Skip to content

Physics in Everyday Life: The Quantum Mechanics and Relativity Running Your Phone, GPS and MRI

Prerequisite:Unsolved Problems in Physics: 95% of the Cosmos Still Has Only a Name

Raw
  • The semiconductors in your phone rest on a consequence of quantum mechanics: an electron in a crystal can occupy only certain discrete bands of energy. Fix the band gap EgE_g and you have fixed, through a single exponential, both the color the material emits and the current that flows through it of its own accord at room temperature.
  • Miniaturization stalled because of tunneling. Every 1 nm1\ \mathrm{nm} shaved off the gate insulator multiplies the leakage current by roughly 7×1077 \times 10^{7}. That number falls out of an exponential you can evaluate by hand.
  • A GPS satellite clock runs fast relative to a clock on the ground by about 38 μs38\ \mu\mathrm{s} per day. This is the difference between a special-relativistic loss of −7.2 μs-7.2\ \mu\mathrm{s} and a general-relativistic gain of +45.7 μs+45.7\ \mu\mathrm{s}. Left uncorrected, the positioning error accumulates to about 11 km11\ \mathrm{km} in a single day.
  • What MRI actually sees is a minute imbalance of orientation among the hydrogen nuclei in your body: five nuclei in every million. That is still enough, because 1 mm31\ \mathrm{mm}^3 contains 3×10143 \times 10^{14} of them.
  • The three technologies share one equation, E=hfE = hf. A band gap becomes the color of light, the Zeeman splitting of a nucleus becomes a radio frequency, and the hyperfine structure of a cesium atom becomes the second itself.

1. Motivation: twentieth-century physics in your pocket

Section titled “1. Motivation: twentieth-century physics in your pocket”

Tell a physicist of 1900 that the theory they are about to build will, a hundred years later, be carried around by the whole of humanity in a slab that fits in the palm of a hand, and they will probably not believe you. Quantum mechanics and relativity both began as small discrepancies in the corner of a laboratory: a black-body spectrum that would not fit, an ether that could not be found.

Yet today, in the few seconds it takes you to open a map on your phone and check where you are, the following happens.

  1. Your finger touches the glass, a change in the capacitance of a transparent electrode is read out, and a silicon integrated circuit turns it into a number. Inside that circuit, electrons move through discrete energy bands.
  2. Differences in the arrival times of radio signals from GPS satellites at an altitude of roughly 2×104 km2\times 10^{4}\ \mathrm{km} are computed. The atomic clocks aboard those satellites have had special- and general-relativistic corrections built into them from the start.
  3. And if you are unwell, you go to a hospital and lie down inside an MRI scanner. The hydrogen nuclei in your body emit radio waves by nuclear magnetic resonance.

In this article we take these three in turn and carry every calculation through to a number. Anyone can say “relativity is being used here”; being able to produce “how many microseconds per day” yourself makes the statement suddenly concrete. The only mathematics we need is exponentials, square roots, and the approximation (1+x)1/2≈1+x/2(1+x)^{1/2} \approx 1 + x/2.

2. Preliminaries: one equation running through all three

Section titled “2. Preliminaries: one equation running through all three”

The three technologies look like they belong to entirely different fields, but at their root lies the same relation.

Definition 2.1(The Planck relation)

A single photon of an electromagnetic wave of frequency ff (angular frequency ω=2πf\omega = 2\pi f) carries energy

E=hf=ℏω,E = hf = \hbar \omega ,

where h=6.62607×10−34 J sh = 6.62607\times 10^{-34}\ \mathrm{J\,s} is the Planck constant and ℏ=h/(2π)\hbar = h/(2\pi) the reduced Planck constant.

Conversely, a system whose two energy levels differ by ΔE\Delta E absorbs and emits electromagnetic radiation at f=ΔE/hf = \Delta E / h.

This equation is a dictionary translating “energy difference” into “frequency”. As we shall see, ΔE\Delta E is the band gap in a semiconductor (visible to infrared), the Zeeman splitting of a nuclear spin in MRI (radio), and the hyperfine structure of the cesium atom in an atomic clock (microwave).

The constants used below are collected here. Values are given to four or five significant figures, based on the CODATA 2018 recommended values.

SymbolValueMeaning
cc2.99792×108 m/s2.99792\times 10^{8}\ \mathrm{m/s}speed of light in vacuum
hh6.62607×10−34 J s6.62607\times 10^{-34}\ \mathrm{J\,s}Planck constant
hchc1239.84 eV nm1239.84\ \mathrm{eV\,nm}conversion between wavelength and energy
kBk_B1.38065×10−23 J/K1.38065\times 10^{-23}\ \mathrm{J/K}Boltzmann constant
kBTk_B T (T=300 KT = 300\ \mathrm{K})0.02585 eV0.02585\ \mathrm{eV}thermal energy at room temperature
mem_e9.109×10−31 kg9.109\times 10^{-31}\ \mathrm{kg}electron mass
GM⊕GM_\oplus3.986×1014 m3/s23.986\times 10^{14}\ \mathrm{m^3/s^2}geocentric gravitational constant
R⊕R_\oplus6.371×106 m6.371\times 10^{6}\ \mathrm{m}mean radius of the Earth

3. The smartphone: discrete energies turned into electronics

Section titled “3. The smartphone: discrete energies turned into electronics”

Metals conduct well; glass does not conduct at all. Semiconductors sit in between, but what makes them interesting is not that they conduct moderately — it is that whether they conduct can be switched from outside. That switch is the transistor, and ten billion transistors together make the heart of a phone.

Why can it be switched? Because the energies available to an electron in a crystal are not continuous but arranged in bands.

Definition 3.1(Band gap)

The energies available to an electron in a crystal split into several continuous regions (energy bands), separated by regions in which no electron state exists (forbidden gaps). The highest band completely filled with electrons at absolute zero is the valence band, the empty band above it the conduction band, and their energy difference

Eg=Ebottom of conduction band−Etop of valence bandE_g = E_{\text{bottom of conduction band}} - E_{\text{top of valence band}}

is called the band gap. A material with Eg=0E_g = 0 is a metal; one whose EgE_g is well above kBTk_B T and of order a few eV is a semiconductor; one with a far larger gap is an insulator.

The reason bands exist is quantum mechanical. In an isolated atom the electron energies form discrete levels; line up 102310^{23} atoms into a crystal and the wave functions of neighboring atoms overlap, splitting each level into a dense band. In a periodic crystal, an electron wave of a certain wavelength is Bragg-reflected and cannot propagate, so a gap opens there — that is the forbidden gap.

Intrinsicn-type (donor-doped)p-type (acceptor-doped)EgThermal excitation is rareElectrons are the majority carriersHoles are the majority carriersConductionbandValencebandDonor levelsAcceptor levels
Band diagrams for an intrinsic, an n-type and a p-type semiconductor. The shaded lower band is the filled valence band; the outlined upper band is the conduction band.

3.2. What the band gap determines, part 1: the color of the light

Section titled “3.2. What the band gap determines, part 1: the color of the light”

Proposition 3.2(Band gap and emission wavelength)

In a direct-gap semiconductor of band gap EgE_g, when an electron at the bottom of the conduction band recombines with a hole at the top of the valence band and emits one photon, the vacuum wavelength λ\lambda of that photon is

λ=hcEg,numericallyλ [nm]=1239.84Eg [eV].\lambda = \frac{hc}{E_g}, \qquad \text{numerically}\quad \lambda\,[\mathrm{nm}] = \frac{1239.84}{E_g\,[\mathrm{eV}]}.
Proof(Proposition 3.2)

The energy the electron loses in recombining is exactly EgE_g. By conservation of energy, the emitted photon carries energy EgE_g as well. By Definition 2.1 the photon energy is E=hfE = hf, and in vacuum f=c/λf = c/\lambda, so

Eg=hcλ  ⟺  λ=hcEg.E_g = \frac{hc}{\lambda} \iff \lambda = \frac{hc}{E_g}.

Substituting hc=1239.84 eV nmhc = 1239.84\ \mathrm{eV\,nm} from the table below Definition 2.1 gives the relation for EgE_g measured in eV and λ\lambda in nm.

Example 3.3(Silicon does not glow; gallium nitride glows blue)

Feeding the tabulated values into Proposition 3.2:

MaterialEgE_gλ=1239.84/Eg\lambda = 1239.84/E_gAppearance
germanium Ge0.66 eV0.66\ \mathrm{eV}1879 nm1879\ \mathrm{nm}infrared
silicon Si1.12 eV1.12\ \mathrm{eV}1107 nm1107\ \mathrm{nm}infrared
gallium arsenide GaAs1.42 eV1.42\ \mathrm{eV}873 nm873\ \mathrm{nm}near infrared (remote controls)
gallium phosphide family≈2.0 eV\approx 2.0\ \mathrm{eV}620 nm620\ \mathrm{nm}red
InGaN (blue LED)≈2.76 eV\approx 2.76\ \mathrm{eV}449 nm449\ \mathrm{nm}blue
gallium nitride GaN3.4 eV3.4\ \mathrm{eV}365 nm365\ \mathrm{nm}ultraviolet

One proviso matters here. Proposition 3.2 assumes a direct gap. Si and Ge are indirect-gap materials — the bottom of the conduction band and the top of the valence band lie at different points in momentum space — so a photon alone cannot conserve momentum and a phonon (a lattice vibration) must assist. The emission probability is therefore smaller by orders of magnitude, and silicon does not emit light. That is why LEDs and lasers are made of GaAs or GaN, while silicon is left to do the computing.

3.3. What the band gap determines, part 2: the current that flows by itself

Section titled “3.3. What the band gap determines, part 2: the current that flows by itself”

At absolute zero a semiconductor is an insulator, but at room temperature thermal energy lifts valence electrons across the gap. The number of these spontaneously generated carriers fixes the character of the material.

Proposition 3.4(Intrinsic carrier density)

In an intrinsic (impurity-free) semiconductor of band gap EgE_g, the density nin_i of conduction electrons at temperature TT satisfies, for Eg≫kBTE_g \gg k_B T,

ni=NcNv exp⁡ ⁣(−Eg2kBT),n_i = \sqrt{N_c N_v}\,\exp\!\left(-\frac{E_g}{2k_B T}\right),

where NcN_c and NvN_v are the effective densities of states of the conduction and valence bands respectively; in typical semiconductors these are of order 1019 cm−310^{19}\ \mathrm{cm^{-3}} at room temperature.

Remark 3.5

This formula follows by integrating the Fermi distribution f(E)=[exp⁡((E−EF)/kBT)+1]−1f(E) = [\exp((E-E_F)/k_BT) + 1]^{-1} against the density of states of each band, approximating it by a Maxwell–Boltzmann distribution where E−EF≫kBTE - E_F \gg k_B T, and imposing the charge-neutrality condition n=pn = p of an intrinsic semiconductor. The derivation is in Chapter 1 of Sze–Ng, Physics of Semiconductor Devices. Here we use only the result, and we care about one feature of it: Eg/2kBTE_g/2k_BT sits in the exponent.

Example 3.6(Si and Ge differ by a factor of 3400 in free electrons)

At room temperature T=300 KT = 300\ \mathrm{K} we have kBT=0.02585 eVk_B T = 0.02585\ \mathrm{eV}, hence 2kBT=0.0517 eV2k_B T = 0.0517\ \mathrm{eV}.

Silicon (Eg=1.12 eVE_g = 1.12\ \mathrm{eV}, Nc=2.8×1019N_c = 2.8\times 10^{19}, Nv=1.04×1019 cm−3N_v = 1.04\times 10^{19}\ \mathrm{cm^{-3}}):

Eg2kBT=1.120.0517=21.66,e−21.66=3.9×10−10,NcNv=2.8×1019⋅1.04×1019=1.71×1019 cm−3,ni=1.71×1019⋅3.9×10−10=6.7×109 cm−3.\begin{aligned} \frac{E_g}{2k_BT} &= \frac{1.12}{0.0517} = 21.66, \qquad e^{-21.66} = 3.9\times 10^{-10},\\ \sqrt{N_cN_v} &= \sqrt{2.8\times 10^{19}\cdot 1.04\times 10^{19}} = 1.71\times 10^{19}\ \mathrm{cm^{-3}},\\ n_i &= 1.71\times 10^{19}\cdot 3.9\times 10^{-10} = 6.7\times 10^{9}\ \mathrm{cm^{-3}}. \end{aligned}

The measured value is 1.0×1010 cm−31.0\times 10^{10}\ \mathrm{cm^{-3}}, agreeing to within a factor of 1.5.

Germanium (Eg=0.66 eVE_g = 0.66\ \mathrm{eV}, Nc=1.04×1019N_c = 1.04\times 10^{19}, Nv=6.0×1018 cm−3N_v = 6.0\times 10^{18}\ \mathrm{cm^{-3}}):

Eg2kBT=0.660.0517=12.77,e−12.77=2.9×10−6,NcNv=1.04×1019⋅6.0×1018=7.9×1018 cm−3,ni=7.9×1018⋅2.9×10−6=2.3×1013 cm−3.\begin{aligned} \frac{E_g}{2k_BT} &= \frac{0.66}{0.0517} = 12.77, \qquad e^{-12.77} = 2.9\times 10^{-6},\\ \sqrt{N_cN_v} &= \sqrt{1.04\times 10^{19}\cdot 6.0\times 10^{18}} = 7.9\times 10^{18}\ \mathrm{cm^{-3}},\\ n_i &= 7.9\times 10^{18}\cdot 2.9\times 10^{-6} = 2.3\times 10^{13}\ \mathrm{cm^{-3}}. \end{aligned}

The measured value is 2.4×1013 cm−32.4\times 10^{13}\ \mathrm{cm^{-3}}; here the agreement is nearly exact.

A difference of merely 0.46 eV0.46\ \mathrm{eV} in EgE_g produces about a factor of 34003400 in the number of free electrons. Such is the power of the exponential. And this difference is part of the answer to “why are modern integrated circuits made of Si rather than Ge?” The current that leaks through a transistor switched OFF is more than three orders of magnitude larger in Ge.

The atomic density of a silicon crystal is 5.0×1022 cm−35.0\times 10^{22}\ \mathrm{cm^{-3}}. With ni=1010 cm−3n_i = 10^{10}\ \mathrm{cm^{-3}}, there is one free electron for every 5×10125\times 10^{12} atoms. Mix in phosphorus at 1016 cm−310^{16}\ \mathrm{cm^{-3}} — one atom in five million — and the free-electron count jumps by a factor of 10610^{6} at a stroke. This is doping, and it is why the semiconductor industry insists on “eleven nines” purity (99.999999999 %). If unintended impurities crept in at 1016 cm−310^{16}\ \mathrm{cm^{-3}}, the entire design would be ruined.

3.4. What stopped miniaturization: tunneling

Section titled “3.4. What stopped miniaturization: tunneling”

A transistor sandwiches a thin insulating film (silicon dioxide SiO2\mathrm{SiO_2}, say) between the gate electrode and the semiconductor, and a voltage on the gate switches the channel beneath it ON and OFF. The thinner the insulator, the better the control, so for forty years the industry made it thinner. Then, in the 2000s, it hit a wall: electrons slip straight through the insulator.

Proposition 3.7(Tunneling transmission through a rectangular barrier)

When a particle of mass mm and energy EE is incident on a rectangular potential barrier of height V0 (>E)V_0\ (> E) and thickness dd, setting

κ=2m(V0−E)ℏ,\kappa = \frac{\sqrt{2m(V_0 - E)}}{\hbar},

the transmission probability TT is, in the regime κd≫1\kappa d \gg 1, approximated by

T≈16 E(V0−E)V02 e−2κd∼e−2κd.T \approx 16\,\frac{E(V_0-E)}{V_0^{2}}\,e^{-2\kappa d} \sim e^{-2\kappa d}.

That is, the transmission falls off exponentially in the thickness dd.

Remark 3.8

The formula is obtained by solving the one-dimensional Schrödinger equation inside and outside the barrier and matching the wave function and its derivative at the boundaries. The essential point is that inside the barrier the wave number becomes purely imaginary, iκi\kappa, so the wave function decays as e−κxe^{-\kappa x}. Derivations appear in Volume V of the Feynman Lectures on Physics and in the tunneling section of any standard quantum mechanics text. In classical mechanics the transmission probability for E<V0E < V_0 is exactly 00, so this is a purely quantum-mechanical effect.

Example 3.9(One nanometer thinner, seventy million times more leakage)

The barrier height seen by an electron at a Si/SiO2\mathrm{Si/SiO_2} interface is V0−E≈3.1 eVV_0 - E \approx 3.1\ \mathrm{eV}. First compute κ\kappa:

2me(V0−E)=2⋅9.109×10−31 kg⋅3.1⋅1.602×10−19 J=9.05×10−49,2me(V0−E)=9.51×10−25 kg m/s,κ=9.51×10−251.0546×10−34=9.02×109 m−1=9.02 nm−1.\begin{aligned} 2m_e(V_0-E) &= 2 \cdot 9.109\times 10^{-31}\ \mathrm{kg} \cdot 3.1 \cdot 1.602\times 10^{-19}\ \mathrm{J} = 9.05\times 10^{-49},\\ \sqrt{2m_e(V_0-E)} &= 9.51\times 10^{-25}\ \mathrm{kg\,m/s},\\ \kappa &= \frac{9.51\times 10^{-25}}{1.0546\times 10^{-34}} = 9.02\times 10^{9}\ \mathrm{m^{-1}} = 9.02\ \mathrm{nm^{-1}}. \end{aligned}

Hence 2κ=18.0 nm−12\kappa = 18.0\ \mathrm{nm^{-1}}, and e−2κde^{-2\kappa d} by thickness is

Oxide thickness dd2κd2\kappa de−2κde^{-2\kappa d}
3.0 nm3.0\ \mathrm{nm}54.154.13×10−243\times 10^{-24}
2.0 nm2.0\ \mathrm{nm}36.136.12×10−162\times 10^{-16}
1.5 nm1.5\ \mathrm{nm}27.127.12×10−122\times 10^{-12}
1.0 nm1.0\ \mathrm{nm}18.018.01.5×10−81.5\times 10^{-8}

Each 1 nm1\ \mathrm{nm} removed multiplies the leakage by e18.0=6.6×107e^{18.0} = 6.6\times 10^{7}, roughly seventy million. Going from 3 nm3\ \mathrm{nm} to 1 nm1\ \mathrm{nm} multiplies it by 101610^{16}.

This is not a metaphor; it is what happened. At 1.2 nm1.2\ \mathrm{nm} — a mere five atomic layers of SiO2\mathrm{SiO_2} — leakage began to dominate power consumption, and the industry gave up on “thinner still”. The move it made instead was to switch to a high-permittivity material (hafnium oxide HfO2\mathrm{HfO_2}, relative permittivity ≈25\approx 25, more than six times the 3.93.9 of SiO2\mathrm{SiO_2}), producing a film that is physically thick but electrically thin. Intel put this into volume production at the 45 nm node in 2007. In other words, your phone contains an answer to a deadline set by the Schrödinger equation.

4. GPS: converting a clock error into meters

Section titled “4. GPS: converting a clock error into meters”

A GPS receiver measures distance from the difference between the transmission time encoded in a satellite’s signal and the time of reception. Radio waves travel at the speed of light, so a timing error Δt\Delta t becomes a distance error c Δtc\,\Delta t:

c×1 ns=2.998×108 m/s×10−9 s=0.30 m.c \times 1\ \mathrm{ns} = 2.998\times 10^{8}\ \mathrm{m/s} \times 10^{-9}\ \mathrm{s} = 0.30\ \mathrm{m}.

One nanosecond is thirty centimeters. To position to within a few meters, the clocks must agree to about ten nanoseconds. But a satellite clock and a ground clock do not fundamentally run at the same rate: the slowing due to velocity (time dilation(Theorem 3.1)[Einstein and Feynman]) and the speeding up due to the difference in gravitational potential (gravitational shift in clock rate(Proposition 5.2)[Einstein and Feynman]) act at the same time. Below we treat both in a single formula.

Definition 4.1(Proper time)

The time actually recorded by a clock moving through spacetime is its proper time τ\tau. In terms of the line element ds2ds^2 written with a coordinate time tt, proper time is defined by

dτ2=−ds2c2d\tau^2 = -\frac{ds^2}{c^2}

(with the sign convention in which ds2<0ds^2 < 0 along a timelike world line). In relativity, “the time a clock records” is always proper time, never coordinate time.

Theorem 4.2(Difference in rate between an orbiting clock and a ground clock)

Approximate the Earth’s gravitational field by the Schwarzschild metric of a mass MM, and neglect the Earth’s rotation and oblateness, the eccentricity of the orbit, and the influence of other bodies. Let τsat\tau_{\mathrm{sat}} be the proper time of a clock on a circular orbit of geocentric radius rr, and τgnd\tau_{\mathrm{gnd}} that of a clock at rest at geocentric radius RR. Then, to first order in the small quantities GM/(rc2)≪1GM/(rc^2) \ll 1 and v2/c2≪1v^2/c^2 \ll 1,

τsat−τgndτgnd≈GMc2(1R−32r).\frac{\tau_{\mathrm{sat}} - \tau_{\mathrm{gnd}}}{\tau_{\mathrm{gnd}}} \approx \frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{3}{2r}\right).

In particular the right-hand side is positive (the satellite clock runs fast) when r>32Rr > \tfrac{3}{2}R, and negative (it runs slow) when r<32Rr < \tfrac{3}{2}R.

Proof(Theorem 4.2)

Write the Schwarzschild metric in spherical coordinates (t,r,θ,φ)(t, r, \theta, \varphi) and restrict to the equatorial plane θ=π/2\theta = \pi/2:

ds2=−(1−2GMrc2)c2dt2+(1−2GMrc2)−1dr2+r2dφ2.ds^{2} = -\left(1 - \frac{2GM}{rc^{2}}\right)c^{2}dt^{2} + \left(1 - \frac{2GM}{rc^{2}}\right)^{-1}dr^{2} + r^{2}d\varphi^{2}.

The satellite. On a circular orbit dr=0dr = 0, so by Definition 4.1

c2dτsat2=(1−2GMrc2)c2dt2−r2dφ2.c^{2}d\tau_{\mathrm{sat}}^{2} = \left(1 - \frac{2GM}{rc^{2}}\right)c^{2}dt^{2} - r^{2}d\varphi^{2}.

Setting the coordinate velocity v=r dφ/dtv = r\,d\varphi/dt and factoring out dt2dt^2,

dτsatdt=1−2GMrc2−v2c2.\frac{d\tau_{\mathrm{sat}}}{dt} = \sqrt{1 - \frac{2GM}{rc^{2}} - \frac{v^{2}}{c^{2}}}.

By hypothesis the correction terms under the root are small compared with 11, so with 1−x≈1−x/2\sqrt{1-x} \approx 1 - x/2 (valid for ∣x∣≪1|x| \ll 1),

dτsatdt≈1−GMrc2−v22c2.\frac{d\tau_{\mathrm{sat}}}{dt} \approx 1 - \frac{GM}{rc^{2}} - \frac{v^{2}}{2c^{2}}.

The ground clock. It is at rest, so dr=dφ=0dr = d\varphi = 0 and

dτgnddt=1−2GMRc2≈1−GMRc2.\frac{d\tau_{\mathrm{gnd}}}{dt} = \sqrt{1 - \frac{2GM}{Rc^{2}}} \approx 1 - \frac{GM}{Rc^{2}}.

Take the ratio. To first order in the small quantities,

dτsatdτgnd≈(1−GMrc2−v22c2)(1+GMRc2)≈1+GMc2(1R−1r)−v22c2.\frac{d\tau_{\mathrm{sat}}}{d\tau_{\mathrm{gnd}}} \approx \left(1 - \frac{GM}{rc^{2}} - \frac{v^{2}}{2c^{2}}\right)\left(1 + \frac{GM}{Rc^{2}}\right) \approx 1 + \frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{1}{r}\right) - \frac{v^{2}}{2c^{2}}.

(The second-order terms are of order 10−1910^{-19} and have been dropped.)

Use the circular-orbit condition. For a circular orbit in the Newtonian approximation, gravity balances the centripetal acceleration, GM/r2=v2/rGM/r^{2} = v^{2}/r, that is v2=GM/rv^{2} = GM/r. Substituting,

dτsatdτgnd≈1+GMc2(1R−1r−12r)=1+GMc2(1R−32r).\frac{d\tau_{\mathrm{sat}}}{d\tau_{\mathrm{gnd}}} \approx 1 + \frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{1}{r} - \frac{1}{2r}\right) = 1 + \frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{3}{2r}\right).

Subtracting 11 from both sides gives the stated formula. The sign statement follows from 1/R−3/(2r)>0  ⟺  r>32R1/R - 3/(2r) > 0 \iff r > \tfrac{3}{2}R.

Example 4.3(GPS satellites: +38.5 μs per day, 11 km per day uncorrected)

A GPS satellite orbits at radius r=2.656×107 mr = 2.656\times 10^{7}\ \mathrm{m} (altitude about 20,200 km20{,}200\ \mathrm{km}); take the ground clock at R=R⊕=6.371×106 mR = R_\oplus = 6.371\times 10^{6}\ \mathrm{m}. First check the orbital speed:

v=GMr=3.986×10142.656×107=1.501×107=3874 m/s,v = \sqrt{\frac{GM}{r}} = \sqrt{\frac{3.986\times 10^{14}}{2.656\times 10^{7}}} = \sqrt{1.501\times 10^{7}} = 3874\ \mathrm{m/s},

about 14,000 km/h14{,}000\ \mathrm{km/h}.

The special-relativistic contribution (slowing due to velocity):

−v22c2=−(3874)22(2.998×108)2=−1.501×1071.798×1017=−8.35×10−11.-\frac{v^{2}}{2c^{2}} = -\frac{(3874)^{2}}{2(2.998\times 10^{8})^{2}} = -\frac{1.501\times 10^{7}}{1.798\times 10^{17}} = -8.35\times 10^{-11}.

Multiplying by one day =86400 s= 86400\ \mathrm{s} gives −8.35×10−11×86400=−7.21×10−6 s-8.35\times 10^{-11} \times 86400 = -7.21\times 10^{-6}\ \mathrm{s}: the clock loses 7.2 μs7.2\ \mu\mathrm{s} per day.

The general-relativistic contribution (gain from sitting in a shallower gravitational potential). Using GM/c2=3.986×1014/8.988×1016=4.435×10−3 mGM/c^{2} = 3.986\times 10^{14}/8.988\times 10^{16} = 4.435\times 10^{-3}\ \mathrm{m},

GMc2(1R−1r)=4.435×10−3(1.5696×10−7−3.765×10−8)=5.29×10−10.\frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{1}{r}\right) = 4.435\times 10^{-3}\left(1.5696\times 10^{-7} - 3.765\times 10^{-8}\right) = 5.29\times 10^{-10}.

Over a day this is 5.29×10−10×86400=4.57×10−5 s5.29\times 10^{-10}\times 86400 = 4.57\times 10^{-5}\ \mathrm{s}: the clock gains 45.7 μs45.7\ \mu\mathrm{s} per day.

The total (using Theorem 4.2 directly gives the same answer):

4.435×10−3(1.5696×10−7−1.52.656×107)=4.435×10−3×1.0049×10−7=4.457×10−10,4.435\times 10^{-3}\left(1.5696\times 10^{-7} - \frac{1.5}{2.656\times 10^{7}}\right) = 4.435\times 10^{-3} \times 1.0049\times 10^{-7} = 4.457\times 10^{-10},4.457×10−10×86400 s=3.85×10−5 s=38.5 μs (gained, per day).4.457\times 10^{-10}\times 86400\ \mathrm{s} = 3.85\times 10^{-5}\ \mathrm{s} = 38.5\ \mu\mathrm{s}\ \text{(gained, per day)}.

Convert to distance. c×38.5 μs=2.998×108×3.85×10−5=1.15×104 mc \times 38.5\ \mu\mathrm{s} = 2.998\times 10^{8}\times 3.85\times 10^{-5} = 1.15\times 10^{4}\ \mathrm{m}. Neglect the correction and the positioning error piles up at about 11 km11\ \mathrm{km} per day. It would take less than half a day for your car navigation to announce that you are in the next prefecture.

In practice this correction is made before launch. The reference frequency of the atomic clock carried by the satellite is offset slightly from its nominal ground value of 10.23 MHz10.23\ \mathrm{MHz} and set to 10.22999999543 MHz10.22999999543\ \mathrm{MHz}. The relative offset is

10.23−10.2299999954310.23=4.4647×10−10,\frac{10.23 - 10.22999999543}{10.23} = 4.4647\times 10^{-10},

and ×86400 s=38.6 μs\times 86400\ \mathrm{s} = 38.6\ \mu\mathrm{s}, agreeing with our hand-computed 38.5 μs38.5\ \mu\mathrm{s} to within 0.3 % (the difference comes from neglecting the Earth’s rotation and oblateness). A clock that becomes correct only once it reaches orbit is built on the ground and launched. The same 38 μs38\ \mu\mathrm{s}, obtained by setting up the special-relativistic and gravitational effects separately, is computed in Example 5.3[Einstein and Feynman].

The two effects on a GPS satellite clock, and their net balance

Remark 4.4

The sign condition r=32Rr = \tfrac{3}{2}R in Theorem 4.2 corresponds to an altitude of 32×6371−6371=3186 km\tfrac{3}{2}\times 6371 - 6371 = 3186\ \mathrm{km}. Below that, the velocity effect beats the gravitational one and the clock runs slow. For the International Space Station (altitude about 400 km400\ \mathrm{km}, r=6.771×106 mr = 6.771\times 10^{6}\ \mathrm{m}),

4.435×10−3(1.5696×10−7−1.56.771×106)=−2.86×10−10,4.435\times 10^{-3}\left(1.5696\times 10^{-7} - \frac{1.5}{6.771\times 10^{6}}\right) = -2.86\times 10^{-10},

which is −2.47×10−5 s=−24.7 μs-2.47\times 10^{-5}\ \mathrm{s} = -24.7\ \mu\mathrm{s} per day, about 0.009 s0.009\ \mathrm{s} per year. Astronauts do come back marginally younger than the rest of us — by a hundredth of a second a year. Rip Van Winkle they are not.

The proton (the nucleus of hydrogen) has spin 1/21/2 and with it a magnetic moment. Put a magnet in a magnetic field and it tries to align; for a quantum-mechanical spin, what appears is not an alignment of “direction” but a splitting of energy levels.

Definition 5.1(Zeeman splitting and the Larmor frequency)

Place a spin-1/21/2 nucleus of gyromagnetic ratio γ\gamma in a static magnetic field B0B_0. Its energy level splits in two, with separation

ΔE=γℏB0\Delta E = \gamma \hbar B_0

(Zeeman splitting). By Definition 2.1, the frequency of the radiation that drives transitions between these two levels is

fL=ΔEh=γB02π,f_L = \frac{\Delta E}{h} = \frac{\gamma B_0}{2\pi},

called the Larmor frequency. For the proton, γ/2π=42.577 MHz/T\gamma/2\pi = 42.577\ \mathrm{MHz/T}.

Proposition 5.2(Larmor frequencies in clinical MRI)

With the proton gyromagnetic ratio γ/2π=42.577 MHz/T\gamma/2\pi = 42.577\ \mathrm{MHz/T}, the Larmor frequencies for static fields B0=1.5 TB_0 = 1.5\ \mathrm{T} and 3.0 T3.0\ \mathrm{T} are

fL(1.5 T)=63.87 MHz,fL(3.0 T)=127.7 MHzf_L(1.5\ \mathrm{T}) = 63.87\ \mathrm{MHz}, \qquad f_L(3.0\ \mathrm{T}) = 127.7\ \mathrm{MHz}

respectively.

Proof(Proposition 5.2)

Substitute into fL=(γ/2π)B0f_L = (\gamma/2\pi) B_0 from Definition 5.1:

fL(1.5 T)=42.577 MHz/T×1.5 T=63.866 MHz,f_L(1.5\ \mathrm{T}) = 42.577\ \mathrm{MHz/T} \times 1.5\ \mathrm{T} = 63.866\ \mathrm{MHz},fL(3.0 T)=42.577 MHz/T×3.0 T=127.73 MHz.f_L(3.0\ \mathrm{T}) = 42.577\ \mathrm{MHz/T} \times 3.0\ \mathrm{T} = 127.73\ \mathrm{MHz}.

63.9 MHz63.9\ \mathrm{MHz} and 127.7 MHz127.7\ \mathrm{MHz}: FM radio in Japan broadcasts between 7676 and 95 MHz95\ \mathrm{MHz}, so MRI works with radio waves right next door to FM. That is why an MRI room is wrapped in a thick radio-frequency shield — to keep outside broadcasts from showing up in the image as noise.

5.2. What is visible is five parts in a million

Section titled “5.2. What is visible is five parts in a million”

Here is where MRI becomes strange. Compare the size of the Zeeman splitting with the thermal energy at room temperature.

Proposition 5.3(Thermal-equilibrium polarization of nuclear spins)

For an ensemble of spin-1/21/2 nuclei in thermal equilibrium at field B0B_0 and temperature TT, the relative difference between the population N+N_+ of the lower level and the population N−N_- of the upper level (the polarization) is

P=N+−N−N++N−=tanh⁡ ⁣(ΔE2kBT)≈ΔE2kBT=γℏB02kBT(ΔE≪kBT).P = \frac{N_+ - N_-}{N_+ + N_-} = \tanh\!\left(\frac{\Delta E}{2k_B T}\right) \approx \frac{\Delta E}{2k_B T} = \frac{\gamma \hbar B_0}{2 k_B T} \qquad (\Delta E \ll k_B T).
Proof(Proposition 5.3)

In thermal equilibrium the populations follow the Boltzmann distribution, N−/N+=e−ΔE/kBTN_-/N_+ = e^{-\Delta E/k_BT}. Setting x=ΔE/(2kBT)x = \Delta E/(2k_BT) we may write N+∝exN_+ \propto e^{x} and N−∝e−xN_- \propto e^{-x}, so

P=ex−e−xex+e−x=tanh⁡x.P = \frac{e^{x} - e^{-x}}{e^{x} + e^{-x}} = \tanh x.

For ∣x∣≪1|x| \ll 1 we have tanh⁡x=x−x3/3+⋯≈x\tanh x = x - x^3/3 + \cdots \approx x, hence P≈ΔE/(2kBT)P \approx \Delta E/(2k_BT). Substituting ΔE=γℏB0\Delta E = \gamma\hbar B_0 from Definition 5.1 gives the claim.

Example 5.4(At body temperature and 1.5 T, the imbalance is five per million)

Take B0=1.5 TB_0 = 1.5\ \mathrm{T} and body temperature T=310 KT = 310\ \mathrm{K}. Putting fL=63.87 MHzf_L = 63.87\ \mathrm{MHz} from Proposition 5.2 into ΔE=hfL\Delta E = h f_L from Definition 5.1,

ΔE=6.626×10−34 J s×6.387×107 Hz=4.232×10−26 J.\Delta E = 6.626\times 10^{-34}\ \mathrm{J\,s} \times 6.387\times 10^{7}\ \mathrm{Hz} = 4.232\times 10^{-26}\ \mathrm{J}.

The thermal energy at body temperature, meanwhile, is

kBT=1.3806×10−23×310=4.280×10−21 J.k_B T = 1.3806\times 10^{-23} \times 310 = 4.280\times 10^{-21}\ \mathrm{J}.

By Proposition 5.3,

P≈4.232×10−262×4.280×10−21=4.94×10−6.P \approx \frac{4.232\times 10^{-26}}{2\times 4.280\times 10^{-21}} = 4.94\times 10^{-6}.

So out of a million protons, only about five are polarized on balance. The remaining 99.9995 % cancel one another out and contribute nothing to the signal.

Imaging is nonetheless possible because the numbers are enormous. The number of protons in 1 mm31\ \mathrm{mm}^3 of water (mass 1 mg1\ \mathrm{mg}) is

1×10−3 g18 g/mol×2×6.022×1023=6.7×1019\frac{1\times 10^{-3}\ \mathrm{g}}{18\ \mathrm{g/mol}} \times 2 \times 6.022\times 10^{23} = 6.7\times 10^{19}

(the factor 22 because each H2O\mathrm{H_2O} molecule carries two hydrogens). Of these, the net polarized number is

6.7×1019×4.94×10−6=3.3×1014.6.7\times 10^{19} \times 4.94\times 10^{-6} = 3.3\times 10^{14}.

That is 330 trillion per 1 mm31\ \mathrm{mm}^3 — quite enough for a strong signal.

Note also that P∝B0P \propto B_0 in Proposition 5.3 means a 3 T3\ \mathrm{T} machine has twice the polarization of a 1.5 T1.5\ \mathrm{T} one. This is the reason for the push to higher fields (and since receiver sensitivity also rises with frequency, the actual improvement in signal-to-noise ratio is larger still).

5.3. How do we know where the signal came from?

Section titled “5.3. How do we know where the signal came from?”

We now know that hydrogen inside the body emits radio waves. But to make a picture we must distinguish which position a signal came from. The answer is to make the Larmor frequency itself depend on position.

Superimpose on the static field a gradient field GG (units T/m\mathrm{T/m}) whose strength varies in proportion to position. By Definition 5.1, the resonance frequency at position xx becomes

f(x)=γ2π(B0+Gx),f(x) = \frac{\gamma}{2\pi}\left(B_0 + G x\right),

so frequency and position are in one-to-one correspondence. Fourier transform the received signal into its frequency components and what you get is exactly the spatial distribution — the central idea of MRI, found independently by Lauterbur and Mansfield in 1973 and recognized by the 2003 Nobel Prize in Physiology or Medicine.

Example 5.5(With a 10 mT/m gradient, 1 mm is 426 Hz)

Take G=10 mT/m=1.0×10−2 T/mG = 10\ \mathrm{mT/m} = 1.0\times 10^{-2}\ \mathrm{T/m}. A displacement of Δx=1 mm=1.0×10−3 m\Delta x = 1\ \mathrm{mm} = 1.0\times 10^{-3}\ \mathrm{m} shifts the resonance frequency by

Δf=γ2πGΔx=42.577×106 Hz/T×1.0×10−2 T/m×1.0×10−3 m=425.8 Hz.\Delta f = \frac{\gamma}{2\pi} G \Delta x = 42.577\times 10^{6}\ \mathrm{Hz/T} \times 1.0\times 10^{-2}\ \mathrm{T/m} \times 1.0\times 10^{-3}\ \mathrm{m} = 425.8\ \mathrm{Hz}.

Conversely, measuring frequency to a resolution of 426 Hz426\ \mathrm{Hz} fixes position to a resolution of 1 mm1\ \mathrm{mm}. Relative to the 63.87 MHz63.87\ \mathrm{MHz} carrier, 426 Hz426\ \mathrm{Hz} is 6.7×10−66.7\times 10^{-6} — again a precision of one part in a million. This is why the static field of an MRI scanner is held uniform to a few ppm across the whole imaging volume.

Incidentally, with a receiver bandwidth of ±32 kHz\pm 32\ \mathrm{kHz} the field of view is

2×32000 Hz42.577×106×1.0×10−2 Hz/m=640004.258×105=0.150 m=15 cm.\frac{2\times 32000\ \mathrm{Hz}}{42.577\times 10^{6}\times 1.0\times 10^{-2}\ \mathrm{Hz/m}} = \frac{64000}{4.258\times 10^{5}} = 0.150\ \mathrm{m} = 15\ \mathrm{cm}.

Imaging a head therefore calls for a somewhat weaker gradient or a wider bandwidth — and so on: every setting of the machine is tied together by this one equation.

Image contrast — the fact that white and gray matter in the brain appear in different shades — comes less from the number of hydrogen nuclei than from how fast the excited spins return to equilibrium: the longitudinal relaxation time T1T_1 and the transverse relaxation time T2T_2 differ from tissue to tissue. Since these are set by the motional state of the water molecules and their interaction with the surrounding macromolecules, MRI sees not only “where the hydrogen is” but “what kind of environment the hydrogen is in”.

Set them side by side once more.

Phone (semiconductors)GPSMRI
Central theoryquantum mechanics (band theory, tunneling)special and general relativityquantum mechanics (nuclear spin) + statistical mechanics
Energy difference ΔE\Delta Eband gap ≈1 eV\approx 1\ \mathrm{eV}Cs-133 hyperfine structure ≈4×10−5 eV\approx 4\times 10^{-5}\ \mathrm{eV}Zeeman splitting ≈2.6×10−7 eV\approx 2.6\times 10^{-7}\ \mathrm{eV}
Corresponding frequency≈1014 Hz\approx 10^{14}\ \mathrm{Hz} (infrared to visible)9.192631770 GHz9.192631770\ \mathrm{GHz} (microwave)6.4×107 Hz6.4\times 10^{7}\ \mathrm{Hz} (VHF)
Decisive numbere−Eg/2kBTe^{-E_g/2k_BT}, e−2κde^{-2\kappa d}38.5 μs38.5\ \mu\mathrm{s} per daypolarization 5×10−65\times 10^{-6}
Theory to application1928 (Bloch) → 1947 (transistor)1915 (general relativity) → 1978 (first GPS satellite)1946 (NMR) → 1977 (human imaging)

Running through all three columns is E=hfE = hf from Definition 2.1. In a semiconductor the band gap sets the color of the light; in MRI the splitting of a nuclear spin sets the radio frequency; and in the atomic clocks of GPS — this is the mildly startling part — the statement that the hyperfine transition of the ground state of cesium-133 has frequency 9 192 631 770 Hz9\,192\,631\,770\ \mathrm{Hz} has been the definition of the second itself since 1967 (a definition retained after the 2019 revision of the SI). Our unit of time is an atomic energy difference read through E=hfE = hf.

The other thing they share is exponentials and a feeling for orders of magnitude. Semiconductor performance is set by the contest between two exponentials, e−Eg/2kBTe^{-E_g/2k_BT} and e−2κde^{-2\kappa d}; GPS cannot ignore a relative error of 10−1010^{-10}; MRI picks up an imbalance of 10−610^{-6}. The “approximations” and “order-of-magnitude estimates” of a high-school textbook are working tools used daily in exactly these situations.

For all this practical success, physics is not finished. The performance limits of semiconductors, room-temperature superconductivity, error correction for quantum computers, and the unification of gravity with quantum theory (for the scale on which both matter, see Planck units(Definition 6.1)[Unsolved Problems in Physics]) — the open problems are collected in unsolved problems in physics. Whatever today’s phone would have been to a physicist of 1900, the same thing is surely happening again by 2120.

Exercise 7.1Easy

A green LED emits at about 530 nm530\ \mathrm{nm}. What is the band gap of its semiconductor, in eV? And can you light such a material by connecting a single 1.5 V1.5\ \mathrm{V} dry cell directly across it? Give your reasoning.

Solution

By Proposition 3.2, Eg=1239.84/λ [nm]E_g = 1239.84/\lambda\,[\mathrm{nm}], so

Eg=1239.84530=2.34 eV.E_g = \frac{1239.84}{530} = 2.34\ \mathrm{eV}.

You cannot light it. An electron crossing a potential difference VV gains energy eVeV, so a 1.5 V1.5\ \mathrm{V} cell supplies only 1.5 eV1.5\ \mathrm{eV}. Emitting one photon requires Eg=2.34 eVE_g = 2.34\ \mathrm{eV}, as used in the derivation of Proposition 3.2, so a forward voltage of at least 2.34 V2.34\ \mathrm{V} is needed. Indeed the forward voltage of a green LED is around 2.02.0 to 3.0 V3.0\ \mathrm{V}, higher than a red LED (about 1.8 V1.8\ \mathrm{V}) and lower than a blue or white one (about 3.03.0 to 3.4 V3.4\ \mathrm{V}). LED forward voltages differ by color precisely because the band gaps differ.

Exercise 7.2Standard

An atomic clock is placed on a geostationary satellite (orbital radius r=4.2164×107 mr = 4.2164\times 10^{7}\ \mathrm{m}). By how many microseconds per day does it drift relative to a clock on the ground, and does it run fast or slow? Use GM/c2=4.435×10−3 mGM/c^{2} = 4.435\times 10^{-3}\ \mathrm{m} and R⊕=6.371×106 mR_\oplus = 6.371\times 10^{6}\ \mathrm{m}.

Solution

Apply Theorem 4.2 directly (a geostationary orbit is circular with essentially zero eccentricity, so the hypotheses hold). First the bracket:

1R=16.371×106=1.5696×10−7 m−1,\frac{1}{R} = \frac{1}{6.371\times 10^{6}} = 1.5696\times 10^{-7}\ \mathrm{m^{-1}},32r=1.54.2164×107=3.5578×10−8 m−1,\frac{3}{2r} = \frac{1.5}{4.2164\times 10^{7}} = 3.5578\times 10^{-8}\ \mathrm{m^{-1}},1R−32r=1.5696×10−7−3.5578×10−8=1.2138×10−7 m−1.\frac{1}{R} - \frac{3}{2r} = 1.5696\times 10^{-7} - 3.5578\times 10^{-8} = 1.2138\times 10^{-7}\ \mathrm{m^{-1}}.

Multiplying by GM/c2GM/c^{2},

GMc2(1R−32r)=4.435×10−3×1.2138×10−7=5.384×10−10.\frac{GM}{c^{2}}\left(\frac{1}{R} - \frac{3}{2r}\right) = 4.435\times 10^{-3} \times 1.2138\times 10^{-7} = 5.384\times 10^{-10}.

The value is positive, so the clock runs fast (consistent with the sign condition in Theorem 4.2: r=4.2164×107>32R=9.56×106r = 4.2164\times 10^{7} > \tfrac{3}{2}R = 9.56\times 10^{6}). Per day,

5.384×10−10×86400 s=4.65×10−5 s=46.5 μs.5.384\times 10^{-10}\times 86400\ \mathrm{s} = 4.65\times 10^{-5}\ \mathrm{s} = 46.5\ \mu\mathrm{s}.

This exceeds the 38.5 μs38.5\ \mu\mathrm{s} of a GPS satellite, because a higher orbit means a larger gravitational effect (the gain) and a lower speed, hence a smaller special-relativistic effect (the loss).

Exercise 7.3Standard

For an MRI scanner with B0=3.0 TB_0 = 3.0\ \mathrm{T}, find the following.

(1) The proton polarization PP at body temperature T=310 KT = 310\ \mathrm{K}. (2) The net polarized number of protons in 1 mm31\ \mathrm{mm}^{3} of water. (3) The frequency resolution required to achieve a spatial resolution of 0.5 mm0.5\ \mathrm{mm} with a gradient field G=20 mT/mG = 20\ \mathrm{mT/m}.

Solution

(1) By Proposition 5.2, fL(3.0 T)=127.73 MHzf_L(3.0\ \mathrm{T}) = 127.73\ \mathrm{MHz}, so from ΔE=hfL\Delta E = h f_L in Definition 5.1,

ΔE=6.626×10−34×1.2773×108=8.464×10−26 J.\Delta E = 6.626\times 10^{-34}\times 1.2773\times 10^{8} = 8.464\times 10^{-26}\ \mathrm{J}.

The thermal energy at body temperature is kBT=1.3806×10−23×310=4.280×10−21 Jk_BT = 1.3806\times 10^{-23}\times 310 = 4.280\times 10^{-21}\ \mathrm{J}. Since ΔE≪kBT\Delta E \ll k_BT (the ratio is about 2×10−52\times 10^{-5}), the approximation in Proposition 5.3 applies and

P≈8.464×10−262×4.280×10−21=9.89×10−6,P \approx \frac{8.464\times 10^{-26}}{2\times 4.280\times 10^{-21}} = 9.89\times 10^{-6},

about 10−510^{-5}, or roughly ten per million. This is exactly twice the 1.5 T1.5\ \mathrm{T} value of Example 5.4, consistent with P∝B0P \propto B_0 in Proposition 5.3.

(2) As in Example 5.4, 1 mm31\ \mathrm{mm}^{3} of water contains 6.7×10196.7\times 10^{19} protons, so

6.7×1019×9.89×10−6=6.6×1014.6.7\times 10^{19}\times 9.89\times 10^{-6} = 6.6\times 10^{14}.

(3) The same computation as Example 5.5:

Δf=γ2πG Δx=42.577×106×2.0×10−2×0.5×10−3=425.8 Hz.\Delta f = \frac{\gamma}{2\pi}G\,\Delta x = 42.577\times 10^{6}\times 2.0\times 10^{-2}\times 0.5\times 10^{-3} = 425.8\ \mathrm{Hz}.

Doubling the gradient makes half the distance correspond to the same frequency difference. Stronger gradients buy finer resolution: that is the basic design principle of MRI. (In practice there is a limit, because rapidly switched gradients stimulate peripheral nerves.)

  • S. M. Sze and K. K. Ng, Physics of Semiconductor Devices, 3rd ed., Wiley, 2007 — Chapter 1 (crystal structure and band theory) and Chapter 4 (the MOS capacitor). The numerical values for intrinsic carrier densities and effective densities of states follow the tables in this book.
  • C. Kittel, Kotai Butsurigaku Nyumon (Introduction to Solid State Physics, 8th ed.), Maruzen, 2005 (in Japanese) — Chapters 7 and 8 (energy bands and semiconductor crystals).
  • R. P. Feynman, R. B. Leighton and M. Sands, Feynman Butsurigaku V: Ryoshi Rikigaku (The Feynman Lectures on Physics, Vol. V: Quantum Mechanics), Iwanami Shoten (in Japanese) — the chapters on tunneling and on two-level systems.
  • N. Ashby, “Relativity in the Global Positioning System”, Living Reviews in Relativity 6 (2003), article 1. doi:10.12942/lrr-2003-1 — the standard review of relativistic effects in GPS, including the discussion of the reference-frequency offset.
  • E. M. Haacke, R. W. Brown, M. R. Thompson and R. Venkatesan, Magnetic Resonance Imaging: Physical Principles and Sequence Design, Wiley, 1999 — the basics of nuclear magnetic resonance, spatial encoding by gradient fields, and relaxation times.
  • BIPM, The International System of Units (SI), 9th edition, 2019 — https://www.bipm.org/en/publications/si-brochure — the definition of the second (the cesium-133 hyperfine transition frequency 9 192 631 770 Hz9\,192\,631\,770\ \mathrm{Hz}).
  • NIST, CODATA Internationally Recommended Values of the Fundamental Physical Constants — https://physics.nist.gov/cuu/Constants/ — the source of the values of hh, kBk_B, mem_e and the proton gyromagnetic ratio used above.

Appendix: Where the numbers come from, and what to watch for

Section titled “Appendix: Where the numbers come from, and what to watch for”

What the GPS calculation ignores. In Theorem 4.2 we neglected the Earth’s rotation. The surface at the equator moves at about 465 m/s465\ \mathrm{m/s}, so the ground clock too is slowed, by −v2/2c2=−1.2×10−12-v^2/2c^2 = -1.2\times 10^{-12} (that is −0.10 μs-0.10\ \mu\mathrm{s} per day). Including this increases the satellite’s relative gain by about 0.1 μs0.1\ \mu\mathrm{s}. Furthermore, since the Earth is not a perfect sphere, operational practice expands the gravitational potential in spherical harmonics and uses a coordinate system fixed to the rotating Earth (defined so that clocks on the geoid all run at the same rate). The rigorous treatment is in Ashby’s review. Periodic variations from orbital eccentricity (for GPS, e≈0.02e \approx 0.02 or less) are handled at the receiver as a correction term of the form −2GMa esin⁡E/c2-2\sqrt{GMa}\,e\sin E/c^2.

On the semiconductor numbers. The effective densities of states Nc,NvN_c, N_v are computed from density-of-states effective masses and differ by a few percent between sources. The factor-of-1.5 discrepancy for silicon in Example 3.6 comes from this uncertainty together with our neglect of the slight shrinking of the band gap with temperature (about −2.7×10−4 eV/K-2.7\times 10^{-4}\ \mathrm{eV/K} for Si near 300 K300\ \mathrm{K}). For order-of-magnitude estimates the accuracy is ample. As for the tunneling transmission, Proposition 3.7 idealizes the barrier as rectangular; a real gate insulator requires accounting for the tilt of the barrier under the applied field (Fowler–Nordheim tunneling) and for interface states. The conclusion “exponential in the thickness” is unaffected.

On the MRI polarization. Proposition 5.3 assumes thermal equilibrium. Recent hyperpolarization techniques polarize nuclear spins strongly by artificial means before introducing them into the body, reaching a few percent polarization — more than ten thousand times the thermal-equilibrium value — with 129^{129}Xe or 13^{13}C. Hyperpolarized xenon MRI, which images the airways of the lung directly, is entering clinical use. The figure 10−610^{-6} should be understood as conditional on thermal equilibrium.

not audited

Report an error in this article ・Operated by: Mugen Giken LLC ・Pricing ・Terms ・Legal notice

© 2026 夢現技研合同会社 ・Code samples are MIT licensed.