{2}, a molecule that is easily liquefied and therefore has strong interactions.

d)

At LOW pressure and HIGH temperature. At low pressure, the molar volume Vn\dfrac{V}{n} is large compared with bb, so V−nb≈VV-nb\approx V; and an2V2\dfrac{an^{2}}{V^{2}} becomes negligible compared with nRTV\dfrac{nRT}{V} since it decreases as 1V2\dfrac{1}{V^{2}} while the main term only decreases as 1V\dfrac{1}{V}. At high temperature, the average kinetic energy 32RT\frac{3}{2}RT becomes large compared with the attraction energy, and the molecules pass each other too quickly to be held back. In practice, at ambient conditions and up to a few atmospheres, the difference is below 1%: this is why secondary school can ignore this correction entirely.

Part B: Exam level (/50)

Exercise 6: Identifying a gas from its molar mass and density

The ideal gas law, rewritten with the mass, becomes an analytical tool: measuring a mass, a volume, a pressure and a temperature is enough to identify an unknown gas.

Average molar mass of air: 29.0 g/mol.

The diagram below shows the sample of b).

unknown gas: 0.887 gV = 500 mLθ = 100 °CP = 98.0 kPa
  • a) Starting from PV=nRTPV=nRT, derive the expressions for the molar mass MM and the density ρ\rho of a gas.
  • b) A gas sample of 0.887 g occupies 500 mL at 100 °C under 98.0 kPa. Calculate its molar mass and suggest what it is.
  • c) Calculate the density of air and that of helium at 25 °C under 101.3 kPa.
  • d) Deduce the maximum mass that a 10.0 L helium balloon can lift, neglecting the mass of the envelope.
  • e) Why does a hot-air balloon also rise, although its composition is identical to that of the surrounding air?

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  • a) M=mRTPVM=\dfrac{mRT}{PV} and ρ=PMRT\rho=\dfrac{PM}{RT}
  • b) n=1.580×10−2n=1.580\times 10^{-2} mol and M=56.1M=56.1 g/mol: butene
  • c) 1.186 g/L for air, 0.164 g/L for helium, ratio 7.24
  • d) 11.86−1.64=10.211.86-1.64=10.2 g of payload
  • e) Heating divides ρ\rho by 1.27: the hot air is 27% less dense
a)

From PV=nRTPV=nRT and n=mMn=\dfrac{m}{M}, we get PV=mMRTPV=\dfrac{m}{M}RT, hence M=mRTPVM=\dfrac{mRT}{PV}. Dividing by the volume, the density ρ=mV\rho=\dfrac{m}{V} satisfies ρ=PMRT\rho=\dfrac{PM}{RT}. This last relation shows that, for a given gas, the density is proportional to the pressure and inversely proportional to the absolute temperature.

b)

T=100+273=373T=100+273=373 K. First n=PVRT=98.0×0.5008.314×373=1.580×10−2n=\dfrac{PV}{RT}=\dfrac{98.0\times 0.500}{8.314\times 373}=1.580\times 10^{-2} mol. Then M=0.8871.580×10−2=56.1M=\dfrac{0.887}{1.580\times 10^{-2}}=56.1 g/mol. This value matches butene C4H8C_{4}H_{8}, whose molar mass is 56.11 g/mol. One could also think of iron, but iron is obviously not a gas at 100 °C: the physical state is part of the identification.

c)

T=298T=298 K. For air: ρ=101.3×29.08.314×298=1.186\rho=\dfrac{101.3\times 29.0}{8.314\times 298}=1.186 g/L. For helium: ρ=101.3×4.0038.314×298=0.164\rho=\dfrac{101.3\times 4.003}{8.314\times 298}=0.164 g/L. The ratio is 7.24, exactly that of the molar masses: at the same pressure and temperature, densities are proportional to molar masses, which is the direct translation of Avogadro's law.

d)

The buoyant force corresponds to the mass of displaced air, that is 1.186×10.0=11.861.186\times 10.0=11.86 g. The balloon already contains 0.164×10.0=1.640.164\times 10.0=1.64 g of helium. The maximum payload is the difference: 11.86−1.64=10.211.86-1.64=10.2 g. That is little: lifting one kilogram would take nearly 1000 L of helium, a balloon about 1.2 m in diameter.

e)

Because what matters for buoyancy is not the composition but the DENSITY. According to ρ=PMRT\rho=\dfrac{PM}{RT}, at constant pressure the density is inversely proportional to the absolute temperature. By heating the air from 20 °C to 100 °C, that is from 293 K to 373 K, we divide ρ\rho by 373293=1.27\dfrac{373}{293}=1.27: the air inside becomes 27% less dense than the air outside, and the buoyant force wins. It is the same principle as with helium, obtained not by changing MM but by changing TT.

Exercise 7: Gas stoichiometry and the pressure after a reaction

As soon as a gas takes part in a reaction, the ideal gas law becomes the conversion tool between the amount of substance and the measured quantities. In a rigid container, it is the TOTAL amount of gas that fixes the pressure, whatever the nature of the species.

The airbag inflates by decomposition of sodium azide: 2 NaN3→2 Na+3 N22\,NaN_{3}\rightarrow 2\,Na+3\,N_{2}. Molar masses (g/mol): NaNa 22.99; NN 14.01. Take R=8.314R=8.314 kPa·L/(mol·K).

The diagram below shows the container of c) before the spark.

P = ?CH₄: 0.100 molO₂: 0.300 molrigid container, 2.00 Lat 150 °C, then spark
  • a) What mass of sodium azide is needed to inflate a 65.0 L bag at 25 °C under 101.3 kPa?
  • b) Methane is burned according to CH4+2 O2→CO2+2 H2OCH_{4}+2\,O_{2}\rightarrow CO_{2}+2\,H_{2}O. At 150 °C and under constant pressure, what volumes of oxygen gas and carbon dioxide correspond to 10.0 L of methane? Does the total volume of the system change?
  • c) Now 0.100 mol of methane and 0.300 mol of oxygen gas are introduced into a RIGID 2.00 L container brought to 150 °C, and ignited. Calculate the pressure before the reaction, then the pressure after complete reaction and return to 150 °C. Comment.
  • d) Give the partial pressures of each species after the reaction. The container is then cooled to 25 °C, a temperature at which water condenses and its vapour pressure is 3.2 kPa. Calculate the new total pressure and explain the size of the drop.

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  • a) n(N2)=2.658n(N_{2})=2.658 mol, M=65.02M=65.02 g/mol, that is 115 g of azide
  • b) 20.0 L of oxygen gas, 10.0 L of carbon dioxide; the total volume stays 30.0 L
  • c) 703 kPa before AND after: the number of moles of gas is conserved
  • d) 176, 176 and 352 kPa; at 25 °C, only 251 kPa, a drop by a factor of 2.8
a)

The bag contains nitrogen gas: n(N2)=PVRT=101.3×65.08.314×298=2.658n\left(N_{2}\right)=\dfrac{PV}{RT}=\dfrac{101.3\times 65.0}{8.314\times 298}=2.658 mol. The equation gives 3 mol of N2N_{2} for 2 mol of NaN3NaN_{3}, so n(NaN3)=23×2.658=1.772n\left(NaN_{3}\right)=\dfrac{2}{3}\times 2.658=1.772 mol. With M(NaN3)=22.99+3(14.01)=65.02M\left(NaN_{3}\right)=22.99+3(14.01)=65.02 g/mol, the mass is 1.772×65.02=1151.772\times 65.02=115 g. The order of magnitude is right: a real airbag contains about a hundred grams of azide.

b)

At constant temperature and pressure, gas volumes are proportional to amounts of substance: the coefficients of the equation can be read directly as volumes. For 10.0 L of methane we therefore need 20.0 L of oxygen gas, and 10.0 L of carbon dioxide and 20.0 L of water vapour form, since at 150 °C water remains a gas. The total volume goes from 10.0+20.0=30.010.0+20.0=30.0 L (methane and oxygen) to 10.0+20.0=30.010.0+20.0=30.0 L (carbon dioxide and water vapour): it does not change. This is no coincidence: the sum of the gaseous coefficients is 3 on both sides of the equation.

c)

Before the reaction, ntotal=0.100+0.300=0.400n_{\text{total}}=0.100+0.300=0.400 mol and T=150+273=423T=150+273=423 K, so P=nRTV=0.400×8.314×4232.00=703P=\dfrac{nRT}{V}=\dfrac{0.400\times 8.314\times 423}{2.00}=703 kPa. The limiting reactant is methane: 0.1001=0.100\dfrac{0.100}{1}=0.100 against 0.3002=0.150\dfrac{0.300}{2}=0.150 for oxygen gas. The reaction consumes 0.100 mol of CH4CH_{4} and 0.200 mol of O2O_{2}, and produces 0.100 mol of CO2CO_{2} and 0.200 mol of H2OH_{2}O. After the reaction, 0.300−0.200=0.1000.300-0.200=0.100 mol of oxygen gas remains, plus 0.100 mol of CO2CO_{2} and 0.200 mol of water vapour, that is ntotal=0.400n_{\text{total}}=0.400 mol: exactly the same total as before. The pressure is therefore UNCHANGED, 703 kPa. This is the counterintuitive result of the exercise: a violent combustion can take place in a rigid container without changing the pressure once the temperature is back to its initial value, simply because the number of moles of gas is conserved, as b) already showed.

d)

The partial pressures are calculated from the mole fractions: P(O2)=0.1000.400×703=176P\left(O_{2}\right)=\dfrac{0.100}{0.400}\times 703=176 kPa, P(CO2)=176P\left(CO_{2}\right)=176 kPa and P(H2O)=0.2000.400×703=352P\left(H_{2}O\right)=\dfrac{0.200}{0.400}\times 703=352 kPa. At 25 °C, water vapour condenses almost entirely: only 3.2 kPa of vapour remains in the gas phase, the saturation value. The permanent gases, for their part, remain at 0.100+0.100=0.2000.100+0.100=0.200 mol and give P=0.200×8.314×2982.00=248P=\dfrac{0.200\times 8.314\times 298}{2.00}=248 kPa. The total pressure is therefore 248+3.2=251248+3.2=251 kPa, against 703 kPa before cooling. The drop by a factor of 2.8 combines two causes that must be told apart: the cooling from 423 K to 298 K accounts for a factor of 423298=1.42\dfrac{423}{298}=1.42, and the disappearance of half of the gas moles by condensation accounts for a factor of 2. The product 1.42×2=2.841.42\times 2=2.84 does give back the observed ratio. It is the same principle as the tin can that crumples as it cools, and as the vapour pressure correction of exercise 2.

before:0.400 mol, P = 703 kPaafter, at 150 °C:0.400 mol, P = 703 kPaCH₄O₂CO₂H₂O

Exercise 8: The Maxwell-Boltzmann distribution and atmospheric escape

At a given temperature, the molecules of a gas do not all have the same speed: they are spread out according to the Maxwell-Boltzmann distribution, an asymmetric bell-shaped curve whose tail extends toward high speeds. Three speeds characterize it: the most probable speed vp=2RTMv_{p}=\sqrt{\dfrac{2RT}{M}}, the average speed vavg=8RTπMv_{avg}=\sqrt{\dfrac{8RT}{\pi M}} and the root-mean-square speed vrms=3RTMv_{rms}=\sqrt{\dfrac{3RT}{M}}.

R=8.314R=8.314 J/(mol·K), MM in kg/mol. Molar masses: N2N_{2} 28.02 g/mol; H2H_{2} 2.016 g/mol. Escape speed of the Earth: 1.12×1041.12\times 10^{4} m/s; of the Moon: 2.38×1032.38\times 10^{3} m/s.

The curve below gives the speed distribution of nitrogen gas at 25 °C.

20040060080010001200140016000.511.522.5N₂, 25 °Cv (m/s)f(v) (10⁻³ s/m)
  • a) Calculate the three characteristic speeds of nitrogen gas at 25 °C. Show that their order and their ratios depend neither on the gas nor on the temperature.
  • b) Describe how the curve changes when nitrogen gas is taken from 25 °C to 1000 °C, then when nitrogen gas is replaced by hydrogen gas at 25 °C. Support each statement with a calculation of vrmsv_{rms}, and say what stays invariant in both cases.
  • c) The upper atmosphere is at about 1000 K. Calculate vrmsv_{rms} of hydrogen gas and of nitrogen gas at this temperature, then the ratio vescvrms\dfrac{v_{esc}}{v_{rms}} for each. Given that a celestial body durably retains a gas when this ratio exceeds about 6, explain why the Earth's atmosphere contains nitrogen gas but almost no hydrogen gas. Then treat the case of the Moon.
  • d) A glass of water left on a table eventually evaporates completely, although it is at 20 °C and not at 100 °C. Explain using the distribution, then say why it is the tail of the curve, and not its average value, that governs evaporation as well as atmospheric escape.

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  • a) vp=421v_{p}=421, vavg=475v_{avg}=475, vrms=515v_{rms}=515 m/s; ratios 1.128 and 1.225, constant
  • b) 1065 m/s at 1273 K and 1920 m/s for H2H_{2}; the area under the curve stays 1
  • c) 3517 and 943 m/s; ratios 3.18 and 11.9: the Earth keeps N2N_{2}, not H2H_{2}
  • d) It is the tail, not the average, that governs evaporation and escape
a)

With M=28.02×10−3M=28.02\times 10^{-3} kg/mol and T=298T=298 K: vp=2×8.314×2980.02802=421v_{p}=\sqrt{\dfrac{2\times 8.314\times 298}{0.02802}}=421 m/s; vavg=8×8.314×298π×0.02802=475v_{avg}=\sqrt{\dfrac{8\times 8.314\times 298}{\pi\times 0.02802}}=475 m/s; vrms=3×8.314×2980.02802=515v_{rms}=\sqrt{\dfrac{3\times 8.314\times 298}{0.02802}}=515 m/s. We always have vp<vavg<vrmsv_{p}<v_{avg}<v_{rms}, and the ratios are vavgvp=82π=1.128\dfrac{v_{avg}}{v_{p}}=\sqrt{\dfrac{8}{2\pi}}=1.128 and vrmsvp=32=1.225\dfrac{v_{rms}}{v_{p}}=\sqrt{\dfrac{3}{2}}=1.225. These ratios are numerical constants: the factor RT/M\sqrt{RT/M} is common to the three expressions and disappears in the ratios. The order is explained by the asymmetry of the curve, whose long tail toward high speeds pulls the average above the peak, and pulls the root mean square even harder since it weights the speeds by their square.

b)

Heating from 298 K to 1273 K: vrmsv_{rms} goes from 515 to 3×8.314×12730.02802=1065\sqrt{\dfrac{3\times 8.314\times 1273}{0.02802}}=1065 m/s, a factor of 1273298=2.07\sqrt{\dfrac{1273}{298}}=2.07. The peak of the curve moves to the right, the curve flattens and widens considerably, and the tail toward high speeds thickens a great deal. Replacing with hydrogen gas at 298 K: vrms=3×8.314×2980.002016=1920v_{rms}=\sqrt{\dfrac{3\times 8.314\times 298}{0.002016}}=1920 m/s, almost four times as fast, in agreement with 28.022.016=3.73\sqrt{\dfrac{28.02}{2.016}}=3.73. Here again the maximum moves to the right and the curve spreads out. What stays invariant in both cases is the area under the curve, which is always 1: it represents all of the molecules. A curve that widens must therefore necessarily come down, which is the key to reading all these figures.

c)

At 1000 K: vrms(H2)=3×8.314×10000.002016=3517v_{rms}\left(H_{2}\right)=\sqrt{\dfrac{3\times 8.314\times 1000}{0.002016}}=3517 m/s and vrms(N2)=3×8.314×10000.02802=943v_{rms}\left(N_{2}\right)=\sqrt{\dfrac{3\times 8.314\times 1000}{0.02802}}=943 m/s. The ratios are 11,2003517=3.18\dfrac{11{,}200}{3517}=3.18 for hydrogen gas and 11,200943=11.9\dfrac{11{,}200}{943}=11.9 for nitrogen gas. Nitrogen gas is well above the threshold of 6: the Earth retains it without difficulty. Hydrogen gas is at 3.2, well below: a non-negligible fraction of its molecules is constantly exceeding the escape speed, and it escapes. This is why hydrogen gas, although the most abundant element in the universe, is almost absent from our atmosphere, as is helium. For the Moon, 2380943=2.52\dfrac{2380}{943}=2.52 for nitrogen gas itself: even heavy gases are below the threshold, which explains why it has no atmosphere. The retention criterion therefore combines the gravity of the body and the molar mass of the gas.

d)

In a glass at 20 °C, the average speed of the water molecules is far below the one that would correspond to boiling, but the distribution is not a single value: its tail contains, at every instant, a small fraction of molecules fast enough to overcome the cohesive forces of the liquid and escape from the surface. These molecules leave, the slower ones stay, and the liquid would cool down if it were not warmed by the table and the air, which immediately regenerates a new tail. The glass therefore ends up emptying completely, just more slowly than at 100 °C, where the whole mass of the liquid can vaporize. The lesson shared with c) is that these two phenomena are governed neither by vpv_{p}, nor by vavgv_{avg}, nor by vrmsv_{rms}, but by the fraction of molecules lying beyond a threshold. This fraction varies extremely sensitively with temperature: a slight warming thickens the tail far more than it moves the peak. It is the same reasoning that will explain, in chemical kinetics, why a rise of 10 °C can double a reaction rate.

50010001500200025003000350040000.511.522.5N₂, 25 °CN₂, 1000 °CH₂, 25 °C (dashed)v (m/s)f(v) (10⁻³ s/m)

Exercise 9: The compressibility factor and the Boyle temperature

The compressibility factor measures the deviation from the ideal gas with a single number: Z=PVnRTZ=\dfrac{PV}{nRT}. It equals exactly 1 for an ideal gas, whatever the conditions. For a real gas, it departs from 1, and the direction of the departure says which imperfection dominates.

Take again the carbon dioxide of exercise 5, with a=364a=364 kPa·L²/mol² and b=0.0427b=0.0427 L/mol, at 300 K and for n=1.00n=1.00 mol. R=8.314R=8.314 kPa·L/(mol·K).

The diagram below shows the sample being compressed.

1.00 mol of CO₂T = 300 KV = 5.00 L; 0.500 L;0.100 L; 0.0600 L
  • a) Using the van der Waals equation, calculate the pressure and then the compressibility factor of carbon dioxide for a volume of 5.00 L, then 0.500 L, then 0.100 L, then 0.0600 L.
  • b) Describe the shape of ZZ as a function of compression and identify, in each regime, which of the two van der Waals correction terms prevails. What does Z<1Z<1 mean physically? And Z>1Z>1?
  • c) Show that at low pressures the van der Waals equation leads to Z≈1+1RT(b−aRT)PZ\approx 1+\dfrac{1}{RT}\left(b-\dfrac{a}{RT}\right)P. Deduce the temperature, called the Boyle temperature, at which a real gas behaves like an ideal gas at low pressures, and calculate it for carbon dioxide.
  • d) The measured Boyle temperature of carbon dioxide is about 715 K, whereas your calculation gives more. Does this disagreement invalidate the model? Justify by recalling what van der Waals assumes, and say what the model still predicts correctly.

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  • a) Z=0.979Z=0.979; 0.8010.801; 0.2860.286; 1.0361.036
  • b) ZZ drops below 1 (attractions), goes through a minimum, then exceeds 1 (molecular volume)
  • c) TB=aRb=1025T_{B}=\dfrac{a}{Rb}=1025 K for carbon dioxide
  • d) The model gives the right qualitative behaviours with two parameters, not the fine values
a)

We apply P=nRTV−nb−an2V2P=\dfrac{nRT}{V-nb}-\dfrac{an^{2}}{V^{2}} then Z=PVnRTZ=\dfrac{PV}{nRT} with nRT=8.314×300=2494nRT=8.314\times 300=2494 kPa·L. For V=5.00V=5.00 L: P=24944.957−36425.0=503.1−14.6=488.6P=\dfrac{2494}{4.957}-\dfrac{364}{25.0}=503.1-14.6=488.6 kPa, so Z=488.6×5.002494=0.979Z=\dfrac{488.6\times 5.00}{2494}=0.979. For V=0.500V=0.500 L: P=24940.4573−3640.250=5454−1456=3998P=\dfrac{2494}{0.4573}-\dfrac{364}{0.250}=5454-1456=3998 kPa, so Z=3998×0.5002494=0.801Z=\dfrac{3998\times 0.500}{2494}=0.801. For V=0.100V=0.100 L: P=24940.0573−3640.0100=43,530−36,400=7129P=\dfrac{2494}{0.0573}-\dfrac{364}{0.0100}=43{,}530-36{,}400=7129 kPa, so Z=7129×0.1002494=0.286Z=\dfrac{7129\times 0.100}{2494}=0.286. For V=0.0600V=0.0600 L: P=24940.0173−3640.00360=144,173−101,111=43,062P=\dfrac{2494}{0.0173}-\dfrac{364}{0.00360}=144{,}173-101{,}111=43{,}062 kPa, so Z=43,062×0.06002494=1.04Z=\dfrac{43{,}062\times 0.0600}{2494}=1.04.

b)

Starting from the largest volume, ZZ is almost 1, then it decreases clearly below 1 as the gas is compressed, goes through a minimum, then rises sharply and ends up exceeding 1. In the first regime, the attractive correction an2V2\dfrac{an^{2}}{V^{2}}, which varies as 1V2\dfrac{1}{V^{2}}, grows faster than the molecular volume correction, which only enters through nbV\dfrac{nb}{V}: the attractions dominate. A Z<1Z<1 then means that the gas is MORE compressible than an ideal gas, because the molecules attract each other and take up less room than expected. In the second regime, the available volume V−nbV-nb tends to zero and the repulsive term blows up: the volume of the molecules themselves dominates, the gas becomes LESS compressible than an ideal gas, and Z>1Z>1. Condensed matter cannot be compressed indefinitely. The minimum marks the point where the two effects exactly compensate.

c)

We write Z=PVRTZ=\dfrac{PV}{RT} for one mole with P=RTV−b−aV2P=\dfrac{RT}{V-b}-\dfrac{a}{V^{2}}, that is Z=VV−b−aRTV=11−bV−aRTVZ=\dfrac{V}{V-b}-\dfrac{a}{RTV}=\dfrac{1}{1-\frac{b}{V}}-\dfrac{a}{RTV}. At large volumes, 11−bV≈1+bV\dfrac{1}{1-\frac{b}{V}}\approx 1+\dfrac{b}{V}, hence Z≈1+1V(b−aRT)Z\approx 1+\dfrac{1}{V}\left(b-\dfrac{a}{RT}\right). Since 1V≈PRT\dfrac{1}{V}\approx\dfrac{P}{RT} to this order, we do get Z≈1+1RT(b−aRT)PZ\approx 1+\dfrac{1}{RT}\left(b-\dfrac{a}{RT}\right)P. The coefficient of PP vanishes when b=aRTb=\dfrac{a}{RT}, that is at the Boyle temperature TB=aRbT_{B}=\dfrac{a}{Rb}. For carbon dioxide: TB=3648.314×0.0427=1025T_{B}=\dfrac{364}{8.314\times 0.0427}=1025 K. Below this temperature, the coefficient is negative and ZZ starts by dropping below 1: this is just what we observed in a) at 300 K. Above it, the gas is already in the regime where the molecular volume prevails and ZZ increases from low pressures on.

d)

The disagreement is real: the order of magnitude is right but the model overestimates by about 40%. This does not invalidate van der Waals, it delimits its scope. The equation only corrects the ideal gas law with two fitted constants: bb assumes spherical, incompressible molecules, and aa sums up all the attractions in a single average term, independent of distance and temperature, which is very crude for a molecule like carbon dioxide. A two-parameter equation cannot reproduce quantitatively a property as fine as a compensation temperature. What the model does predict correctly, on the other hand, is essential: the existence of a minimum of ZZ, the fact that the attractive regime comes before the repulsive regime, the very existence of a Boyle temperature, liquefaction and the critical point, and the return to the ideal gas at low pressure and high temperature. It is the mark of a good physical model to give the right qualitative behaviours with two parameters, while leaving the precise numerical values to empirical equations of state.

246810121416180.511.52ideal gas: Z = 1Z = 0.286 for 0.100 Lattractions: Z < 1molecular volume: Z > 1n/V (mol/L)Z

Exercise 10: Problem: scuba diving and Dalton's law

Under water, the pressure increases by about 1 atmosphere every 10 metres. The partial pressures of the gases breathed increase accordingly, and two of them become dangerous well before the diver notices.

Air contains 21.0% of O2O_{2} and 79.0% of N2N_{2} by moles. Take Patm=101.3P_{atm}=101.3 kPa at the surface, and the total pressure at depth dd is P=101.3(1+d10)P=101.3\left(1+\dfrac{d}{10}\right) with dd in metres. The toxicity threshold of oxygen is set at a partial pressure of 160 kPa.

The diagram below shows the situation.

0 m10 m20 m30 m40 m50 msurface: 101.3 kPadiver at 30.0 mair breathed:21.0% O₂79.0% N₂
  • a) Calculate the total pressure and the partial pressure of O2O_{2} for a diver at 30.0 m.
  • b) At what depth, when breathing air, is the oxygen toxicity threshold reached?
  • c) Nitrox 32 contains 32.0% of O2O_{2}. Redo the calculation of b for this mixture.
  • d) Nitrox is presented as “safer” than air. Does your result contradict this claim? Explain what Nitrox really improves.
  • e) For very deep dives, nitrogen is replaced by helium. Give one advantage related to this chapter and one practical drawback.

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  • a) P=405.2P=405.2 kPa and P(O2)=85.1P(O_{2})=85.1 kPa, well under the threshold
  • b) d=65.2d=65.2 m
  • c) d=39.4d=39.4 m, MUCH shallower than with air
  • d) Nitrox protects against nitrogen, not oxygen: longer, but shallower
  • e) Helium eliminates narcosis but chills, distorts the voice and leaks by effusion
a)

At 30.0 m: P=101.3(1+30.010)=101.3×4.00=405.2P=101.3\left(1+\dfrac{30.0}{10}\right)=101.3\times 4.00=405.2 kPa, that is 4 atmospheres. The partial pressure of oxygen is P(O2)=0.210×405.2=85.1P\left(O_{2}\right)=0.210\times 405.2=85.1 kPa. This is still far from 160 kPa: recreational diving at 30 m is safe from this point of view.

b)

We look for dd such that 0.210×101.3(1+d10)=1600.210\times 101.3\left(1+\dfrac{d}{10}\right)=160. Then 1+d10=1600.210×101.3=16021.27=7.521+\dfrac{d}{10}=\dfrac{160}{0.210\times 101.3}=\dfrac{160}{21.27}=7.52, so d10=6.52\dfrac{d}{10}=6.52 and d=65.2d=65.2 m. This is well beyond the limit of recreational diving, which is set at 40 m for other reasons.

c)

With 32.0%: 1+d10=1600.320×101.3=16032.42=4.941+\dfrac{d}{10}=\dfrac{160}{0.320\times 101.3}=\dfrac{160}{32.42}=4.94, so d=39.4d=39.4 m. The maximum depth is therefore MUCH SHALLOWER than with ordinary air: 39 m instead of 65 m.

d)

No, there is no contradiction, but the claim needs a qualification. Nitrox is safer with respect to NITROGEN, not oxygen. By replacing part of the N2N_{2} with O2O_{2}, the partial pressure of nitrogen is lowered at every depth, which reduces the amount of nitrogen dissolved in the tissues, hence the risk of decompression sickness and narcosis. In return, the partial pressure of oxygen is raised, and therefore the risk of toxicity, which IMPOSES a shallower maximum depth. Nitrox thus lets you stay longer, but not as deep: it is a shift of risk, not an elimination.

e)

Advantage: helium is chemically inert and above all far less soluble in fatty tissues than nitrogen, which eliminates narcosis and reduces the load of dissolved gas. Practical drawback related to this chapter: its very low molar mass, 4.003 g/mol, gives it a high thermal conductivity and a molecular speed about 2.6 times that of nitrogen, which chills the diver considerably and distorts the voice. On top of that comes its cost, and the fact that it escapes from cylinders by effusion faster than any other gas, exactly as in the balloon of exercise 4.

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