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Learning Objectives

By the end of this chapter, you should be able to:

Introduction

Chapters 13 dismantled the ether and rebuilt kinematics and dynamics on Einstein’s postulates, but light itself — a wave, according to Maxwell’s equations, which special relativity leaves intact — remained conceptually untouched. Chapters 45 then developed that wave picture in full quantitative detail: interference and diffraction, both direct, precise confirmations that light obeys a wave equation. This chapter takes up a second, independent crisis of classical physics, one concerning not the kinematics of light but its very nature. Four phenomena — blackbody radiation, the photoelectric effect, X-ray production, and Compton scattering — each show, in a different experimental setting, that electromagnetic radiation exchanges energy with matter not continuously, as a wave should, but in discrete packets. The concept that emerges, the photon, carries energy E=hfE = hf and momentum p=h/λp = h/\lambda, and behaves in each of these experiments like a particle, even though light indisputably also shows the wave behavior of Chapters 45 in other settings. A final phenomenon, pair production, shows that a photon’s energy can be converted entirely into matter, tying the particle nature of light directly to the mass–energy equivalence of Chapter 3. Reconciling these two faces of light is the beginning of quantum mechanics.

6.1Blackbody Radiation and Planck’s Hypothesis

Any object at temperature TT emits electromagnetic radiation across a continuous range of wavelengths, with an intensity distribution depending on TT. An idealized perfect absorber and emitter is called a blackbody; its emitted spectral distribution, the blackbody spectrum, depends only on temperature, not on the material. A good laboratory approximation is a small hole in the wall of an otherwise closed, heated cavity: radiation entering the hole is absorbed and re-emitted many times by the cavity walls before any of it can escape, so the radiation leaking out through the hole is, to excellent approximation, in thermal equilibrium with the cavity walls and independent of what the walls are made of.

The Ultraviolet Catastrophe

Late-nineteenth-century classical physics attempted to compute this spectrum by treating the electromagnetic field inside the cavity as a superposition of standing-wave modes, each behaving as an independent harmonic oscillator, and invoking the equipartition theorem — every such oscillator, in thermal equilibrium at temperature TT, should carry average energy kBTk_BT, independent of its frequency. Counting the number of standing-wave modes per unit volume in a wavelength interval dλd\lambda (a purely geometric problem, fixed by the cavity’s size) and multiplying by kBTk_BT per mode gives the Rayleigh–Jeans law,

u(λ,T)=8πkBTλ4,u(\lambda,T) = \frac{8\pi k_BT}{\lambda^4},

for the spectral energy density. This matches the observed spectrum reasonably well at long wavelength, but diverges as λ0\lambda \to 0: since the number of short-wavelength modes grows without bound and each is assigned the same energy kBTk_BT, the predicted radiated energy — obtained by integrating u(λ,T)u(\lambda,T) over all λ\lambda — is infinite. This absurd prediction, sharply contradicted by the observed spectrum (which rises from zero at short wavelength, peaks, and falls off at long wavelength), became known as the ultraviolet catastrophe: not a small discrepancy to be patched, but a qualitative failure of classical statistical mechanics applied to the electromagnetic field.

Figure 6.1 plots both curves against each other. Raising the temperature moves the peak and lifts the total area, as the next section’s displacement and Stefan–Boltzmann laws require; the classical curve, plotted alongside, runs off the top of the graph at short wavelength no matter what temperature is chosen.

Screenshot of the Blackbody Spectrum simulation

Figure 6.1:The blackbody spectrum as a function of temperature, with the Rayleigh–Jeans prediction available for comparison. The gap between the two at short wavelength is the ultraviolet catastrophe.

Interactive simulation: Blackbody Spectrum

Planck’s Quantization Hypothesis

Max Planck resolved this in 1900 by a hypothesis with no classical justification: the oscillators making up the cavity walls cannot exchange energy with the field continuously, but only in discrete multiples of a fundamental quantum,

En=nhf,n=0,1,2,,E_n = nhf, \qquad n = 0, 1, 2, \ldots,

where ff is the oscillator’s frequency and hh is a new fundamental constant (Planck’s constant), h=6.626×1034 Jsh = 6.626\times 10^{-34}\ \text{J}\cdot\text{s}. With this assumption, the average energy of a mode at frequency ff in thermal equilibrium at temperature TT is not kBTk_BT (the equipartition value, independent of ff, which causes the catastrophe) but

E=hfehf/kBT1,\langle E \rangle = \frac{hf}{e^{hf/k_BT} - 1},

which suppresses high-frequency (short-wavelength) modes because at high ff, hfkBThf \gg k_BT makes a single quantum too “expensive” to be thermally excited: the Boltzmann factor ehf/kBTe^{-hf/k_BT} governing how likely a mode is to hold even one quantum falls off exponentially, cutting off the ultraviolet divergence entirely. This leads to Planck’s radiation law for the spectral energy density,

u(λ,T)=8πhcλ51ehc/λkBT1,u(\lambda, T) = \frac{8\pi hc}{\lambda^5}\, \frac{1}{e^{hc/\lambda k_B T} - 1},

which matches the observed blackbody spectrum at all wavelengths and temperatures, and reduces to the Rayleigh–Jeans law in the limit hfkBThf \ll k_BT, i.e. at long wavelength, where ehf/kBT1hf/kBTe^{hf/k_BT}-1 \approx hf/k_BT and quantization effects become negligible — exactly the regime in which the classical calculation had already succeeded. Planck himself regarded the quantization of oscillator energy as a mathematical device rather than a physical claim about light. It was Einstein who, five years later, proposed taking it literally.

Wien’s Displacement Law and the Stefan–Boltzmann Law

Differentiating u(λ,T)u(\lambda,T) with respect to λ\lambda and setting the result to zero gives Wien’s displacement law for the wavelength of peak emission,

λmaxT=2.898×103 mK,\lambda_{\max} T = 2.898\times 10^{-3}\ \text{m}\cdot\text{K},

which is why hotter objects glow at shorter (bluer) wavelengths — from the deep red of a heating element to the blue-white of a hot star. Integrating u(λ,T)u(\lambda,T) over all wavelengths gives the total power radiated per unit surface area of an ideal blackbody, the Stefan–Boltzmann law,

PA=σT4,σ=5.670×108 Wm2K4,\frac{P}{A} = \sigma T^4, \qquad \sigma = 5.670\times 10^{-8}\ \text{W}\cdot\text{m}^{-2}\cdot\text{K}^{-4},

with σ\sigma the Stefan–Boltzmann constant. The steep T4T^4 dependence means that radiated power is extremely sensitive to temperature: doubling an object’s absolute temperature increases its radiated power per unit area sixteenfold. Real objects are not perfect blackbodies; a surface’s actual radiated power is P/A=εσT4P/A = \varepsilon\sigma T^4, where the emissivity ε1\varepsilon \le 1 measures how closely the surface approximates an ideal absorber and emitter (ε=1\varepsilon = 1 for a true blackbody).

Worked Example: The Sun as a Blackbody

The Sun’s surface (photosphere) has an effective temperature of T5778 KT \approx 5778\ \text{K} and radius R=6.96×108 mR_\odot = 6.96\times10^8\ \text{m}. Treating it as an ideal blackbody, Wien’s law gives the wavelength of peak emission,

λmax=2.898×103 mK5778 K=5.02×107 m=502 nm,\lambda_{\max} = \frac{2.898\times10^{-3}\ \text{m}\cdot\text{K}}{5778\ \text{K}} = 5.02\times10^{-7}\ \text{m} = 502\ \text{nm},

squarely in the green part of the visible spectrum — the Sun’s spectrum actually peaks near the middle of the range of wavelengths the human eye evolved to detect, though scattering in Earth’s atmosphere and the eye’s overall spectral response make sunlight appear white or yellow rather than green. The Stefan–Boltzmann law gives the power radiated per unit area, P/A=σT4=(5.670×108 Wm2K4)(5778 K)46.32×107 W/m2P/A = \sigma T^4 = (5.670\times10^{-8}\ \text{W}\cdot\text{m}^{-2}\cdot\text{K}^{-4})(5778\ \text{K})^4 \approx 6.32\times10^7\ \text{W/m}^2. Multiplying by the Sun’s surface area, A=4πR26.09×1018 m2A = 4\pi R_\odot^2 \approx 6.09\times10^{18}\ \text{m}^2, gives a total radiated power (luminosity)

P=PAA(6.32×107 W/m2)(6.09×1018 m2)3.85×1026 W,P = \frac{P}{A}\cdot A \approx (6.32\times10^7\ \text{W/m}^2)(6.09\times10^{18}\ \text{m}^2) \approx 3.85\times10^{26}\ \text{W},

in close agreement with the Sun’s independently measured luminosity of 3.828×1026 W3.828\times10^{26}\ \text{W} — the same figure used in Chapter 3, Problem 6 to estimate the Sun’s rate of mass loss via E=mc2E=mc^2. That two completely independent lines of physics (blackbody radiation here, and mass–energy equivalence there) connect so tightly to the same measured number is a testament to how well both theories describe the physical world.

Historical Context: Lenard’s Puzzle

Planck’s quantization hypothesis was aimed narrowly at the blackbody spectrum, and Planck himself did not initially believe that light itself came in discrete packets. Evidence pointing in that direction had, in fact, already been gathering independently. In 1902, three years before Einstein’s photon paper, Philipp Lenard studied the photoelectric effect using an arc lamp and a retarding-voltage apparatus much like the one described below, and found — to general puzzlement at the time — that the stopping voltage (and hence the photoelectrons’ maximum kinetic energy) did not increase with the lamp’s intensity, contrary to every expectation from Maxwell’s wave theory of light, in which a more intense wave carries proportionally more energy to whatever absorbs it. Lenard had no explanation; the result simply sat as an unresolved anomaly in the physics literature for three years, alongside blackbody radiation, until Einstein showed that both puzzles have the same root cause: light exchanges energy with matter in discrete quanta, not continuously.

6.2The Photoelectric Effect and X-Ray Production

The Photoelectric Effect

When light of sufficiently short wavelength strikes a metal surface, electrons are ejected — the photoelectric effect. A typical apparatus measures the photocurrent as a function of a retarding voltage VV applied between the emitting surface and a collector; the voltage at which the current just reaches zero, the stopping potential V0V_0, gives the maximum kinetic energy of the ejected electrons, Kmax=eV0K_{\max} = eV_0. Plotting the measured photocurrent against retarding voltage traces out a curve that falls smoothly to zero at V0V_0 rather than dropping abruptly, because the ejected electrons are emitted with a distribution of kinetic energies up to KmaxK_{\max}, not a single sharp value; V0V_0 marks where even the fastest electrons are turned back.

Three experimental features of this effect resist any explanation in terms of classical electromagnetic waves, in which energy is delivered continuously and is proportional to intensity:

  1. KmaxK_{\max} is independent of light intensity. Classically, a more intense wave delivers more energy per unit time to an electron and should eject electrons with more kinetic energy. Experimentally, increasing intensity increases the number of photoelectrons (the current) but not KmaxK_{\max}.

  2. KmaxK_{\max} depends linearly on frequency, and there exists a sharp threshold frequency f0f_0, characteristic of the metal, below which no photoelectrons are emitted at all, regardless of intensity or exposure time. Classically, a wave of any frequency should eventually eject electrons if given enough time to deliver sufficient energy, so a hard threshold — and one depending on frequency rather than intensity — has no classical explanation.

  3. Emission is (essentially) instantaneous, with no observable time lag even at very low intensity. Classically, a dim wave should take a measurable time to deliver enough energy to an electron to free it; a rough classical estimate for a very weak source predicts delays of minutes to hours, yet no such delay is ever observed.

Einstein resolved all three in 1905 by proposing that light itself is quantized: it consists of discrete packets, photons, each carrying energy

E=hf,E = hf,

with hh the same constant Planck introduced. In the photoelectric effect, a single photon transfers its entire energy to a single electron in one interaction. If ϕ\phi (the metal’s work function) is the minimum energy needed to remove an electron from the metal, conservation of energy gives

Kmax=hfϕ,K_{\max} = hf - \phi,

the photoelectric equation. This immediately explains all three observations: KmaxK_{\max} depends on ff (through the photon energy hfhf) but not on intensity, since intensity only changes the number of photons per second, not the energy of each one; the threshold frequency is f0=ϕ/hf_0 = \phi/h, below which a single photon simply does not carry enough energy to free an electron, no matter how many photons arrive; and emission is instantaneous because each electron absorbs one photon’s energy all at once, not gradually. A plot of KmaxK_{\max} (equivalently, eV0eV_0) versus ff is a straight line of slope hh and yy-intercept ϕ-\phi, and Millikan’s precise measurement of exactly this line (1916) provided both a direct experimental value of hh and strong confirmation of Einstein’s photon hypothesis — for which, not for relativity, Einstein received the 1921 Nobel Prize in Physics.

The three stubborn facts are best met in the order Lenard and Millikan met them, with the apparatus in front of you. In Figure 6.2 the light’s intensity, its wavelength, the target metal, and the retarding voltage are all under control, and the photocurrent and stopping potential are read off directly. Turn the intensity up at fixed wavelength: the current rises and the stopping potential does not move. Shorten the wavelength instead: the stopping potential climbs, and a plot of eV0eV_0 against ff — the simulation will accumulate one for you — is a straight line whose slope is hh and whose intercept names the metal. Cross the threshold from the long-wavelength side and the current stops altogether, at full intensity.

Screenshot of the Photoelectric Effect simulation

Figure 6.2:The photoelectric apparatus: a photocathode, an adjustable light source, and a retarding voltage. (This is one of PhET’s original Java simulations, run in the browser by CheerpJ; it downloads a Java runtime before it starts, so give it a few seconds on first load.)

Interactive simulation: Photoelectric Effect

Worked Example: The Photoelectric Effect in Cesium

Cesium has one of the lowest work functions of any metal, ϕ=2.14 eV\phi = 2.14\ \text{eV}, which is why it is used in the photocathodes of photomultiplier tubes and early photoelectric light meters.

Ultraviolet light of wavelength λ=250 nm\lambda = 250\ \text{nm} illuminates a cesium surface. Using the convenient combination hc=1240 eVnmhc = 1240\ \text{eV}\cdot\text{nm},

Ephoton=hcλ=1240 eVnm250 nm=4.96 eV.E_{\text{photon}} = \frac{hc}{\lambda} = \frac{1240\ \text{eV}\cdot\text{nm}}{250\ \text{nm}} = 4.96\ \text{eV}.

The maximum kinetic energy of the photoelectrons is Kmax=Ephotonϕ=4.96 eV2.14 eV=2.82 eVK_{\max} = E_{\text{photon}} - \phi = 4.96\ \text{eV} - 2.14\ \text{eV} = 2.82\ \text{eV}, so the stopping potential is V0=2.82 VV_0 = 2.82\ \text{V}. The threshold wavelength — the longest wavelength that can still eject an electron — follows from ϕ=hc/λ0\phi = hc/\lambda_0:

λ0=hcϕ=1240 eVnm2.14 eV=579 nm,\lambda_0 = \frac{hc}{\phi} = \frac{1240\ \text{eV}\cdot\text{nm}}{2.14\ \text{eV}} = 579\ \text{nm},

which falls in the visible (yellow) part of the spectrum. Cesium is therefore photoelectrically sensitive to ordinary visible light, unlike most metals, whose work functions of 45 eV5\ \text{eV} push their threshold wavelengths into the ultraviolet.

Applications: Photomultipliers and Photovoltaic Cells

The photoelectric effect underlies two technologies central to modern experimental physics and everyday life. A photomultiplier tube exploits a low-work-function photocathode (often a cesium compound, as in the worked example above) to convert a single incoming photon into a single ejected photoelectron, then accelerates that electron into a series of intermediate electrodes (dynodes), each of which is struck hard enough to eject several additional electrons by secondary emission; the resulting cascade, multiplying the electron count by a factor of a few at each of perhaps ten dynode stages, converts the arrival of a single photon into a macroscopic, easily measured current pulse containing millions of electrons. This single-photon sensitivity makes photomultiplier tubes essential wherever extremely faint light must be detected and counted, including the gamma-ray detectors used in PET scanners (discussed later in this chapter) and in nuclear and particle-physics experiments generally.

A closely related but distinct effect, the photovoltaic effect, underlies solar cells: rather than ejecting an electron entirely from the material, an absorbed photon in a semiconductor promotes an electron across the material’s band gap (the semiconductor analog of the work function, examined further in solid-state contexts), and a built-in electric field at a junction between two differently doped semiconductor layers then separates the resulting electron and the vacancy (hole) it leaves behind before they can recombine, driving a current through an external circuit. As in the ordinary photoelectric effect, only photons with energy exceeding a threshold (the band-gap energy) contribute usable electrons, which is why solar-cell efficiency depends sensitively on matching the semiconductor’s band gap to the solar spectrum.

X-Ray Production: Bremsstrahlung

The photoelectric effect converts a photon into an energetic electron; an energetic electron can conversely give up part of its energy as radiation when it is abruptly decelerated in matter. This bremsstrahlung process is the standard laboratory and industrial method of producing X-rays. It is an energy-bookkeeping inverse of the photoelectric effect, not its literal microscopic time reverse (which would involve radiative recombination into a bound state). In an X-ray tube, electrons are accelerated from rest through a large potential difference VV (typically tens to hundreds of kilovolts) and strike a dense metal target (commonly tungsten). As each electron decelerates within the target — bremsstrahlung, German for “braking radiation” — it radiates part or all of its kinetic energy as one or more photons.

Because an individual electron can, in principle, lose its entire kinetic energy eVeV in a single deceleration event (converting essentially all its kinetic energy into one photon), there is a sharply defined maximum photon energy — and correspondingly a minimum wavelength — that the tube can produce, set by

eV=hcλminλmin=hceV,eV = \frac{hc}{\lambda_{\min}} \quad \Longrightarrow \quad \lambda_{\min} = \frac{hc}{eV},

known as the Duane–Hunt limit. Most electrons instead lose their energy gradually over many collisions, radiating photons of smaller energy at each step and producing a continuous spectrum of wavelengths longer than λmin\lambda_{\min} — but no photon in the entire spectrum can have a wavelength shorter than λmin\lambda_{\min}, since no single electron carries more than eVeV of kinetic energy to begin with. Superimposed on this continuous bremsstrahlung spectrum are sharp characteristic X-ray lines, produced when an incident electron knocks an inner-shell electron out of a target atom and an outer electron falls down to fill the vacancy, emitting a photon of energy fixed by the target element’s inner-shell energy levels (Moseley’s law for these characteristic energies is developed in Chapter 11). Unlike the continuous bremsstrahlung background, the characteristic lines depend on the target material, not on the accelerating voltage (once VV is large enough to eject the inner-shell electron in the first place).

Bremsstrahlung is worth separating into its classical and its quantum halves, because only the second is new here. The classical half — that a charge which accelerates radiates, and that the radiation carries energy away — is already in Maxwell’s equations, and Figure 6.3 is that statement on its own: shake a charge and kinks in its field propagate outward at cc, taking energy with them. Stopping a charge dead is an acceleration like any other, so an electron slamming into a tungsten anode must radiate. What classical physics cannot supply is the sharp edge at λmin\lambda_{\min}: a continuous field theory sets no floor on the wavelength radiated in a single event, and the Duane–Hunt limit exists only because the radiated energy comes in quanta hfhf and one electron brings only eVeV to spend.

Screenshot of the Radio Waves simulation

Figure 6.3:An accelerating charge and the field it radiates. Move the charge by hand and watch the disturbance propagate outward at cc — the classical mechanism behind bremsstrahlung, and the one the electron in an X-ray tube obeys on its way to producing a photon of energy up to eVeV.

Interactive simulation: Radio Waves

Worked Example: Minimum Wavelength from a Diagnostic X-Ray Tube

A medical diagnostic X-ray tube is operated at an accelerating voltage of V=80.0 kVV = 80.0\ \text{kV}. The Duane–Hunt limit gives

λmin=hceV=1240 eVnm8.00×104 eV=1.55×102 nm=15.5 pm.\lambda_{\min} = \frac{hc}{eV} = \frac{1240\ \text{eV}\cdot\text{nm}}{8.00\times10^{4}\ \text{eV}} = 1.55\times10^{-2}\ \text{nm} = 15.5\ \text{pm}.

This is comparable to, and somewhat shorter than, typical interatomic spacings in crystals (0.1\sim 0.10.3 nm0.3\ \text{nm}), which is why X-rays of this energy scale are useful for crystallographic diffraction (Chapter 5) as well as medical imaging, where their short wavelength (and correspondingly high photon energy) allows them to penetrate soft tissue while being partially absorbed by denser bone.

6.3Compton Scattering, Pair Production, and the Photon

Compton Scattering

Even after the photoelectric effect, one could imagine “photon-like” energy exchange as a property specific to bound electrons in a metal, without light itself consisting of localized particles carrying momentum. Arthur Compton’s 1923 experiment removed this loophole by showing that photons scattering from a free electron transfer momentum exactly as a particle collision would.

In Compton’s experiment, X-rays of a single wavelength λ\lambda are directed at a target of loosely bound (effectively free) electrons, and the wavelength λ\lambda' of the scattered X-rays is measured as a function of scattering angle θ\theta. Classically, an electromagnetic wave incident on a charge should simply drive that charge to oscillate at the incident frequency and re-radiate at the same frequency (Thomson scattering); no wavelength shift is expected. Compton observed a systematic increase in wavelength, λ>λ\lambda' > \lambda, growing with scattering angle θ\theta and independent of the target material — a signature of a two-body collision, not wave re-radiation.

Deriving the Compton Formula

Treat the photon as a particle with energy E=hc/λE = hc/\lambda and momentum p=E/c=h/λp = E/c = h/\lambda (consistent with the massless-particle limit of the energy–momentum relation from Chapter 3), and apply conservation of relativistic energy and momentum to an elastic collision between the photon and an initially free, stationary electron of mass mem_e. Let the photon scatter through angle θ\theta, emerging with wavelength λ\lambda', while the electron recoils with momentum pep_e and (relativistic) energy EeE_e. The three momentum components entering the collision — incident photon momentum h/λh/\lambda along the initial direction, and zero for the electron — must balance the two outgoing momenta, whose vector sum (photon momentum h/λh/\lambda' at angle θ\theta, electron momentum pep_e at some recoil angle) forms a triangle. The law of cosines applied to that triangle gives

(pec)2=(hcλ)2+(hcλ)22(hcλ)(hcλ)cosθ.(i)(p_ec)^2 = \left(\frac{hc}{\lambda}\right)^2 + \left(\frac{hc}{\lambda'}\right)^2 - 2\left(\frac{hc}{\lambda}\right)\left(\frac{hc}{\lambda'}\right)\cos\theta. \tag{i}

Conservation of energy, with the electron initially at rest (Ee(0)=mec2E_e^{(0)} = m_ec^2), gives

Ee=hcλhcλ+mec2.(ii)E_e = \frac{hc}{\lambda} - \frac{hc}{\lambda'} + m_ec^2. \tag{ii}

Squaring (ii) and using the energy–momentum invariant Ee2=(pec)2+(mec2)2E_e^2 = (p_ec)^2 + (m_ec^2)^2 from Chapter 3 to eliminate EeE_e in favor of pecp_ec, then substituting (i) for (pec)2(p_ec)^2, produces (after the (hcλ)2\left(\frac{hc}{\lambda}\right)^2, (hcλ)2\left(\frac{hc}{\lambda'}\right)^2, and (mec2)2(m_ec^2)^2 terms cancel identically between the two sides) the much simpler relation

mec2(hcλhcλ)=hcλhcλ(1cosθ).m_ec^2\left(\frac{hc}{\lambda} - \frac{hc}{\lambda'}\right) = \frac{hc}{\lambda}\cdot\frac{hc}{\lambda'}\,(1-\cos\theta).

Dividing through by hchc, multiplying both sides by λλ/mec2\lambda\lambda'/m_ec^2, and simplifying λ(1λ1λ)λ=λλ\lambda\left(\frac1\lambda-\frac1{\lambda'}\right)\lambda' = \lambda'-\lambda yields the Compton scattering formula:

λλ=hmec(1cosθ).\lambda' - \lambda = \frac{h}{m_ec}(1 - \cos\theta).

The constant h/mec=2.426×1012 mh/m_ec = 2.426\times 10^{-12}\ \text{m} is the Compton wavelength of the electron. The formula correctly predicts zero shift at θ=0\theta = 0 (forward, undeflected “scattering”) and maximum shift 2h/mec2h/m_ec at θ=180°\theta = 180° (photon backscattered), matches the observed angular dependence precisely, and — crucially — is independent of the incident wavelength λ\lambda itself, matching experiment. Compton scattering is direct, quantitative confirmation that a photon carries momentum p=h/λp = h/\lambda and transfers it to a free electron exactly as one particle colliding with another.

The Compton formula in terms of photon energy

The wavelength form λλ=(h/mec)(1cosθ)\lambda' - \lambda = (h/m_ec)(1-\cos\theta) is the natural one for X-ray diffraction work, where wavelengths are measured directly, but gamma-ray spectroscopy — including the Compton-edge discussion below — more often calls for the scattered photon’s energy E=hc/λE' = hc/\lambda' directly in terms of the incident energy E=hc/λE = hc/\lambda. Substituting λ=hc/E\lambda = hc/E and λ=hc/E\lambda' = hc/E' into the Compton formula gives

hcEhcE=hmec(1cosθ).\frac{hc}{E'} - \frac{hc}{E} = \frac{h}{m_ec}(1-\cos\theta).

Multiplying through by EE/(hc)EE'/(hc) and solving for EE' yields

E=E1+Emec2(1cosθ).E' = \frac{E}{1 + \dfrac{E}{m_ec^2}(1-\cos\theta)}.

Setting θ=180°\theta = 180° gives the minimum possible scattered-photon energy, Emin=E/[1+2E/(mec2)]E'_{\min} = E/[1 + 2E/(m_ec^2)], and hence the maximum possible energy ΔEmax=EEmin\Delta E_{\max} = E - E'_{\min} that a single Compton-scattering event can deposit in a detector — the location of the Compton edge introduced below.

Worked Example: Compton-Scattered Molybdenum X-Rays

X-rays of wavelength λ=0.100 nm\lambda = 0.100\ \text{nm} (comparable to characteristic molybdenum KαK_\alpha X-rays used in crystallography) Compton-scatter off free electrons at θ=60°\theta = 60°. The wavelength shift is

Δλ=hmec(1cos60°)=(2.426×1012 m)(10.500)=1.21×1012 m=1.21 pm,\Delta\lambda = \frac{h}{m_ec}(1-\cos 60°) = (2.426\times10^{-12}\ \text{m})(1 - 0.500) = 1.21\times10^{-12}\ \text{m} = 1.21\ \text{pm},

so the scattered wavelength is λ=101.2 pm\lambda' = 101.2\ \text{pm}. In photon-energy terms, the incident photon carries E=hc/λ=(1240 eVnm)/(0.100 nm)=12.40 keVE = hc/\lambda = (1240\ \text{eV}\cdot\text{nm})/(0.100\ \text{nm}) = 12.40\ \text{keV}, while the scattered photon carries E=hc/λ=(1240 eVnm)/(0.1012 nm)=12.25 keVE' = hc/\lambda' = (1240\ \text{eV}\cdot\text{nm})/(0.1012\ \text{nm}) = 12.25\ \text{keV}. The energy transferred to the recoiling electron is therefore ΔE=EE0.15 keV=150 eV\Delta E = E - E' \approx 0.15\ \text{keV} = 150\ \text{eV} — a small but entirely measurable fraction of the incident photon’s energy, exactly the kind of energy loss Compton measured to confirm the formula.

The Compton Edge

In a real gamma-ray or X-ray detector, photons scatter through the full range of angles 0θ180°0 \le \theta \le 180° available inside the detector material, and the detector records the energy ΔE(θ)=EE(θ)\Delta E(\theta) = E - E'(\theta) actually deposited by the recoiling electron for each scattering event. Because ΔE(θ)\Delta E(\theta) increases monotonically with θ\theta (least energy transfer for forward scattering, most for backscattering), there is a sharply defined maximum possible energy deposit, occurring at θ=180°\theta = 180° — the Compton edge — beyond which no Compton-scattered electron can deposit more energy in a single scattering event, no matter how many photons are examined. A photon that instead deposits its entire energy in one interaction (via the photoelectric effect on a bound atomic electron, rather than Compton scattering a free one) produces a separate, sharp peak at the full incident photon energy, the photopeak. Gamma-ray spectroscopists routinely distinguish these two features — a sharp photopeak plus a broad continuum of Compton-scattered energies cut off abruptly at the Compton edge — when interpreting a detector’s measured energy spectrum, since both are simultaneous, competing ways the same photon can interact with the detector material.

Pair Production and Annihilation

A further, still more dramatic demonstration of the particle nature of light is pair production: a sufficiently energetic photon, passing near a nucleus, can convert entirely into an electron–positron pair,

γe+e+,\gamma \rightarrow e^- + e^+,

requiring a photon energy of at least 2mec2=1.022 MeV2m_ec^2 = 1.022\ \text{MeV} (twice the electron rest energy) — a direct manifestation of mass–energy equivalence (Chapter 3), converting a massless particle’s energy into the rest mass of two massive particles.

A nearby massive third body — typically an atomic nucleus — is required to conserve momentum. This can be seen directly from the energy–momentum four-vector formalism of Chapter 3: an isolated photon of energy EγE_\gamma has momentum pγ=Eγ/cp_\gamma = E_\gamma/c, but a resulting electron–positron pair with the same total energy EγE_\gamma (by energy conservation) necessarily has total momentum strictly less than Eγ/cE_\gamma/c, because each massive particle satisfies E2=(pc)2+(mc2)2>(pc)2E^2 = (pc)^2+(mc^2)^2 > (pc)^2, so pc<Epc < E for each — the pair’s combined momentum cannot match the photon’s original momentum at the same total energy. A nucleus nearby can absorb the small difference in momentum (recoiling with negligible kinetic energy, because its mass is so much larger than mem_e) while barely affecting the energy balance, resolving the mismatch; in a vacuum with no such third body available, momentum conservation alone forbids the process outright, regardless of how much energy the lone photon carries.

The reverse process, pair annihilation, e+e+2γe^- + e^+ \to 2\gamma (two photons are required, rather than one, to conserve momentum in the electron–positron center-of-momentum frame — see Chapter 3, Problem 3), converts rest mass entirely back into photon energy and is used, for example, in positron-emission tomography (PET) imaging, where each annihilation of an injected positron-emitting tracer with a nearby atomic electron produces two back-to-back 511 keV511\ \text{keV} gamma rays that a ring of detectors uses to reconstruct the tracer’s location.

Worked Example: Sharing Energy Above Pair-Production Threshold

A photon of energy Eγ=3.00 MeVE_\gamma = 3.00\ \text{MeV}, well above the 1.022 MeV1.022\ \text{MeV} threshold, undergoes pair production near a heavy nucleus. Because the nucleus is far more massive than the electron or positron, it absorbs essentially none of the available kinetic energy (a large mass can supply whatever small momentum balance is needed while carrying away almost no energy, exactly analogous to how a wall barely recoils, and gains almost no kinetic energy, when it reflects a ball). The energy left over after paying the 2mec22m_ec^2 rest-mass cost is therefore shared, to good approximation, between the electron and positron as kinetic energy:

Ke+Ke+Eγ2mec2=3.00 MeV1.022 MeV=1.978 MeV.K_{e^-} + K_{e^+} \approx E_\gamma - 2m_ec^2 = 3.00\ \text{MeV} - 1.022\ \text{MeV} = 1.978\ \text{MeV}.

If the pair shares this energy symmetrically (not required by any conservation law, but a useful simplifying assumption), each particle carries about 0.989 MeV0.989\ \text{MeV} of kinetic energy — comparable to its own rest energy, so each is produced at a substantial fraction of the speed of light.

The Photon: A Unified Picture

Four seemingly unrelated phenomena — blackbody radiation, the photoelectric effect, X-ray production, and Compton scattering — together with pair production and annihilation, are all consequences of a single underlying fact: electromagnetic radiation exchanges energy and momentum with matter in discrete, particle-like quanta, E=hfE=hf and p=h/λp=h/\lambda, rather than continuously. Blackbody radiation shows that an oscillator can only emit or absorb energy in these units; the photoelectric effect shows that a photon transfers its entire energy to a single electron in one step; X-ray production shows how an electron’s kinetic energy can be converted into photons, with a sharply bounded maximum photon energy; Compton scattering shows that a photon carries not just energy but momentum, exchanged with a free electron exactly as in a two-body collision; and pair production and annihilation show that a photon’s energy is, via E=mc2E=mc^2, interconvertible with the rest mass of matter itself. The characteristic quantum features of all five are explained, quantitatively and without exception, by the same photon concept. Yet, as Chapters 45 demonstrated, light also produces interference and diffraction patterns with no possible explanation in a naive particle picture. Chapter 7 confronts this apparent contradiction directly, and shows that it is resolved not by choosing one description over the other, but by recognizing that matter, too, has a wave nature — and that wave and particle descriptions are two complementary faces of a single, more complete quantum picture.

6.4Summary

6.5Problems

Solution to Exercise 6.1 #

Wien’s law gives

T=2.898×103 m K500×109 m=5.80×103 K.T=\frac{2.898\times10^{-3}\ \text{m K}}{500\times10^{-9}\ \text{m}}=5.80\times10^3\ \text{K}.

The difference from 5778 K5778\ \text{K} is 18 K18\ \text{K}, or 0.3%0.3\%. Therefore, the peak wavelength estimates the solar surface temperature as about 5800 K5800\ \text{K}, in excellent agreement with the stated value.

Solution to Exercise 6.2 #

Wien’s law gives λmax=(2.898×103 m K)/(2900 K)=9.99×107 m=999 nm\lambda_{\max}=(2.898\times10^{-3}\ \text{m K})/(2900\ \text{K})=9.99\times10^{-7}\ \text{m}=999\ \text{nm}, which is infrared. The blackbody flux is

PA=σT4=(5.670×108 W m2K4)(2900 K)4=4.01×106 W/m2.\frac PA=\sigma T^4=(5.670\times10^{-8}\ \text{W m}^{-2}\text{K}^{-4})(2900\ \text{K})^4=4.01\times10^6\ \text{W/m}^2.
Blackbody spectral radiance curve at 2900 kelvin peaking at 999 nanometers in the infrared, with the visible band from 380 to 750 nanometers shaded and shown to cover only the rising edge of the curve.

Figure 6.4:The filament’s blackbody curve peaks in the infrared at 999 nm999\ \text{nm}; the shaded visible band captures only the small, rising left shoulder of the distribution.

Therefore, the filament peaks near 1.00 μm1.00\ \mu\text{m} in the infrared and radiates 4.01×106 W/m24.01\times10^6\ \text{W/m}^2 ideally; most of its power is invisible infrared rather than useful visible light.

Solution to Exercise 6.3 #

The radius is R=500(6.96×108 m)=3.48×1011 mR=500(6.96\times10^8\ \text{m})=3.48\times10^{11}\ \text{m}. Thus

P=4πR2σT4=4π(3.48×1011 m)2(5.670×108)(3200 K)4=9.05×1030 W.P=4\pi R^2\sigma T^4=4\pi(3.48\times10^{11}\ \text{m})^2(5.670\times10^{-8})(3200\ \text{K})^4=9.05\times10^{30}\ \text{W}.

The ratio is 9.05×1030/(3.83×1026)=2.36×1049.05\times10^{30}/(3.83\times10^{26})=2.36\times10^4. Therefore, the red giant radiates about 9.1×1030 W9.1\times10^{30}\ \text{W}, or 2.4×1042.4\times10^4 times the Sun’s luminosity.

Solution to Exercise 6.4 #

Using hc=1240 eV nmhc=1240\ \text{eV nm},

Eγ=1240 eV nm400 nm=3.10 eV,Kmax=3.10 eV2.28 eV=0.82 eV.E_\gamma=\frac{1240\ \text{eV nm}}{400\ \text{nm}}=3.10\ \text{eV},\qquad K_{\max}=3.10\ \text{eV}-2.28\ \text{eV}=0.82\ \text{eV}.

Since eV0=KmaxeV_0=K_{\max}, V0=0.82 VV_0=0.82\ \text{V}. At threshold, ϕ=hc/λ0\phi=hc/\lambda_0, so λ0=1240/2.28=544 nm\lambda_0=1240/2.28=544\ \text{nm}. Therefore, the photon energy is 3.10 eV3.10\ \text{eV}, the largest electron kinetic energy is 0.82 eV0.82\ \text{eV}, the stopping potential is 0.82 V0.82\ \text{V}, and the threshold wavelength is 544 nm544\ \text{nm}.

Solution to Exercise 6.5 #

The frequencies are f1=c/(450 nm)=6.67×1014 Hzf_1=c/(450\ \text{nm})=6.67\times10^{14}\ \text{Hz} and f2=c/(360 nm)=8.33×1014 Hzf_2=c/(360\ \text{nm})=8.33\times10^{14}\ \text{Hz}. Subtracting eV0=hfϕeV_0=hf-\phi for the two data points gives

h=e(1.280.65) Vf2f1=3.78×1015 eV s=6.06×1034 J s.h=\frac{e(1.28-0.65)\ \text{V}}{f_2-f_1}=3.78\times10^{-15}\ \text{eV s}=6.06\times10^{-34}\ \text{J s}.

Then ϕ=hf1eV1=(3.78×1015)(6.67×1014)0.65=1.87 eV\phi=hf_1-eV_1=(3.78\times10^{-15})(6.67\times10^{14})-0.65=1.87\ \text{eV}.

Stopping potential versus frequency with two measured points and the straight line through them, showing the line's slope equals h over e and its frequency-axis intercept equals the threshold frequency.

Figure 6.5:The two measurements determine the line V0=(h/e)fϕ/eV_0=(h/e)f-\phi/e completely: its slope gives hh without assuming a textbook value, and its intercept with V0=0V_0=0 gives the threshold frequency f0=ϕ/hf_0=\phi/h.

Therefore, the data give h=6.06×1034 J sh=6.06\times10^{-34}\ \text{J s} and a work function of 1.87 eV1.87\ \text{eV}.

Solution to Exercise 6.6 #

The incident photon energy is E=1240/150=8.27 eVE=1240/150=8.27\ \text{eV}, which exceeds ϕ=6.35 eV\phi=6.35\ \text{eV}. Thus Kmax=8.276.35=1.92 eVK_{\max}=8.27-6.35=1.92\ \text{eV}. The threshold wavelength is

λ0=1240 eV nm6.35 eV=195 nm.\lambda_0=\frac{1240\ \text{eV nm}}{6.35\ \text{eV}}=195\ \text{nm}.

Therefore, 150 nm150\ \text{nm} ultraviolet light ejects electrons with up to 1.92 eV1.92\ \text{eV} kinetic energy, while visible and near-UV wavelengths longer than 195 nm195\ \text{nm} cannot overcome platinum’s work function.

Solution to Exercise 6.7 #

An electron accelerated through 120 kV120\ \text{kV} gains eV=120 keVeV=120\ \text{keV}. Hence

λmin=hceV=1240 eV nm120000 eV=0.0103 nm.\lambda_{\min}=\frac{hc}{eV}=\frac{1240\ \text{eV nm}}{120000\ \text{eV}}=0.0103\ \text{nm}.

Therefore, the minimum wavelength is 0.0103 nm0.0103\ \text{nm} and the maximum photon energy is 120 keV120\ \text{keV}; doubling the voltage halves λmin\lambda_{\min}.

Solution to Exercise 6.8 #

Each incident electron begins with energy eVeV, but it can lose any fraction of that energy in one encounter and can lose the rest in subsequent collisions, target excitation, or heat. A photon made in one braking event can therefore have any energy from nearly zero up to eVeV, with Eγ=hc/λE_\gamma=hc/\lambda. Therefore, the many allowed energy shares produce a continuous bremsstrahlung spectrum, even though the endpoint energy and minimum wavelength are sharp.

Solution to Exercise 6.9 #

At 9090^\circ, Δλ=h/(mec)=2.426 pm=0.002426 nm\Delta\lambda=h/(m_ec)=2.426\ \text{pm}=0.002426\ \text{nm}. Thus

λ=0.0711 nm+0.002426 nm=0.073526 nm,\lambda'=0.0711\ \text{nm}+0.002426\ \text{nm}=0.073526\ \text{nm},
E=1240 eV nm0.073526 nm=16.86 keV.E'=\frac{1240\ \text{eV nm}}{0.073526\ \text{nm}}=16.86\ \text{keV}.

The incident energy is 1240/0.0711=17.44 keV1240/0.0711=17.44\ \text{keV}, so the electron receives 17.4416.86=0.58 keV17.44-16.86=0.58\ \text{keV}.

Wavelength shift versus scattering angle from zero to 180 degrees, with the 90 degree and 180 degree cases marked, alongside a bar chart comparing the fractional shift at 90 degrees for visible light and for X-rays on a log scale.

Figure 6.6:Left: Δλ=(h/mec)(1cosθ)\Delta\lambda=(h/m_ec)(1-\cos\theta) depends only on angle, not wavelength; this problem’s 9090^\circ shift and Problem 10’s 180180^\circ shift are both points on the same curve. Right: the same 2.426 pm2.426\ \text{pm} shift is four parts per million of a visible wavelength but several percent of an X-ray wavelength (Problem 12) — why Compton scattering was discovered with X-rays, not light.

Therefore, the shift is 2.426 pm2.426\ \text{pm}, the scattered photon has wavelength 0.07353 nm0.07353\ \text{nm} and energy 16.86 keV16.86\ \text{keV}, and the electron receives about 0.58 keV0.58\ \text{keV}.

Solution to Exercise 6.10 #

Putting θ=180\theta=180^\circ into Δλ=(h/mec)(1cosθ)\Delta\lambda=(h/m_ec)(1-\cos\theta) gives

Δλ=hmec[1(1)]=2hmec=4.852×1012 m=4.852 pm.\Delta\lambda=\frac{h}{m_ec}[1-(-1)]=\frac{2h}{m_ec}=4.852\times10^{-12}\ \text{m}=4.852\ \text{pm}.

For λh/(mec)\lambda\ll h/(m_ec), λ=λ+2h/(mec)2h/(mec)\lambda'=\lambda+2h/(m_ec)\approx2h/(m_ec), so E/E=λ/λ1E'/E=\lambda/\lambda'\ll1 and (EE)/E1(E-E')/E\approx1. This is the θ=180\theta=180^\circ endpoint of the same curve shown in Figure 6.6. Therefore, backscattering shifts the wavelength by 4.852 pm4.852\ \text{pm} and transfers nearly 100%100\% of a sufficiently energetic photon’s energy to the electron.

Solution to Exercise 6.11 #

Let A=hc/λA=hc/\lambda, B=hc/λB=hc/\lambda', and M=mec2M=m_ec^2. Equations (i) and (ii) give

Ee2=(AB+M)2=A2+B2+M22AB+2AM2BM,E_e^2=(A-B+M)^2=A^2+B^2+M^2-2AB+2AM-2BM,
Ee2=(pec)2+M2=A2+B22ABcosθ+M2.E_e^2=(p_ec)^2+M^2=A^2+B^2-2AB\cos\theta+M^2.

Cancelling A2A^2, B2B^2, and M2M^2 leaves 2AB+2M(AB)=2ABcosθ-2AB+2M(A-B)=-2AB\cos\theta, or M(AB)=AB(1cosθ)M(A-B)=AB(1-\cos\theta). Therefore, explicit cancellation gives exactly the simplified relation quoted in the text.

Solution to Exercise 6.12 #

At 9090^\circ, Δλ=2.426 pm\Delta\lambda=2.426\ \text{pm}. Therefore,

Δλλ=2.426×1012 m600×109 m=4.04×106.\frac{\Delta\lambda}{\lambda}=\frac{2.426\times10^{-12}\ \text{m}}{600\times10^{-9}\ \text{m}}=4.04\times10^{-6}.

The right-hand panel of Figure 6.6 compares this fraction directly with the X-ray case of Problem 9. Therefore, visible light shifts by only four parts per million, a tiny shift that is difficult to resolve in ordinary Compton-scattering measurements, whereas the same fixed Compton shift is a measurable fraction of an X-ray wavelength.

Solution to Exercise 6.13 #

At minimum, the photon supplies two electron rest energies:

Emin=2mec2=2(0.511 MeV)=1.022 MeV,E_{\min}=2m_ec^2=2(0.511\ \text{MeV})=1.022\ \text{MeV},
λ=1240 eV nm1.022×106 eV=0.00121 nm=1.21 pm.\lambda=\frac{1240\ \text{eV nm}}{1.022\times10^6\ \text{eV}}=0.00121\ \text{nm}=1.21\ \text{pm}.

An isolated photon has p=E/cp=E/c, but two massive particles with the same total energy have total momentum less than E/cE/c; energy and momentum cannot both be conserved. Therefore, pair production requires at least 1.022 MeV1.022\ \text{MeV} photons of wavelength about 1.21 pm1.21\ \text{pm} and a nearby nucleus to absorb recoil momentum.

Solution to Exercise 6.14 #

The rest-energy cost is 2mec2=1.022 MeV2m_ec^2=1.022\ \text{MeV}, leaving

Kavailable=2.50 MeV1.022 MeV=1.478 MeV.K_\mathrm{available}=2.50\ \text{MeV}-1.022\ \text{MeV}=1.478\ \text{MeV}.

Equal sharing gives Ke=Ke+=0.739 MeVK_e=K_{e^+}=0.739\ \text{MeV} and total energy 0.739+0.511=1.250 MeV0.739+0.511=1.250\ \text{MeV} for each.

Horizontal stacked bar showing the incident 2.50 megaelectronvolt photon energy divided into four segments: the electron rest energy, the positron rest energy, and each particle's 0.739 megaelectronvolt kinetic energy.

Figure 6.7:The photon’s 2.50 MeV2.50\ \text{MeV} splits into a fixed 1.022 MeV1.022\ \text{MeV} entry fee (the two rest masses) and a remaining 1.478 MeV1.478\ \text{MeV} divided equally as kinetic energy.

Therefore, each particle has 0.739 MeV0.739\ \text{MeV} kinetic energy and 1.250 MeV1.250\ \text{MeV} total energy.

Solution to Exercise 6.15 #

At rest the electron and positron have total energy 2mec2=1.022 MeV2m_ec^2=1.022\ \text{MeV} and total momentum zero. The two photons must have equal, opposite momenta and equal energies, so each has 0.511 MeV0.511\ \text{MeV}. Its wavelength is

λ=1240 eV nm511000 eV=0.00243 nm=2.43 pm.\lambda=\frac{1240\ \text{eV nm}}{511000\ \text{eV}}=0.00243\ \text{nm}=2.43\ \text{pm}.

Therefore, annihilation produces two opposite 511 keV511\ \text{keV} gamma rays of wavelength 2.43 pm2.43\ \text{pm}; a detector ring records their coincident, back-to-back directions to localize the annihilation line through the patient.

Solution to Exercise 6.16 #

The threshold is 2mpc2=2(938 MeV)=1876 MeV=1.876 GeV2m_pc^2=2(938\ \text{MeV})=1876\ \text{MeV}=1.876\ \text{GeV}. Its wavelength is

λ=1240 eV nm1.876×109 eV=6.61×107 nm=0.661 fm.\lambda=\frac{1240\ \text{eV nm}}{1.876\times10^9\ \text{eV}}=6.61\times10^{-7}\ \text{nm}=0.661\ \text{fm}.

Compared with the electron-pair threshold wavelength 1.21 pm1.21\ \text{pm}, this is smaller by about 1836, the proton-to-electron mass ratio. Therefore, proton--antiproton production needs about 1.88 GeV1.88\ \text{GeV} photons with a 0.661 fm0.661\ \text{fm} wavelength.

Solution to Exercise 6.17 #

For 180180^\circ scattering, E=E/[1+2E/(mec2)]E'=E/[1+2E/(m_ec^2)]. Hence

E=0.662 MeV1+2(0.662/0.511)=0.184 MeV,E'=\frac{0.662\ \text{MeV}}{1+2(0.662/0.511)}=0.184\ \text{MeV},
ΔEmax=0.662 MeV0.184 MeV=0.478 MeV.\Delta E_{\max}=0.662\ \text{MeV}-0.184\ \text{MeV}=0.478\ \text{MeV}.

Full photoelectric absorption deposits 0.662 MeV0.662\ \text{MeV}.

Idealized gamma-ray energy-deposition spectrum showing a continuum of energies rising toward a Compton edge at 0.478 megaelectronvolts, and a separate sharp photopeak at 0.662 megaelectronvolts.

Figure 6.8:A real detector shows both features side by side: a continuum of partial-absorption events ending at the 180180^\circ Compton edge, and a separate sharp photopeak from full photoelectric absorption. (Continuum shape is schematic, not the exact Klein–Nishina cross section.)

Therefore, the Compton edge is 0.478 MeV0.478\ \text{MeV} and the photopeak is 0.662 MeV0.662\ \text{MeV}; both appear because photons can either scatter incompletely or be fully absorbed.

Solution to Exercise 6.18 #

The charge needed is Q=1.0×1012 CQ=1.0\times10^{-12}\ \text{C}, so

N=Qe=1.0×1012 C1.602×1019 C=6.24×106 electrons.N=\frac Qe=\frac{1.0\times10^{-12}\ \text{C}}{1.602\times10^{-19}\ \text{C}}=6.24\times10^6\ \text{electrons}.

Ten stages multiplying by four give 410=1.05×1064^{10}=1.05\times10^6 electrons, or 1.68×1013 C1.68\times10^{-13}\ \text{C}, below the stated threshold. Therefore, a photomultiplier makes a photon detectable by multiplying one photoelectron into millions, but ten factor-four stages alone are short of a 1.0×1012 C1.0\times10^{-12}\ \text{C} pulse.

Solution to Exercise 6.19 #

Classical treatments assume electromagnetic energy is continuously divisible: cavity modes can receive the continuous equipartition energy kBTk_BT, and a brighter wave can transfer energy continuously to an electron. The linked quantum postulates replace this assumption with exchanges in indivisible packets of size hfhf: Planck applied the quantization first to the cavity-wall oscillators, suppressing high-frequency modes, and Einstein extended the same quantum of energy to the radiation itself, so one electron receives one photon’s energy at a time. Thus both puzzles share the same cure — energy exchange in units of hfhf — even though the photoelectric effect requires the stronger claim that the radiation field itself is quantized.

Solution to Exercise 6.20 #

The threshold condition is EγEgE_\gamma\ge E_g, so

λmax=1240 eV nm1.1 eV=1.13×103 nm=1.13 μm.\lambda_{\max}=\frac{1240\ \text{eV nm}}{1.1\ \text{eV}}=1.13\times10^3\ \text{nm}=1.13\ \mu\text{m}.

This lies in the near infrared. Photon energy above the band gap first creates an electron--hole pair; excess energy is rapidly lost to lattice vibrations rather than producing proportional electrical work. Therefore, silicon can use wavelengths up to about 1.13 μm1.13\ \mu\text{m}, and photons far above the 1.1 eV1.1\ \text{eV} gap waste much of their extra energy as heat.