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A cavity-QED platform places a quantum emitter in a selected resonator mode and engineers both the coherent interaction and the channels through which energy and information leave. The physical platform is not specified by a Jaynes–Cummings Hamiltonian alone. It also contains:

  • a resonator geometry and polarization structure;
  • an emitter source, trap, or trajectory;
  • state preparation and frequency control;
  • spatial and angular overlap with the vacuum field;
  • useful ports and parasitic loss;
  • cavity and emitter stabilization;
  • a receiver chain; and
  • a calibration model connecting detector records to intracavity dynamics.

The same symbols gg, κ\kappa, and γ\gamma can describe a neutral atom between macroscopic mirrors, an ion in a fiber cavity, a Rydberg atom crossing a superconducting microwave resonator, or an emitter near a photonic-crystal defect. The apparatus needed to realize and infer those rates is radically different in each case.

Required background. Cavity QED derives the light–matter response; optical cavities supplies resonator modes; input–output theory supplies port amplitudes; optical dipole traps supplies emitter confinement. Fabricated superconducting emitters are treated in circuit QED.

Throughout this page,

κ=∑jκj+κint\kappa = \sum_j\kappa_j +\kappa_{\mathrm{int}}

is the cavity energy-decay rate. The intracavity photon number decays as e−κte^{-\kappa t}, the field amplitude decays as e−κt/2e^{-\kappa t/2}, and

κ2π\frac{\kappa}{2\pi}

is the full width at half maximum of an isolated empty-cavity power resonance. The emitter population-decay rate outside the selected cavity channel is γ\gamma, while pure dephasing is γϕ\gamma_\phi. Its optical coherence rate is

γ⊥=γ2+γϕ.\gamma_\perp = \frac{\gamma}{2} +\gamma_\phi.

The rate dictionary must be restated when comparing experiments. Some authors call the cavity field-amplitude decay rate κ\kappa, or use γ\gamma for an atomic half width. Dimensionless numbers agree only after those definitions are translated.

For one designated output port,

ηesc=κuseκ\eta_{\mathrm{esc}} = \frac{\kappa_{\mathrm{use}}}{\kappa}

is the escape fraction conditional on a photon already occupying the cavity mode. It is not the mode-matching efficiency into the cavity, the emitter-to-cavity branching probability, propagation efficiency, or detector efficiency.

From Emitter Preparation to Detected Photons

Section titled “From Emitter Preparation to Detected Photons”

A useful cavity-QED experiment can be represented as

source⟶emitter⟷cavity⟶port⟶receiver.\text{source} \longrightarrow \text{emitter} \longleftrightarrow \text{cavity} \longrightarrow \text{port} \longrightarrow \text{receiver}.

Each arrow has its own state space and efficiency. For a generated photon, one possible end-to-end accounting is

Pclick=PprepPemitβcavηescηpathηdet,P_{\mathrm{click}} = P_{\mathrm{prep}} P_{\mathrm{emit}} \beta_{\mathrm{cav}} \eta_{\mathrm{esc}} \eta_{\mathrm{path}} \eta_{\mathrm{det}},

where the factors are conditional in sequence:

  • PprepP_{\mathrm{prep}} prepares the emitter and motional state;
  • PemitP_{\mathrm{emit}} completes the intended control protocol;
  • βcav\beta_{\mathrm{cav}} sends the photon into the selected cavity mode;
  • ηesc\eta_{\mathrm{esc}} sends it through the useful port;
  • ηpath\eta_{\mathrm{path}} transmits it through filters, fibers, and optics; and
  • ηdet\eta_{\mathrm{det}} converts the arriving photon into an accepted record.

For these sequential conditional events, the product is the probability chain rule and does not require independence. It fails if one substitutes unconditional efficiencies from different spectral or motional ensembles. For coherent protocols with reabsorption, the event “entered the cavity” need not define an irreversible intermediate step; integrate output flux instead.

Two opposing mirrors form the most direct optical cavity-QED architecture. Its strengths are:

  • an open mode volume that can be loaded with neutral atoms, ions, molecules, ensembles, or solid-state samples;
  • well-understood Gaussian modes and polarization control;
  • independent input and output ports;
  • access for trapping, cooling, and control beams; and
  • high finesse with low-loss dielectric coatings.

For a weakly dispersive linear cavity of one-way group optical length LoptL_{\mathrm{opt}} (including mirror group delay where relevant),

νFSR≈c2Lopt,\nu_{\mathrm{FSR}} \approx \frac{c}{2L_{\mathrm{opt}}},

and, for an isolated high-finesse resonance,

κ2π=δνcav≈νFSRF.\frac{\kappa}{2\pi} = \delta\nu_{\mathrm{cav}} \approx \frac{\nu_{\mathrm{FSR}}}{\mathcal F}.

The approximate standing-wave mode volume

V∼πw02Lphys4V \sim \frac{\pi w_0^2L_{\mathrm{phys}}}{4}

shows why short cavities and small waists raise the vacuum field. This estimate assumes a paraxial vacuum standing mode with slowly varying waist; cavity QED explains energy normalization and the limits of a closed-mode volume.

Open access brings engineering costs:

  • cavity length noise directly becomes detuning noise;
  • mirrors constrain optical access and trap geometry;
  • intracavity traps can shift the emitter and cavity coatings can charge;
  • transverse modes can approach the working resonance;
  • atomic motion samples the standing wave; and
  • mirror transmission must be balanced against absorption and scatter.

High finesse is useful only if the cavity can be locked without injecting unacceptable photons, heating, or differential Stark shifts during the quantum sequence.

Laser-machined concave structures on fiber facets can produce short cavities with small waists while coupling naturally to fiber modes. They are attractive when compactness and a large gg matter.

The small geometry makes the following effects consequential:

  • overlap between the cavity eigenmode and the fiber guided mode;
  • asymmetric mirror transmissions chosen for a preferred port;
  • coating loss and scattering on small curved surfaces;
  • birefringence and polarization-mode splitting;
  • dielectric charging near trapped ions or atoms;
  • limited side access;
  • mechanical and thermal stability of the fiber mounts; and
  • contamination or damage under vacuum.

The small geometric mode volume is a maximum-coupling statement. Realized performance still depends on placing and cooling the emitter at the correct standing-wave antinode.

Photonic-band-gap defects can confine optical fields to wavelength-scale volumes and route output directly into a waveguide. This can produce a large vacuum field without extreme photon storage time.

Important departures from an open Fabry–Pérot cavity are:

  • the emitter samples a strongly varying near field;
  • polarization can vary within the mode;
  • surfaces are close enough to create Casimir–Polder forces, charging, heating, or spectral shifts;
  • fabrication disorder changes resonance frequency, quality factor, and port coupling;
  • the cavity may be one-sided only after waveguide and intrinsic losses are separated; and
  • quasinormal-mode normalization may be needed in an open or dispersive structure.

For trapped atoms, the nanostructure must be integrated with a stable near-surface trap. For solid-state emitters, implantation position, dipole orientation, spectral diffusion, phonon sidebands, and inhomogeneous fabrication spread replace atomic loading as dominant challenges.

Total internal reflection confines traveling-wave modes around a dielectric boundary. Atoms or other emitters couple to the evanescent field. Advantages include high quality factor, small effective mode volume, and natural waveguide or fiber coupling.

Real devices often support clockwise and counterclockwise modes. Surface roughness couples them and produces standing-wave doublets. An apparent spectral splitting can therefore arise from cavity backscattering before an emitter is introduced. Empty-cavity polarization and direction-mode spectra are essential controls.

Optical architecture Principal strength Typical dominant constraint Essential calibration
Macroscopic Fabry–Pérot Open access and high finesse Length noise and moderate mode volume Ringdown, waist, mirror transmissions
Fiber Fabry–Pérot Small volume and direct fiber interface Birefringence, access, coating loss Fiber mode matching and polarization splitting
Photonic crystal Wavelength-scale volume and integration Surface physics and fabrication disorder Local field map and waveguide loss
Whispering-gallery or ring High QQ with evanescent access Counterpropagating-mode coupling Empty-cavity doublet and external coupling

No row is uniformly best. The right objective may be coherent swaps, single-pass extinction, high photon extraction, long emitter coherence, parallel fabrication, or optical-network compatibility.

Why Rydberg atoms compensate for long wavelength

Section titled “Why Rydberg atoms compensate for long wavelength”

Microwave modes occupy much larger physical volumes than optical modes, so their zero-point electric field is smaller. Highly excited Rydberg atoms compensate through:

  • electric-dipole matrix elements that grow strongly with principal quantum number;
  • long radiative lifetimes;
  • adjacent transitions in the microwave domain; and
  • state-selective field ionization after the atom leaves the cavity.

In traditional microwave cavity QED, circular Rydberg atoms cross a superconducting cavity one by one. Their coupling is time dependent,

g(t)=g0u[r(t)]Cang(t),g(t) = g_0 u[\mathbf r(t)] C_{\mathrm{ang}}(t),

and the interaction pulse area is controlled by velocity, trajectory, Stark tuning, and the spatial mode.

The atom is both quantum system and probe. Ramsey zones before and after the cavity can convert a photon-number-dependent phase into an atomic-state probability without absorbing the photon.

The mean thermal occupation of a mode at angular frequency ωc\omega_c and temperature TT is

nˉth=1exp⁡(ℏωc/kBT)−1.\bar n_{\mathrm{th}} = \frac{1}{ \exp(\hbar\omega_c/k_BT)-1 }.

At optical frequency, room-temperature thermal occupation is negligible. At microwave frequency it is an experimental variable.

For

ωc2π=51 GHz,\frac{\omega_c}{2\pi} = 51\,\mathrm{GHz},

the quantum energy corresponds to

ℏωckB=2.45 K.\frac{\hbar\omega_c}{k_B} = 2.45\,\mathrm K.

Therefore,

nˉth≈{0.049,T=0.80 K,1.19,T=4.0 K,122,T=300 K.\bar n_{\mathrm{th}} \approx \begin{cases} 0.049, & T=0.80\,\mathrm K,\\ 1.19, & T=4.0\,\mathrm K,\\ 122, & T=300\,\mathrm K. \end{cases}

A cryogenic enclosure, low-emissivity apertures, and thermal filtering are part of state preparation. Measuring the empty-cavity photon statistics is stronger evidence than inferring temperature from a cryostat sensor.

Long photon storage compared with transit time allows several atoms to probe the same field. Off-resonant interactions imprint a photon-number-dependent Ramsey phase while suppressing actual photon exchange. Finite detuning, thermal photons, and atomic velocity spread limit how closely this realizes a nondemolition measurement (Raimond, Brune, and Haroche).

Useful photon escape versus output coupling, compared with escape fraction and the eliminated-cavity estimate.

Opening the useful port increases its fraction of cavity loss, but eventually reduces emission into the cavity. The solid curve is the exact probability for a resonant initially excited two-level emitter with no pure dephasing; the dashed curve eliminates the cavity. Rates are (g,γ,κloss)/(2π)=(12,3,4) MHz(g,\gamma,\kappa_{\mathrm{loss}})/(2\pi)=(12,3,4)\,\mathrm{MHz}. The maximum of the solid curve is at κuse/(2π)≃37.0 MHz\kappa_{\mathrm{use}}/(2\pi)\simeq37.0\,\mathrm{MHz}.

For a chosen transition, write

g(r)=g0u(r)CpolCint,g(\mathbf r) = g_0 u(\mathbf r) C_{\mathrm{pol}} C_{\mathrm{int}},

where:

  • g0g_0 is the maximum coupling for a reference dipole at the field maximum;
  • u(r)u(\mathbf r) is the complex spatial mode normalized to unit maximum;
  • CpolC_{\mathrm{pol}} is the projection onto local polarization; and
  • CintC_{\mathrm{int}} contains the angular-momentum matrix element relative to the reference transition.

One useful geometric summary of motion is

⟨∣g∣2⟩=g02⟨∣u(r)∣2∣Cpol∣2∣Cint∣2⟩.\langle|g|^2\rangle = g_0^2 \left\langle |u(\mathbf r)|^2 |C_{\mathrm{pol}}|^2 |C_{\mathrm{int}}|^2 \right\rangle.

A mean-square coupling does not generally determine a spectrum. For quasistatic motion, average the complex response or detected intensity over the actual distribution; these nonlinear operations do not commute with replacing ∣g∣2|g|^2 by its mean. Fast motion instead requires a dynamical averaging model.

Near a Fabry–Pérot antinode, a Gaussian standing-wave field may be modeled as

u(r,z)=exp⁡(−r2w02)cos⁡(kz).u(r,z) = \exp\left(-\frac{r^2}{w_0^2}\right) \cos(kz).

For a Gaussian axial position distribution of variance σz2\sigma_z^2 centered at z0z_0,

⟨cos⁡2(kz)⟩=12[1+e−2k2σz2cos⁡(2kz0)].\left\langle \cos^2(kz) \right\rangle = \frac12 \left[ 1 + e^{-2k^2\sigma_z^2} \cos(2kz_0) \right].

The same mean coupling can arise from a tightly localized atom away from an antinode or a broadly distributed atom centered at one. Sideband spectra, trap-frequency measurements, and position-dependent cavity transmission help distinguish them.

Neutral atoms may be delivered by a fountain, conveyor lattice, moving optical tweezer, or loading from a magneto-optical trap. Ions can be held by electrodes while a cavity is positioned around the radio-frequency trap. Flying atomic beams trade long interaction time for simple replenishment.

Intracavity trapping introduces coupled design constraints:

  • the trap should localize the emitter where ∣g∣|g| is large;
  • differential Stark shifts should not destroy resonance or qubit coherence;
  • trap light should not populate or heat the cavity mode;
  • cavity cooling or sideband cooling should remove recoil heating;
  • the cavity lock should remain stable when control beams switch; and
  • a lost emitter should be distinguished from a state change.

Optical tweezers and ion traps explain the corresponding confinement mechanisms.

A real alkali atom, ion, molecule, quantum dot, or defect is not exactly a two-level emitter. Cavity polarization and magnetic field select among Zeeman or hyperfine transitions. Off-resonant states can produce:

  • additional dispersive shifts;
  • Raman scattering and optical pumping;
  • polarization rotation;
  • dark states;
  • leakage outside the qubit manifold; and
  • unequal couplings to nominally degenerate cavity polarizations.

An effective two-level model should be checked by varying magnetic field, probe polarization, detuning, and control-state preparation. A fitted γ\gamma should not silently absorb optical pumping into dark states.

For NN emitters in the weak-excitation limit, the bright collective coupling is

G=∑i=1N∣gi∣2.G = \sqrt{ \sum_{i=1}^{N} |g_i|^2 }.

For equal magnitudes, G=N ∣g∣G=\sqrt N\,|g|. This single bright-mode description assumes initially unexcited emitters with sufficiently similar transition frequencies. Inhomogeneous frequencies or linewidths couple bright and dark combinations; one fitted GG cannot encode all later dynamics.

Resolve the total energy decay into physical channels:

κ=κ1+κ2+κwg+κabs+κsc+⋯ .\kappa = \kappa_1 +\kappa_2 +\kappa_{\mathrm{wg}} +\kappa_{\mathrm{abs}} +\kappa_{\mathrm{sc}} +\cdots.

Only selected terms are useful for a given task. A reflection interface may want one dominant input–output port. A transmission experiment needs two ports. A network node may sacrifice storage time to make κuse/κ\kappa_{\mathrm{use}}/\kappa large.

The design trade is explicit:

  • decreasing useful transmission can raise finesse and QQ;
  • increasing useful transmission can improve escape and bandwidth;
  • intrinsic loss reduces both storage and collection;
  • port asymmetry changes the reflected phase and impedance condition.

The loaded linewidth alone cannot separate these contributions. Combine ringdown with calibrated reflection and transmission, or use independent mirror and waveguide characterization.

Let ηmm\eta_{\mathrm{mm}} be the incident-power fraction in the selected spatial and polarization mode. In a detector integrating complete orthogonal modes, unmatched prompt reflection adds power without interfering with the cavity mode. A finite aperture or subsequent mode projection can make the detected components overlap and interfere. Spectral mismatch likewise requires the detector’s temporal response.

Thus a power dip is not a direct absorption measurement. Complex reflection, transverse-mode imaging, and a known detection-mode projection distinguish coupling, interference, and loss.

Define detunings

Δc=ωp−ωc,Δa=ωp−ωa.\Delta_c = \omega_p-\omega_c, \qquad \Delta_a = \omega_p-\omega_a.

Technical fluctuations give distributions of both variables. Cavity length noise, laser noise, magnetic-field noise, ac Stark shifts, and emitter motion can broaden a spectrum in different ways.

An out-of-loop frequency reference can distinguish physical detuning noise from an artificially quiet in-loop error signal. Noise slow compared with a scan produces drift or inhomogeneous broadening; faster noise can dephase the emitter. Neither effect is automatically a Markovian increase of γ\gamma.

With negligible pure dephasing, use

C0=4g02κγC_0 = \frac{4g_0^2}{\kappa\gamma}

for maximum single-emitter cooperativity. A motion- and state-averaged value is

Ceff=4⟨∣g∣2⟩κγ.C_{\mathrm{eff}} = \frac{ 4\langle|g|^2\rangle }{ \kappa\gamma }.

If pure dephasing matters, the weak-probe response is instead organized by

C⊥=2⟨∣g∣2⟩κγ⊥.C_\perp = \frac{ 2\langle|g|^2\rangle }{ \kappa\gamma_\perp }.

These are useful averages of local response parameters. For fixed coupling, cooperativity compares cavity and free-space channels; for a broad distribution, CeffC_{\mathrm{eff}} is not generally a sufficient parameter for measured transmission or emission. None of these quantities alone establishes resolved coherent exchange.

For an idealized optical transition and cavity, one often summarizes design as “large Q/VQ/V.” The realized cooperativity also depends on:

  • branching ratio of the selected transition;
  • Debye–Waller or zero-phonon fraction for solid-state emitters;
  • angular-momentum coefficient;
  • position and polarization overlap;
  • spectral diffusion and pure dephasing;
  • atom number and state purity; and
  • additional cavity modes.

Publishing both C0C_0 and CeffC_{\mathrm{eff}}, with the reduction factors listed, prevents a simulated field maximum from being mistaken for measured performance.

Consider a linear cavity with

L=200 μm,F=5.00×104,λ=780 nm.\begin{aligned} L &= 200\,\mu\mathrm m, \\ \mathcal F &= 5.00\times10^4, \\ \lambda &= 780\,\mathrm{nm}. \end{aligned}

Its free spectral range is

νFSR=c2L=7.49×1011 Hz.\nu_{\mathrm{FSR}} = \frac{c}{2L} = 7.49\times10^{11}\,\mathrm{Hz}.

The empty-cavity full width is

κ2π=νFSRF=15.0 MHz.\frac{\kappa}{2\pi} = \frac{\nu_{\mathrm{FSR}}}{\mathcal F} = 15.0\,\mathrm{MHz}.

Thus the energy lifetime is

τE=1κ=10.6 ns,\tau_E = \frac{1}{\kappa} = 10.6\,\mathrm{ns},

while the field-amplitude 1/e1/e time is 2/κ=21.2 ns2/\kappa=21.2\,\mathrm{ns}.

Suppose independent spectroscopy gives

g02π=25.0 MHz,γ2π=6.0 MHz.\frac{g_0}{2\pi} = 25.0\,\mathrm{MHz}, \qquad \frac{\gamma}{2\pi} = 6.0\,\mathrm{MHz}.

Then

C0=4(25.0)2(15.0)(6.0)=27.8.\begin{aligned} C_0 &= \frac{ 4(25.0)^2 }{ (15.0)(6.0) } \\ &= 27.8. \end{aligned}

If motion and internal-state preparation reduce ⟨∣g∣2⟩\sqrt{\langle|g|^2\rangle} to 0.70g00.70g_0, then

Ceff=(0.70)2C0=13.6.C_{\mathrm{eff}} = (0.70)^2C_0 = 13.6.

Both are high-cooperativity values. A strong-coupling claim still requires a comparison of gg with the dissipative pole widths and evidence that the observed doublet belongs to one emitter and one cavity mode.

With the energy-decay convention above, the resonant linear amplitude poles are

λ±=−κ/2+γ⊥2±(κ/2−γ⊥)24−g2.\lambda_\pm=-\frac{\kappa/2+\gamma_\perp}{2} \pm\sqrt{\frac{(\kappa/2-\gamma_\perp)^2}{4}-g^2}.

An imaginary part signals underdamped normal modes, but visible peak separation also depends on their width and the measured port. High cooperativity can occur at κ≫g\kappa\gg g, where cavity emission is efficient without several coherent swaps.

An avoided crossing as the emitter is tuned through the cavity, together with empty-cavity mode characterization, identifies coupled emitter–cavity resonances. It does not distinguish a quantized field from classical coupled oscillators in linear response: even oscillatory transients have a classical counterpart (Zhu et al.). Photon antibunching, an excitation-dependent Jaynes–Cummings ladder, or verified emitter–photon entanglement tests additional quantum structure.

Prepare ∣e,0⟩|e,0\rangle on resonance with fixed gg, zero-temperature loss, and γϕ=0\gamma_\phi=0. Cavity QED derives the integrated cavity flux,

Pcav=κκ+γC1+C,C=4g2κγ.P_{\mathrm{cav}} =\frac{\kappa}{\kappa+\gamma}\frac{C}{1+C}, \qquad C=\frac{4g^2}{\kappa\gamma}.

The useful-port probability is therefore

Puse=κuseκ+γ4g24g2+κγ.P_{\mathrm{use}} =\frac{\kappa_{\mathrm{use}}}{\kappa+\gamma} \frac{4g^2}{4g^2+\kappa\gamma}.

The extra κ/(κ+γ)\kappa/(\kappa+\gamma) factor accounts for repeated coherent exchange before final decay. The eliminated-cavity result C/(1+C)C/(1+C) is recovered for κ≫g,γ\kappa\gg g,\gamma; high cooperativity alone does not justify it. Shaped Raman emission is a different preparation protocol with its own efficiency.

Let x=κusex=\kappa_{\mathrm{use}}, ℓ=κ−κuse\ell=\kappa-\kappa_{\mathrm{use}}, and A=4g2/γA=4g^2/\gamma, holding g,γ,ℓg,\gamma,\ell fixed. Then

Puse(x)=Ax(x+ℓ+γ)(x+ℓ+A).P_{\mathrm{use}}(x)= \frac{Ax}{(x+\ell+\gamma)(x+\ell+A)}.

Differentiation gives the unique positive optimum

x⋆=(ℓ+γ)(ℓ+A).x_\star=\sqrt{(\ell+\gamma)(\ell+A)}.

Opening the port beyond this point reduces the interaction time faster than it improves extraction. In practice, changing mirror transmission may also change geometry or loss; this optimum holds only for the stated fixed parameters.

From a Local Interface to a Quantum Network

Section titled “From a Local Interface to a Quantum Network”

A photon source needs both successful extraction and the desired temporal, spectral, and polarization mode. Antibunching constrains multiphoton contamination; it does not establish brightness or indistinguishability. Two-photon interference probes the latter.

For two-photon heralding between nodes, the success probability includes both node-emission probabilities, both channel transmissions, and the interference/detection success. A single-photon heralding protocol has a different loss dependence. State-transfer and gate fidelities must specify whether failed detection, leakage, and lost emitters are retained as erasures or conditioned away. Reiserer and Rempe develop these interface requirements; cavity and circuit QED frontiers discusses extensions to larger systems.

A linear optical cavity has length L=300 μmL=300\,\mu\mathrm m and finesse F=6.0×104\mathcal F=6.0\times10^4.

  1. Find the free spectral range.
  2. Find κ/(2π)\kappa/(2\pi) under this page’s convention.
  3. Find the intracavity energy and field-amplitude 1/e1/e times.
Solution

The free spectral range is

νFSR=c2L=4.997×1011 Hz.\nu_{\mathrm{FSR}} = \frac{c}{2L} = 4.997\times10^{11}\,\mathrm{Hz}.

The power-resonance full width is

κ2π=νFSRF=8.33 MHz.\frac{\kappa}{2\pi} = \frac{\nu_{\mathrm{FSR}}}{\mathcal F} = 8.33\,\mathrm{MHz}.

Thus

κ=2π(8.33×106) s−1=5.23×107 s−1.\kappa = 2\pi(8.33\times10^6)\,\mathrm{s^{-1}} = 5.23\times10^7\,\mathrm{s^{-1}}.

The energy lifetime is

τE=1κ=19.1 ns.\tau_E = \frac{1}{\kappa} = 19.1\,\mathrm{ns}.

Since field amplitude decays at κ/2\kappa/2,

τA=2κ=38.2 ns.\tau_A = \frac{2}{\kappa} = 38.2\,\mathrm{ns}.

Calling 1/κ1/\kappa the amplitude lifetime would create a factor-of-two error.

An atom is centered at an antinode of

u(r,z)=e−r2/w02cos⁡(kz).u(r,z) = e^{-r^2/w_0^2}\cos(kz).

Its axial position is Gaussian with kσz=0.30k\sigma_z=0.30. Each transverse Cartesian coordinate is Gaussian with σr/w0=0.10\sigma_r/w_0=0.10. Internal-state and polarization overlap are ideal. Find ⟨∣g∣2⟩/g02\langle|g|^2\rangle/g_0^2 and grms/g0g_{\mathrm{rms}}/g_0.

Solution

At an antinode,

⟨cos⁡2(kz)⟩=1+e−2k2σz22=1+e−0.182=0.918.\left\langle \cos^2(kz) \right\rangle = \frac{ 1+e^{-2k^2\sigma_z^2} }{2} = \frac{1+e^{-0.18}}{2} = 0.918.

For two independent transverse Gaussian coordinates,

⟨e−2r2/w02⟩=11+4σr2/w02=11.04=0.962.\left\langle e^{-2r^2/w_0^2} \right\rangle = \frac{1}{ 1+4\sigma_r^2/w_0^2 } = \frac{1}{1.04} = 0.962.

Therefore

⟨∣g∣2⟩g02=(0.918)(0.962)=0.883,\frac{ \langle|g|^2\rangle }{ g_0^2 } = (0.918)(0.962) = 0.883,

and

grmsg0=0.883=0.940.\frac{g_{\mathrm{rms}}}{g_0} = \sqrt{0.883} = 0.940.

This gives the mean local cooperativity. Averaging an actual transmission spectrum still requires the distribution of gg, as Exercise 7 demonstrates.

3. High cooperativity without strong coupling

Section titled “3. High cooperativity without strong coupling”

A platform has

g2π=10 MHz,κ2π=100 MHz,γ2π=0.10 MHz,\frac{g}{2\pi} = 10\,\mathrm{MHz}, \quad \frac{\kappa}{2\pi} = 100\,\mathrm{MHz}, \quad \frac{\gamma}{2\pi} = 0.10\,\mathrm{MHz},

with negligible pure dephasing. Find CC and classify the regime.

Solution

Common factors of 2π2\pi cancel:

C=4g2κγ=4(10)2(100)(0.10)=40.C = \frac{4g^2}{\kappa\gamma} = \frac{ 4(10)^2 }{ (100)(0.10) } = 40.

The cooperativity is high, so cavity-mediated emission can dominate free-space decay. However,

κ=10g,\kappa = 10g,

so a cavity excitation leaks much faster than a coherent exchange period. This is a high-cooperativity bad-cavity or Purcell regime, not unambiguous strong coupling.

In the resonant, eliminated-cavity regime κ≫g,γ\kappa\gg g,\gamma, with negligible pure dephasing and one initial emitter excitation, take

βcav=C1+C.\beta_{\mathrm{cav}} = \frac{C}{1+C}.

For C=19C=19, a useful-port fraction ηesc=0.75\eta_{\mathrm{esc}}=0.75, path transmission ηpath=0.60\eta_{\mathrm{path}}=0.60, and detector efficiency ηdet=0.80\eta_{\mathrm{det}}=0.80:

  1. find the click probability conditional on successful emitter preparation and emission;
  2. compare equal fractional improvements of each efficiency, then equal absolute improvements that remain physically attainable.
Solution

The cavity branching estimate is

βcav=1920=0.95.\beta_{\mathrm{cav}} = \frac{19}{20} = 0.95.

The conditional click probability is

Pclick∣emit=(0.95)(0.75)(0.60)(0.80)=0.342.\begin{aligned} P_{\mathrm{click|emit}} &= (0.95)(0.75)(0.60)(0.80) \\ &= 0.342. \end{aligned}

The product gives 34.2%. Equal fractional improvements of any one factor give the same fractional improvement of the product. For equal absolute increments, the smallest factor has the largest logarithmic derivative ∂ln⁡P/∂ηi=1/ηi\partial\ln P/\partial\eta_i=1/\eta_i, so path transmission is most effective here. Improving CC further has diminishing effect because C/(1+C)C/(1+C) is already 0.95. Costs and feasible headroom matter.

The formula assumes matched spectra, independent receiver operation per trial, and the stated cavity elimination.

For a 51 GHz51\,\mathrm{GHz} cavity:

  1. calculate ℏωc/kB\hbar\omega_c/k_B;
  2. find nˉth\bar n_{\mathrm{th}} at 0.50 K0.50\,\mathrm K and 1.0 K1.0\,\mathrm K;
  3. find the temperature required for nˉth=0.01\bar n_{\mathrm{th}}=0.01.
Solution

Since ℏωc=hνc\hbar\omega_c=h\nu_c,

ℏωckB=h(51×109)kB=2.45 K.\frac{\hbar\omega_c}{k_B} = \frac{h(51\times10^9)}{k_B} = 2.45\,\mathrm K.

At 0.50 K0.50\,\mathrm K,

nˉth=1e2.45/0.50−1=7.5×10−3.\bar n_{\mathrm{th}} = \frac{1}{e^{2.45/0.50}-1} = 7.5\times10^{-3}.

At 1.0 K1.0\,\mathrm K,

nˉth=1e2.45−1=9.45×10−2.\bar n_{\mathrm{th}} = \frac{1}{e^{2.45}-1} = 9.45\times10^{-2}.

For a target nˉ\bar n,

ℏωckBT=ln⁡(1+1nˉ).\frac{\hbar\omega_c}{k_BT} = \ln\left(1+\frac{1}{\bar n}\right).

Thus

T=2.45 Kln⁡101=0.530 K.T = \frac{2.45\,\mathrm K}{\ln101} = 0.530\,\mathrm K.

The cavity can still see excess photons from warmer apertures or technical injection even when the local cryostat temperature satisfies this estimate.

A cavity has

κuse=2π(6 MHz),κother=2π(2 MHz),κint=2π(2 MHz).\kappa_{\mathrm{use}} = 2\pi(6\,\mathrm{MHz}), \quad \kappa_{\mathrm{other}} = 2\pi(2\,\mathrm{MHz}), \quad \kappa_{\mathrm{int}} = 2\pi(2\,\mathrm{MHz}).

The emitter coupling and decay are

g2π=12 MHz,γ2π=3 MHz.\frac{g}{2\pi} = 12\,\mathrm{MHz}, \qquad \frac{\gamma}{2\pi} = 3\,\mathrm{MHz}.

Find ηesc\eta_{\mathrm{esc}} and CC. Then double κuse\kappa_{\mathrm{use}} while leaving all other quantities unchanged. Recompute both and explain the trade.

Solution

Initially,

κ2π=6+2+2=10 MHz,\frac{\kappa}{2\pi} = 6+2+2 = 10\,\mathrm{MHz},

so

ηesc=610=0.60.\eta_{\mathrm{esc}} = \frac{6}{10} = 0.60.

The cooperativity is

C=4(12)2(10)(3)=19.2.C = \frac{4(12)^2}{(10)(3)} = 19.2.

After doubling the useful coupling,

κ′2π=12+2+2=16 MHz,\frac{\kappa'}{2\pi} = 12+2+2 = 16\,\mathrm{MHz},

and

ηesc′=1216=0.75.\eta_{\mathrm{esc}}' = \frac{12}{16} = 0.75.

However,

C′=4(12)2(16)(3)=12.0.C' = \frac{4(12)^2}{(16)(3)} = 12.0.

The useful escape fraction improves while storage and cooperativity fall. The best choice depends on whether the protocol is limited by internal channeling, output extraction, bandwidth, or coherent exchange.

7. Why mean coupling can mispredict transmission

Section titled “7. Why mean coupling can mispredict transmission”

For a resonant weak probe in a two-port cavity, normalize transmitted power to its empty-cavity value. With no prompt transmitted path and no pure dephasing, T(C)=1/(1+C)2T(C)=1/(1+C)^2. Compare an emitter fixed at C=10C=10 with a quasistatic ensemble spending equal time at C=0C=0 and C=20C=20. Both have ⟨C⟩=10\langle C\rangle=10.

Solution

The fixed emitter transmits 1/121=0.008261/121=0.00826. Averaging detected power for the two configurations gives

⟨T⟩=12(1+1212)=0.50113.\langle T\rangle=\frac12\left(1+\frac1{21^2}\right)=0.50113.

The large difference comes from the uncoupled half of the sample. A coherent receiver averaging field amplitude would instead average 1/(1+C)1/(1+C) before forming the selected statistic. Neither measurement is specified by ⟨C⟩\langle C\rangle alone.

For g/(2π)=12 MHzg/(2\pi)=12\,\mathrm{MHz}, γ/(2π)=3 MHz\gamma/(2\pi)=3\,\mathrm{MHz}, and fixed unwanted loss ℓ/(2π)=4 MHz\ell/(2\pi)=4\,\mathrm{MHz}, find the useful-port coupling that maximizes the escape probability of one prepared emitter excitation. Does making the port arbitrarily open help?

Solution

In the same frequency units A/(2π)=4(12)2/3=192 MHzA/(2\pi)=4(12)^2/3=192\,\mathrm{MHz}. Therefore

x⋆2π=(4+3)(4+192) MHz=37.0 MHz.\frac{x_\star}{2\pi} =\sqrt{(4+3)(4+192)}\,\mathrm{MHz} =37.0\,\mathrm{MHz}.

For x→∞x\to\infty, Puse∼A/x→0P_{\mathrm{use}}\sim A/x\to0 even though the cavity escape fraction x/(x+ℓ)x/(x+\ell) tends to one. The initially excited emitter then mainly decays outside a cavity that responds too rapidly to build up a field.

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