4.E: UHV and Effects of Gas Pressure (Exercises)
- Page ID
- 25380
\( \newcommand{\vecs}[1]{\overset { \scriptstyle \rightharpoonup} {\mathbf{#1}} } \)
\( \newcommand{\vecd}[1]{\overset{-\!-\!\rightharpoonup}{\vphantom{a}\smash {#1}}} \)
\( \newcommand{\dsum}{\displaystyle\sum\limits} \)
\( \newcommand{\dint}{\displaystyle\int\limits} \)
\( \newcommand{\dlim}{\displaystyle\lim\limits} \)
\( \newcommand{\id}{\mathrm{id}}\) \( \newcommand{\Span}{\mathrm{span}}\)
( \newcommand{\kernel}{\mathrm{null}\,}\) \( \newcommand{\range}{\mathrm{range}\,}\)
\( \newcommand{\RealPart}{\mathrm{Re}}\) \( \newcommand{\ImaginaryPart}{\mathrm{Im}}\)
\( \newcommand{\Argument}{\mathrm{Arg}}\) \( \newcommand{\norm}[1]{\| #1 \|}\)
\( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\)
\( \newcommand{\Span}{\mathrm{span}}\)
\( \newcommand{\id}{\mathrm{id}}\)
\( \newcommand{\Span}{\mathrm{span}}\)
\( \newcommand{\kernel}{\mathrm{null}\,}\)
\( \newcommand{\range}{\mathrm{range}\,}\)
\( \newcommand{\RealPart}{\mathrm{Re}}\)
\( \newcommand{\ImaginaryPart}{\mathrm{Im}}\)
\( \newcommand{\Argument}{\mathrm{Arg}}\)
\( \newcommand{\norm}[1]{\| #1 \|}\)
\( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\)
\( \newcommand{\Span}{\mathrm{span}}\) \( \newcommand{\AA}{\unicode[.8,0]{x212B}}\)
\( \newcommand{\vectorA}[1]{\vec{#1}} % arrow\)
\( \newcommand{\vectorAt}[1]{\vec{\text{#1}}} % arrow\)
\( \newcommand{\vectorB}[1]{\overset { \scriptstyle \rightharpoonup} {\mathbf{#1}} } \)
\( \newcommand{\vectorC}[1]{\textbf{#1}} \)
\( \newcommand{\vectorD}[1]{\overrightarrow{#1}} \)
\( \newcommand{\vectorDt}[1]{\overrightarrow{\text{#1}}} \)
\( \newcommand{\vectE}[1]{\overset{-\!-\!\rightharpoonup}{\vphantom{a}\smash{\mathbf {#1}}}} \)
\( \newcommand{\vecs}[1]{\overset { \scriptstyle \rightharpoonup} {\mathbf{#1}} } \)
\(\newcommand{\longvect}{\overrightarrow}\)
\( \newcommand{\vecd}[1]{\overset{-\!-\!\rightharpoonup}{\vphantom{a}\smash {#1}}} \)
\(\newcommand{\avec}{\mathbf a}\) \(\newcommand{\bvec}{\mathbf b}\) \(\newcommand{\cvec}{\mathbf c}\) \(\newcommand{\dvec}{\mathbf d}\) \(\newcommand{\dtil}{\widetilde{\mathbf d}}\) \(\newcommand{\evec}{\mathbf e}\) \(\newcommand{\fvec}{\mathbf f}\) \(\newcommand{\nvec}{\mathbf n}\) \(\newcommand{\pvec}{\mathbf p}\) \(\newcommand{\qvec}{\mathbf q}\) \(\newcommand{\svec}{\mathbf s}\) \(\newcommand{\tvec}{\mathbf t}\) \(\newcommand{\uvec}{\mathbf u}\) \(\newcommand{\vvec}{\mathbf v}\) \(\newcommand{\wvec}{\mathbf w}\) \(\newcommand{\xvec}{\mathbf x}\) \(\newcommand{\yvec}{\mathbf y}\) \(\newcommand{\zvec}{\mathbf z}\) \(\newcommand{\rvec}{\mathbf r}\) \(\newcommand{\mvec}{\mathbf m}\) \(\newcommand{\zerovec}{\mathbf 0}\) \(\newcommand{\onevec}{\mathbf 1}\) \(\newcommand{\real}{\mathbb R}\) \(\newcommand{\twovec}[2]{\left[\begin{array}{r}#1 \\ #2 \end{array}\right]}\) \(\newcommand{\ctwovec}[2]{\left[\begin{array}{c}#1 \\ #2 \end{array}\right]}\) \(\newcommand{\threevec}[3]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \end{array}\right]}\) \(\newcommand{\cthreevec}[3]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \end{array}\right]}\) \(\newcommand{\fourvec}[4]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \\ #4 \end{array}\right]}\) \(\newcommand{\cfourvec}[4]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \\ #4 \end{array}\right]}\) \(\newcommand{\fivevec}[5]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \\ #4 \\ #5 \\ \end{array}\right]}\) \(\newcommand{\cfivevec}[5]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \\ #4 \\ #5 \\ \end{array}\right]}\) \(\newcommand{\mattwo}[4]{\left[\begin{array}{rr}#1 \amp #2 \\ #3 \amp #4 \\ \end{array}\right]}\) \(\newcommand{\laspan}[1]{\text{Span}\{#1\}}\) \(\newcommand{\bcal}{\cal B}\) \(\newcommand{\ccal}{\cal C}\) \(\newcommand{\scal}{\cal S}\) \(\newcommand{\wcal}{\cal W}\) \(\newcommand{\ecal}{\cal E}\) \(\newcommand{\coords}[2]{\left\{#1\right\}_{#2}}\) \(\newcommand{\gray}[1]{\color{gray}{#1}}\) \(\newcommand{\lgray}[1]{\color{lightgray}{#1}}\) \(\newcommand{\rank}{\operatorname{rank}}\) \(\newcommand{\row}{\text{Row}}\) \(\newcommand{\col}{\text{Col}}\) \(\renewcommand{\row}{\text{Row}}\) \(\newcommand{\nul}{\text{Nul}}\) \(\newcommand{\var}{\text{Var}}\) \(\newcommand{\corr}{\text{corr}}\) \(\newcommand{\len}[1]{\left|#1\right|}\) \(\newcommand{\bbar}{\overline{\bvec}}\) \(\newcommand{\bhat}{\widehat{\bvec}}\) \(\newcommand{\bperp}{\bvec^\perp}\) \(\newcommand{\xhat}{\widehat{\xvec}}\) \(\newcommand{\vhat}{\widehat{\vvec}}\) \(\newcommand{\uhat}{\widehat{\uvec}}\) \(\newcommand{\what}{\widehat{\wvec}}\) \(\newcommand{\Sighat}{\widehat{\Sigma}}\) \(\newcommand{\lt}{<}\) \(\newcommand{\gt}{>}\) \(\newcommand{\amp}{&}\) \(\definecolor{fillinmathshade}{gray}{0.9}\)This section provides a limited number of examples of the application of the formulae given in the previous section to determine the:
- Density of Molecules in the Gas Phase
- Mean Free Path of Molecules in the Gas Phase
- Flux of Molecules incident upon a Surface
- Rate of Adsorption of Molecules and Surface Coverages
If you have not already been through Section 4.2 then I would suggest that you stop now and return to this page only after you have done so !
Within any one of the following sub-sections, it will be assumed that you have already done the previous questions and may make use of the answers from these questions - you are therefore advised to work through the questions in the order they are presented.
A. Molecular Gas Densities
Calculate the molecular gas density for an ideal gas at 300 K, under the following conditions (giving your answer in molecules m-3 ): At a pressure of 10-6 Torr
Solution
The molecular gas density at this pressure is 3.2 x 1016 molecules m-3
Rationale
The gas density is easily obtained from the ideal gas law :
\[n = \dfrac{N}{V} = \dfrac{P}{k\,T} \nonumber \] [ molecules. m-3 ]
| where : | P - pressure [ N m-2 ] |
| k - Boltzmann's constant ( = 1.38 x 10-23 J K-1 ) | |
| T - temperature [ K ] |
Hence,
P = ( 1 x 10-6 / 760 ) x 101325 = 1.333 x 10-4 N m-2
n = 1.333 x 10-4 / (1.38x10-23 x 300 ) = 3.2 x 1016 molecules m-3
Calculate the molecular gas density for an ideal gas at 300 K, under the following conditions (giving your answer in molecules m-3 ): At a pressure of 10-9 Torr
Solution
The molecular gas density at this pressure is 3.2 x 1013 molecules m-3
Rationale
The gas density is directly proportional to the pressure , hence when the pressure of the gas is reduced by 3 decades from 10-6 Torr (as in the previous question) to 10-9 Torr, the gas density will also be lowered by a factor of 1000.
i.e. n = 3.2 x 1016 / 1000 = 3.2 x 1013 molecules m-3
B. Mean Free Path of Molecules in the Gas Phase
Calculate the mean free path of CO molecules in a vessel at the indicated pressure and temperature, using a value for the collision cross section of CO of 0.42 nm2.
P = 10-4 Torr, at 300 K
Solution
The mean free path of CO under these conditions is 0.52 m
Rationale
The mean free path, , is given by the equation :
\(\lambda=\frac{k T}{1.414 P \sigma}\)[ m ]
where, in this instance,
P = (1 x 10-4 / 760) x 101325 = 1.333 x 10-2 N m-2
and
σ = 0.42 nm2 = 4.2 x 10-19 m2
Substitution gives
λ = ( 1.38x10-23 x 300 ) / (1.414 x 1.33x10-2 x 4.2x10-19 )
⇒ λ = 0.52 m
Calculate the mean free path of CO molecules in a vessel at the indicated pressure and temperature, using a value for the collision cross section of CO of 0.42 nm2.
P = 10-9 Torr, at 300 K
Solution
The mean free path of CO under these new conditions is 52000 m ( = 5.2 x 104 m)
Rationale
The mean free path of molecules in the gas phase is inversely proportional to the pressure , hence when the pressure of the gas is reduced by 5 decades from 10-4 Torr to 10-9 Torr, the mean free path will increase by a factor of 100000.
i.e. λ = 0.52 x 100000 = 5.2 x 104 m
C. Fluxes of Molecules Incident upon a Surface
Calculate the flux of molecules incident upon a solid surface under the following conditions:
[Note - 1 u = 1.66 x 10-27 kg: atomic masses ; m(O) =16.0 u, m(H) = 1.0 u]
- Oxygen gas ( P = 1 Torr ) at 300 K
Solution
The flux of oxygen molecules under these conditions is 3.58 x 1024 molecules m-2 s-1
Rationale
The incident flux is given by the following equation (with all quantities expressed in SI units).
\[F=\frac{P}{\sqrt{2 \pi m k T}} \nonumber \][ molecules m-2 s-1 ]
In this instance ,
P = (1/760) x 101325 = 133.3 N m-2
and
m = 32 x 1.66x10-27 = 5.32x10-26 kg
so
F = 133.3 / (2 x 3.1416 x 5.32x10-26 x 1.38x10-23 x 300 )1/2
i.e. F = 3.58 x 1024 molecules m-2 s-1
Calculate the flux of molecules incident upon a solid surface under the following conditions:
[Note - 1 u = 1.66 x 10-27 kg: atomic masses ; m(O) =16.0 u, m(H) = 1.0 u]
- Oxygen gas ( P = 10-6Torr ) at 300 K
Solution
The flux of oxygen molecules under these conditions is 3.58 x 1018 molecules m-2 s-1
Rationale
The flux is directly proportional to the pressure : consequently a decrease in pressure by 6 orders of magnitude (all other conditions remaining the same) leads to a corresponding decrease in the flux i.e.
F = 3.58x1024 x ( 10-6 / 1 )
⇒ F = 3.58 x 1018 molecules m-2 s-1
Calculate the flux of molecules incident upon a solid surface under the following conditions:
[Note - 1 u = 1.66 x 10-27 kg: atomic masses ; m(O) =16.0 u, m(H) = 1.0 u]
- Hydrogen gas ( P = 10-6Torr ) at 300 K
Solution
The flux of hydrogen molecules under these conditions is 1.43 x 1019 molecules m-2 s-1
Rationale
The flux is inversely proportional to the square root of the mass of the incident gas species - hence, using the answer obtained for oxygen at this pressure as a starting point
F = 3.58x1018 x ( 32 / 2 )1/2
⇒ F = 1.43 x 1019 molecules m-2 s-1
Calculate the flux of molecules incident upon a solid surface under the following conditions:
[Note - 1 u = 1.66 x 10-27 kg: atomic masses ; m(O) =16.0 u, m(H) = 1.0 u]
- Hydrogen gas ( P = 10-6Torr ) at 1000 K
Solution
The flux of hydrogen molecules under these conditions is 7.83 x 1018 molecules m-2 s-1
Rationale
The flux is inversely proportional to the square root of the gas phase temperature - hence , by comparison with the previous result
F = 1.43 x 1019 x ( 300 / 1000 )1/2
⇒ F = 7.83 x 1018 molecules m-2 s-1
D. The Kinetically Limited Uptake of Molecules onto a Surface
The rate of adsorption of molecules onto a surface can be determined from the flux of molecules incident on the surface and the sticking probability pertaining at that instant in time (note that in general the sticking probability itself will be dependent upon a number of factors including the existing coverage of adsorbed species).
In the following examples we will assume that the surface is initially clean (i.e. the initial coverage is zero), and that there is no desorption of the molecules once they have adsorbed. You should determine coverages as the ratio of the adsorbate concentration to the density of surface substrate atoms (which you may assume to be 1019 m-2 ). In the first two questions we will assume that the sticking probability is constant over the coverage range concerned.
Calculate the surface coverage obtained after exposure to a pressure of 10-8 Torr of CO for 20 s at 300 K - you may take the sticking probability of CO on this surface to have a constant value of 0.9 up to the coverage concerned.
Solution
The surface coverage of CO molecules obtained is θ = 0.069
Rationale
Firstly we need to calculate the incident flux of CO using the Hertz-Knudsen formula : this gives
F = 3.83 x 1016 molecules m-2 s-1
Since the sticking probability is constant, the number of molecules per m2 is simply given by
| Coverage | = F x S x t |
| = 3.83 x 1016 x 0.9 x 20 | |
| = 6.90 x 1017 molecules m-2 |
which, when ratioed to the surface density of substrate atoms, gives
θ = 6.90x1017 / 1.0x1019 ⇒ θ = 0.069
Calculate the surface coverage of atomic nitrogen obtained by dissociative adsorption after exposure to a pressure of 10-8 Torr of nitrogen gas for 20 s at 300 K - you may take the dissociative sticking probability of molecular nitrogen on this surface to be constant and equal to 0.1
Solution
The surface coverage of N atoms obtained is θ = 0.015
Rationale
We can use the answer to the previous question to save some work here since the flux of incident molecules will be the same - the differences are that
- each nitrogen molecule that sticks gives rise to two adsorbed N atoms,
- the sticking probability is lower by a factor of 9
Hence,
Coverage , θ = 0.069 x (2/1) x (0.1/0.9) ⇒ θ = 0.015
In general, the sticking probability varies with coverage - most obviously, the sticking probability must tend to zero as the coverage approaches its saturation value. These calculations are not quite so easy !
Calculate the surface coverage obtained after exposure to a pressure of 10-8 Torr of CO for 200 s at 300 K - the sticking probability of CO in this case should be taken to vary linearly with coverage between a value of unity at zero coverage and a value of zero at saturation coverage (which you should take to be 6.5 x 1018 molecules m-2 ).
Solution
The surface coverage of CO molecules obtained is 4.5 x 1018 molecules m-2 or θ = 0.45
Rationale
We have calculated the incident flux, F , of CO under these conditions in a previous question; it is equal 3.83 x 1016 molecules m-2 s-1. We are also told that the maximum surface coverage, Nsat , is 6.5 x 1018 molecules m-2.
Let N(t) be the surface coverage in molecules m-2 at any time, t.
| Then | \(\frac{d N}{d t}=F \cdot S(N) \Rightarrow \int \frac{d N}{S(N)}=F \int d t\) |
| where | S(N) = ( 1 - ( N / Nsat ) ) |
If we use the Langmuir definition for the surface coverage, i.e. θ = ( N / Nsat ) ,
Then dθ = dN / Nsat and
\[N_{s a t} \frac{d \theta}{d t}=F . S(\theta) \quad \Rightarrow \quad \int \frac{d \theta}{S(\theta)}=\frac{F}{N_{s a t}} \int d t \nonumber \]
where S(θ) = ( 1 - θ ) .
To answer this question we need to integrate the differential equation from t = 0 to t = 200 s which gives
\[[-\ln (1-\theta)]_{\theta=0}^{\theta \operatorname{final}}=\frac{F}{N_{\text {sat }}}[t]_0^{200} \nonumber \]
⇒ θfinal = 0.692 (where θ is still defined in the Langmuir manner)
So, the absolute coverage of CO molecules is given by
⇒ Coverage = 0.692 x 6.5 x 1018 molecules m-2 = 4.5 x 1018 molecules m-2.
and the coverage defined in the standard surface science manner is obtained by ratioing with the atom density of substrate atoms in the first layer
⇒ θ = ( 4.5 x 1018 / 1.0 x 1019 ) = 0.450


