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Radiation Pressure

Radiation pressure is mechanical momentum transfer from an electromagnetic field to matter. For a freely moving atom, a photon absorbed from a traveling wave changes the atomic momentum by +ℏk+\hbar\mathbf k. Subsequent spontaneous emission gives a recoil −ℏks-\hbar\mathbf k_s, so one complete scattering cycle changes the atomic momentum by

Δp=ℏ(k−ks).\Delta\mathbf p = \hbar \left( \mathbf k-\mathbf k_s \right).

In free space, the mean spontaneous-emission direction often vanishes. The mean cycle impulse is then ℏk\hbar\mathbf k, directed along the incident beam. The emitted direction still fluctuates, so the same cycles that produce a mean force also produce momentum diffusion and recoil heating.

For a closed two-level atom driven by one traveling wave, the steady scattering force is

Fsc=ℏkΓ2s01+s0+(2Δv/Γ)2.\mathbf F_{\mathrm{sc}} = \hbar\mathbf k \frac{\Gamma}{2} \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 }.

Here Γ\Gamma is the excited-state population decay rate, s0=2∣Ω∣2/Γ2s_0=2|\Omega|^2/\Gamma^2 is the on-resonance saturation parameter, and Δv\Delta_v is the Doppler-shifted detuning. This compact expression is powerful, but its assumptions matter: a closed transition, a stationary internal state, one traveling mode, controlled recoil averaging, and center-of-mass motion slow enough that the internal steady state can follow.

Radiation pressure is not synonymous with every optical force. The dissipative scattering force follows the beam’s phase gradient and requires irreversible emission. The conservative dipole force follows an intensity gradient and is generated by a position-dependent light shift. Real laser fields can exert both.

This page owns:

  1. the momentum ledger for absorption, stimulated emission, and spontaneous emission;
  2. the mean scattering force of a driven two-level atom;
  3. saturation, resonant cross section, and the maximum force;
  4. Doppler-shifted force and the low-velocity damping slope;
  5. recoil, momentum diffusion, and mechanical heating;
  6. the distinction between scattering and dipole forces;
  7. multibeam, multilevel, cavity, and experimental limitations;
  8. the mechanical bridge to laser cooling without re-deriving cooling temperatures or trap architectures.

Nearby canonical homes remain distinct:

  • Photon Momentum owns the historical evidence, the classical field-momentum connection, and the relation pγ=h/λp_\gamma=h/\lambda.
  • Optical Bloch Equations owns the driven density-matrix dynamics, steady-state population, and saturation derivation used here.
  • Spontaneous Emission owns the radiative decay rate, angular pattern, branching, and environment dependence.
  • AC Stark Shift and Dynamic Polarizability own conservative light shifts, dipole potentials, and multilevel polarizabilities.
  • Quantum-Jump Trajectories owns state evolution conditioned on individual emission records.
  • Optomechanics owns radiation-pressure coupling to a retained cavity mode, dynamical backaction, and measurement noise.

This page treats the center-of-mass mechanics of a laser-driven atom and cross-links rather than duplicating those subjects.

A plane wave of intensity II carries energy flux II and momentum flux I/cI/c in vacuum. At normal incidence, an ideal absorbing surface therefore feels pressure

Pabs=Ic.P_{\mathrm{abs}} = \frac{I}{c}.

A perfectly reflecting surface reverses the normal momentum and feels

Prefl=2Ic.P_{\mathrm{refl}} = \frac{2I}{c}.

Radiation pressure therefore does not by itself prove that the field is in a photon-number state. Classical Maxwell fields carry momentum. The photon description becomes especially useful when individual absorption and emission recoils, counting fluctuations, and internal transitions must be tracked.

An atom does not present a hard geometric disk. Near an allowed resonance, its optical response defines a frequency-, polarization-, state-, and intensity-dependent effective cross section. In the weak-field limit, the force can be written

Fsc=Icσ(Δv).F_{\mathrm{sc}} = \frac{I}{c} \sigma(\Delta_v).

This has the same momentum-flux structure as macroscopic pressure, but the atomic cross section can be much larger than the atom’s geometric area. Saturation eventually makes the response nonlinear in II.

For a traveling mode with wave vector k\mathbf k, absorption removes one field quantum of momentum ℏk\hbar\mathbf k. Momentum conservation gives

Δpatomabs=+ℏk.\Delta\mathbf p_{\mathrm{atom}}^{\mathrm{abs}} = +\hbar\mathbf k.

The statement assumes that any momentum supplied to an optical element, substrate, or second field has already been included in the chosen system boundary.

Stimulated emission into the same traveling mode adds a photon with momentum ℏk\hbar\mathbf k to that mode. The atom receives

Δpatomstim=−ℏk.\Delta\mathbf p_{\mathrm{atom}}^{\mathrm{stim}} = -\hbar\mathbf k.

Absorption and stimulated emission therefore push in opposite directions. It is incorrect to count every coherent excitation as a permanent +ℏk+\hbar\mathbf k impulse while ignoring stimulated return.

If the emitted photon has wave vector ks\mathbf k_s, the atomic recoil is

Δpatomsp=−ℏks.\Delta\mathbf p_{\mathrm{atom}}^{\mathrm{sp}} = -\hbar\mathbf k_s.

For one absorption–spontaneous-emission cycle,

Δpcycle=ℏk−ℏks.\Delta\mathbf p_{\mathrm{cycle}} = \hbar\mathbf k - \hbar\mathbf k_s.

The emitted photon is not generally isotropic. Electric-dipole radiation has an angular pattern fixed by the transition and polarization. In inversion-symmetric free space one often has

⟨ks⟩=0,\left\langle \mathbf k_s \right\rangle = 0,

even though the second moment is nonzero. Cavities, waveguides, nearby surfaces, collective emission, or chiral coupling can make the mean emission recoil directional.

Momentum transfer in one scattering cycle, the saturated single-beam force, and Doppler damping from two red-detuned beams

Top: absorption supplies +ℏk+\hbar\mathbf k and spontaneous emission supplies −ℏks-\hbar\mathbf k_s. Middle: the single-beam force is a power-broadened, saturating resonance. Bottom: two weak counterpropagating red-detuned beams produce a net force opposing small velocities, while recoil fluctuations remain.

Let R\mathbf R and P\mathbf P be the center-of-mass position and canonical momentum. For an interaction Hamiltonian Hint(R)H_{\mathrm{int}}(\mathbf R), the optical force operator is

F^=−∇RHint.\widehat{\mathbf F} = - \boldsymbol\nabla_{\mathbf R} H_{\mathrm{int}}.

Ehrenfest’s theorem gives

ddt⟨P⟩=⟨F^⟩\frac{d}{dt} \left\langle \mathbf P \right\rangle = \left\langle \widehat{\mathbf F} \right\rangle

when no other external force is present. A traveling wave contains both an amplitude gradient and a phase gradient. Differentiating the light–matter Hamiltonian separates:

  • an amplitude-gradient contribution associated with the reactive dipole force;
  • a phase-gradient contribution associated with directed momentum transfer.

The cycle picture and the force-operator picture are two descriptions of the same momentum conservation. The cycle picture is particularly transparent after spontaneous events can be treated as resolved or coarse-grained jumps.

Let RabsR_{\mathrm{abs}} and RstimR_{\mathrm{stim}} denote the net upward and stimulated downward rates in a rate description. For a closed two-level transition,

ρ˙ee=Rabs−Rstim−Γρee.\dot\rho_{ee} = R_{\mathrm{abs}} - R_{\mathrm{stim}} - \Gamma\rho_{ee}.

At steady state,

Rabs−Rstim=Γρeess.R_{\mathrm{abs}} - R_{\mathrm{stim}} = \Gamma\rho_{ee}^{\mathrm{ss}}.

The net rate at which directed photons are removed from the traveling beam equals the spontaneous-emission rate. If the mean spontaneous recoil is zero,

Fsc=ℏkΓρeess.\mathbf F_{\mathrm{sc}} = \hbar\mathbf k \Gamma\rho_{ee}^{\mathrm{ss}}.

In a coherently driven atom, absorption and stimulated emission need not admit a unique trajectory decomposition at every instant. The steady-state balance above is the operational statement needed for the mean force.

Use a closed transition ∣g⟩↔∣e⟩|g\rangle\leftrightarrow|e\rangle with angular frequency ω0\omega_0, population decay rate Γ\Gamma, and a plane-wave laser with angular frequency ωL\omega_L and wave vector k\mathbf k. This chapter uses atom-minus-laser detuning:

Δ=ω0−ωL.\Delta = \omega_0-\omega_L.

Red detuning has Δ>0\Delta>0. All frequencies and decay rates are angular quantities unless divided by 2π2\pi.

The Rabi Hamiltonian contains the off-diagonal coefficient ℏΩ/2\hbar\Omega/2. Define the on-resonance saturation parameter

s0=2∣Ω∣2Γ2.s_0 = \frac{ 2|\Omega|^2 }{ \Gamma^2 }.

For a nonrelativistic atom with velocity v\mathbf v, the laser frequency in the atomic rest frame is

ωL′≃ωL−k⋅v.\omega_L' \simeq \omega_L - \mathbf k\mathbin{\cdot}\mathbf v.

The effective detuning is therefore

Δv=Δ+k⋅v.\Delta_v = \Delta + \mathbf k\mathbin{\cdot}\mathbf v.

Writing the optical phase and transforming it is safer than memorizing a Doppler sign. A reference using laser-minus-atom detuning displays the opposite sign.

The optical Bloch steady state gives

ρeess=12s01+s0+(2Δv/Γ)2.\rho_{ee}^{\mathrm{ss}} = \frac12 \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 }.

It is also useful to define the detuning-dependent saturation parameter

s(Δv)=s01+(2Δv/Γ)2.s(\Delta_v) = \frac{ s_0 }{ 1+ \left( 2\Delta_v/\Gamma \right)^2 }.

Then

ρeess=s2(1+s).\rho_{ee}^{\mathrm{ss}} = \frac{ s }{ 2(1+s) }.

The spontaneous scattering rate is

Rsc=Γρeess,R_{\mathrm{sc}} = \Gamma\rho_{ee}^{\mathrm{ss}},

or

Rsc=Γ2s01+s0+(2Δv/Γ)2.R_{\mathrm{sc}} = \frac{\Gamma}{2} \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 }.

The corresponding mean force is

Fsc=ℏkRsc.\mathbf F_{\mathrm{sc}} = \hbar\mathbf k R_{\mathrm{sc}}.

This result assumes the mean emitted momentum vanishes. If it does not, replace the impulse per cycle:

F=ℏ(k−⟨ks⟩)Rsc.\mathbf F = \hbar \left( \mathbf k - \left\langle \mathbf k_s \right\rangle \right) R_{\mathrm{sc}}.

On resonance,

Rsc(0)=Γ2s01+s0.R_{\mathrm{sc}}(0) = \frac{\Gamma}{2} \frac{ s_0 }{ 1+s_0 }.

As s0→∞s_0\to\infty,

ρeess⟶12,\rho_{ee}^{\mathrm{ss}} \longrightarrow \frac12,

and

Rsc⟶Γ2.R_{\mathrm{sc}} \longrightarrow \frac{\Gamma}{2}.

The ideal two-level force is bounded by

Fmax⁡=ℏkΓ2.F_{\max} = \frac{ \hbar k\Gamma }{ 2 }.

The associated maximum acceleration is

amax⁡=ℏkΓ2m.a_{\max} = \frac{ \hbar k\Gamma }{ 2m }.

Increasing intensity far beyond saturation does not make a closed two-level atom scatter arbitrarily fast. The atom spends approximately half its time excited, and stimulated emission competes with absorption.

The force profile is Lorentzian in Δv\Delta_v with a saturated half-width

ΔHWHM=Γ21+s0.\Delta_{\mathrm{HWHM}} = \frac{\Gamma}{2} \sqrt{ 1+s_0 }.

Intensity therefore changes both the peak and the velocity or frequency range over which the force is substantial. A broadened force profile is not evidence that Γ\Gamma itself increased.

The steady formula assumes that position, velocity, intensity, detuning, and polarization vary slowly enough for the internal state to relax toward the local steady state. A short pulse or rapid transit requires time-dependent optical Bloch evolution and the impulse

Δp=∫titfF(t) dt.\Delta\mathbf p = \int_{t_i}^{t_f} \mathbf F(t)\,dt.

A coherent π\pi pulse can transfer approximately one photon recoil, but repeated dissipative force requires a mechanism that resets the internal state.

The photon flux in a plane wave is

Φγ=IℏωL.\Phi_\gamma = \frac{ I }{ \hbar\omega_L }.

In the weak-field limit,

Rsc=Φγσ(Δv).R_{\mathrm{sc}} = \Phi_\gamma \sigma(\Delta_v).

For an ideal closed electric-dipole transition with the appropriate polarization and degeneracy assumptions,

σ0=3λ22π,\sigma_0 = \frac{ 3\lambda^2 }{ 2\pi },

and

σ(Δv)=σ01+(2Δv/Γ)2.\sigma(\Delta_v) = \frac{ \sigma_0 }{ 1+ \left( 2\Delta_v/\Gamma \right)^2 }.

Then

Fsc=Icσ(Δv).F_{\mathrm{sc}} = \frac{I}{c} \sigma(\Delta_v).

This directly connects the photon-cycle result to incident momentum flux.

Define IsatI_{\mathrm{sat}} by

s0=IIsat.s_0 = \frac{I}{I_{\mathrm{sat}}}.

For the same ideal cycling transition and conventions,

Isat=πhcΓ3λ3.I_{\mathrm{sat}} = \frac{ \pi h c\Gamma }{ 3\lambda^3 }.

At finite intensity one may write an effective nonlinear cross section

σeff=σ01+s0+(2Δv/Γ)2,\sigma_{\mathrm{eff}} = \frac{ \sigma_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 },

so that F=Iσeff/cF=I\sigma_{\mathrm{eff}}/c. This is bookkeeping for saturation, not a linear material cross section independent of the incident field.

The familiar σ0\sigma_0 and IsatI_{\mathrm{sat}} require a declared transition. Real corrections include:

  • Clebsch–Gordan coefficients and laser polarization;
  • ground- and excited-state degeneracy;
  • branching into states outside the driven cycle;
  • optical pumping among Zeeman or hyperfine levels;
  • imperfect spatial mode and intensity calibration;
  • laser linewidth and frequency noise;
  • nearby transitions and interference;
  • collective and propagation effects.

Quoting a universal saturation intensity without the transition, polarization, and state preparation is incomplete.

Consider a cycling transition with rounded parameters

λ=780 nm,Γ2π=6.0 MHz,m=1.44×10−25 kg.\begin{aligned} \lambda &= 780\ \mathrm{nm}, \\ \frac{\Gamma}{2\pi} &= 6.0\ \mathrm{MHz}, \\ m &= 1.44\times10^{-25}\ \mathrm{kg}. \end{aligned}

Take

s0=2,Δ=Γ2,v=0.s_0=2, \qquad \Delta=\frac{\Gamma}{2}, \qquad v=0.

The force denominator is

1+s0+(2Δ/Γ)2=4,1+s_0+ \left( 2\Delta/\Gamma \right)^2 = 4,

so

Rsc=Γ4≃9.4×106 s−1.R_{\mathrm{sc}} = \frac{\Gamma}{4} \simeq 9.4\times10^6\ \mathrm{s^{-1}}.

The photon recoil momentum is

ℏk=hλ≃8.5×10−28 kg m s−1.\hbar k = \frac{h}{\lambda} \simeq 8.5\times10^{-28}\ \mathrm{kg\,m\,s^{-1}}.

Hence

Fsc≃8.0×10−21 N,a≃5.6×104 m s−2.\begin{aligned} F_{\mathrm{sc}} &\simeq 8.0\times10^{-21}\ \mathrm N, \\ a &\simeq 5.6\times10^4\ \mathrm{m\,s^{-2}}. \end{aligned}

The force is microscopic, but the mass is smaller still. During 10 μs10\ \mathrm{\mu s}, a constant-force estimate gives approximately

Nsc=Rsct≃94N_{\mathrm{sc}} = R_{\mathrm{sc}}t \simeq 94

cycles and a speed change

Δv≃Nscℏkm≃0.56 m s−1.\Delta v \simeq N_{\mathrm{sc}} \frac{\hbar k}{m} \simeq 0.56\ \mathrm{m\,s^{-1}}.

This estimate must be audited for Doppler feedback. At the predicted final speed,

kΔvΓ≃0.12.\frac{k\Delta v}{\Gamma} \simeq 0.12.

The atom has moved measurably across the force profile, so even this short constant-force estimate is only approximate. Over longer slowing times, laser chirping or a position-dependent Zeeman shift is needed to maintain resonance.

Define

pr=ℏk,p_r = \hbar k,

the recoil velocity

vr=ℏkm,v_r = \frac{ \hbar k }{ m },

and the recoil energy

Er=ℏ2k22m.E_r = \frac{ \hbar^2k^2 }{ 2m }.

The recoil angular frequency is

ωr=Erℏ.\omega_r = \frac{E_r}{\hbar}.

These scales determine when center-of-mass motion must be quantized rather than treated as a continuous classical trajectory.

For absorption from fixed k\mathbf k followed by free-space emission with ∣ks∣≃k|\mathbf k_s|\simeq k and ⟨ks⟩=0\langle\mathbf k_s\rangle=0,

⟨∣Δp∣2⟩=2ℏ2k2.\left\langle |\Delta\mathbf p|^2 \right\rangle = 2\hbar^2k^2.

The corresponding recoil contribution to kinetic energy is

⟨∣Δp∣2⟩2m=2Er\frac{ \left\langle |\Delta\mathbf p|^2 \right\rangle }{ 2m } = 2E_r

per independent cycle. The total energy change also contains mechanical work from the mean force:

E˙kin=F⋅v+diffusive heating.\dot E_{\mathrm{kin}} = \mathbf F\mathbin{\cdot}\mathbf v + \text{diffusive heating}.

Directed acceleration and random heating are different moments of the same recoil process.

Let u\mathbf u be a unit vector along a measured axis. In an independent-cycle model,

ddtVar⁡(pu)=ℏ2Rsc[(u⋅k)2+⟨(u⋅ks)2⟩].\begin{aligned} \frac{d}{dt} \operatorname{Var}(p_u) = \hbar^2R_{\mathrm{sc}} \Big[ & \left( \mathbf u\mathbin{\cdot}\mathbf k \right)^2 \\ &+ \left\langle \left( \mathbf u\mathbin{\cdot}\mathbf k_s \right)^2 \right\rangle \Big]. \end{aligned}

The first term is absorption-number noise along the incident beam. The second is random spontaneous-emission recoil. If a Fokker–Planck equation uses

ddtVar⁡(pu)=2Dp,u,\frac{d}{dt} \operatorname{Var}(p_u) = 2D_{p,u},

then

Dp,u=ℏ2Rsc2[(u⋅k)2+⟨(u⋅ks)2⟩].\begin{aligned} D_{p,u} = \frac{\hbar^2R_{\mathrm{sc}}}{2} \Big[ & \left( \mathbf u\mathbin{\cdot}\mathbf k \right)^2 \\ &+ \left\langle \left( \mathbf u\mathbin{\cdot}\mathbf k_s \right)^2 \right\rangle \Big]. \end{aligned}

Authors also use a convention without the factor of two. A quoted momentum diffusion coefficient is ambiguous until its defining equation is stated.

For isotropic emission,

⟨(u⋅ks)2⟩=k23.\left\langle \left( \mathbf u\mathbin{\cdot}\mathbf k_s \right)^2 \right\rangle = \frac{k^2}{3}.

Along the incident beam,

ddtVar⁡(p∥)=43ℏ2k2Rsc.\frac{d}{dt} \operatorname{Var}(p_\parallel) = \frac43 \hbar^2k^2 R_{\mathrm{sc}}.

Electric-dipole emission is not generally isotropic, so the factor 1/31/3 must be replaced by the angular moment of the actual radiation pattern.

At high saturation or in structured fields, the simple Poisson-cycle model can miss:

  • antibunching and temporal correlations in resonance fluorescence;
  • fluctuations of the coherent dipole force;
  • standing-wave position dependence;
  • internal-state switching;
  • cavity-modified emission;
  • collective scattering and reabsorption.

The mean force can remain accurate while its noise model fails. Mechanical heating, linewidths, and trap loss depend on the second moments.

For a far-detuned, slowly varying two-level field, the ground-state light shift in this chapter’s detuning convention is

Ug(r)≃−ℏ∣Ω(r)∣24Δ.U_g(\mathbf r) \simeq - \frac{ \hbar|\Omega(\mathbf r)|^2 }{ 4\Delta }.

The conservative dipole force is

Fdip=−∇Ug.\mathbf F_{\mathrm{dip}} = - \boldsymbol\nabla U_g.

For red detuning, Δ>0\Delta>0, this ideal ground state is attracted toward larger intensity.

In the same weak, far-detuned limit,

Rsc≃Γ∣Ω∣24Δ2.R_{\mathrm{sc}} \simeq \frac{ \Gamma|\Omega|^2 }{ 4\Delta^2 }.

The light shift scales as I/ΔI/\Delta, while scattering scales as I/Δ2I/\Delta^2. Increasing detuning at fixed trap depth reduces the scattering cost in the ideal one-line model, but finite power and multilevel structure limit that strategy.

PropertyScattering forceDipole force
responseabsorptive or dissipativedispersive or reactive
directionoptical phase gradient, often k\mathbf kintensity or dressed-energy gradient
steady originirreversible photon redistributionposition-dependent light shift
saturationbounded by the internal cycling ratedepends on dressed potential and adiabaticity
fluctuationsphoton recoil and force noise are intrinsictechnical and quantum fluctuations can remain
uniform plane wavegenerally nonzero near resonancezero if amplitude is uniform

A focused beam can exert both forces simultaneously. Calling the total force “radiation pressure” without specifying its dissipative and conservative parts can hide the relevant physics.

Consider two equal, incoherently added traveling waves along ±x\pm x, each with on-resonance saturation parameter s0≪1s_0\ll1. For velocity vv along +x+x, their detunings are

Δ+=Δ+kv,\Delta_+ = \Delta+kv,

and

Δ−=Δ−kv.\Delta_- = \Delta-kv.

The low-saturation net force is

F(v)=ℏkΓs02[11+(2Δ+/Γ)2−11+(2Δ−/Γ)2].\begin{aligned} F(v) = \frac{\hbar k\Gamma s_0}{2} \Bigg[ & \frac{ 1 }{ 1+ \left( 2\Delta_+/\Gamma \right)^2 } \\ &- \frac{ 1 }{ 1+ \left( 2\Delta_-/\Gamma \right)^2 } \Bigg]. \end{aligned}

At v=0v=0, the two forces cancel.

For ∣kv∣≪Γ|kv|\ll\Gamma, expand:

F(v)≃−αv.F(v) \simeq -\alpha v.

The friction coefficient is

α=8ℏk2s0(Δ/Γ)[1+(2Δ/Γ)2]2.\alpha = \frac{ 8\hbar k^2s_0 \left( \Delta/\Gamma \right) }{ \left[ 1+ \left( 2\Delta/\Gamma \right)^2 \right]^2 }.

With this page’s convention, red detuning has Δ>0\Delta>0, so α>0\alpha>0 and the force opposes small velocities. Blue detuning reverses the slope and produces antidamping.

This is the mechanical seed of Doppler Cooling. It is not a complete temperature theory: the same scattering events generate momentum diffusion, and equilibrium follows from the balance between damping and noise. Multilevel polarization-gradient mechanisms can operate below the simple two-level Doppler scale.

A single counterpropagating beam can slow a selected velocity class, but it also gives nonzero mean acceleration. Two opposite beams cancel at zero velocity while retaining a velocity-odd restoring force in momentum space. Spatial confinement requires additional position dependence, such as magnetic-field-induced Zeeman shifts or a conservative potential.

When every beam is weak and mutual coherences average away, the total force can be approximated by

F≃∑jℏkjRj.\mathbf F \simeq \sum_j \hbar\mathbf k_j R_j.

Each rate uses its own Doppler detuning and polarization coupling.

Independent Lorentzians fail when:

  • the total saturation is appreciable;
  • coherent beams form standing waves;
  • polarization varies in space;
  • several ground states support dark or bright superpositions;
  • stimulated processes couple the modes;
  • optical pumping changes the addressed state;
  • beat notes are slow on the internal timescale.

Then the force must be obtained from a multilevel master equation or equivalent dressed-state treatment using the full spatial field.

Two coherent beams with a frequency difference form a moving intensity and phase pattern. The atom can exchange momentum coherently between modes without a spontaneous event. Bragg diffraction, Raman transitions, and Bloch oscillations are not captured by adding independent scattering rates.

If the excited state decays to an undriven level, the nominal cycling rate is temporary. After roughly the inverse leakage probability in photon cycles, population accumulates outside the addressed transition. Repump lasers may restore cycling, but they add:

  • additional recoil directions;
  • new excited-state fractions;
  • coherences and dark states;
  • branching uncertainty;
  • frequency and polarization requirements.

The measured force is determined by the complete steady-state population flow, not by the strongest line alone.

Magnetic sublevels have different Clebsch–Gordan coefficients and polarization selection rules. A changing quantization axis or imperfect polarization can make s0s_0, branching, and the emission pattern depend on position and velocity.

Molecules often have many rovibrational decay channels. Strong radiation pressure requires highly diagonal branching and multiple repumps. A large absorption cross section does not guarantee many usable cycles.

In an optically thick cloud, incident intensity changes through the sample and emitted photons can be reabsorbed. Multiple scattering produces collective forces and extra diffusion. The independent-atom, undepleted-beam formula is then incomplete.

Directional Emission and Structured Reservoirs

Section titled “Directional Emission and Structured Reservoirs”

If spontaneous or stimulated emission is enhanced into a cavity mode, the mean emitted momentum need not vanish. The cycle force becomes

F=ℏ(kin−⟨kout⟩)R.\mathbf F = \hbar \left( \mathbf k_{\mathrm{in}} - \left\langle \mathbf k_{\mathrm{out}} \right\rangle \right) R.

Momentum bookkeeping must include the cavity mirrors and drive. A cavity can modify both damping and diffusion.

A one-dimensional waveguide can favor one propagation direction. Then emission itself supplies a directed average recoil. Such forces are not described by the free-space assumption ⟨ks⟩=0\langle\mathbf k_s\rangle=0.

Surfaces alter the electromagnetic mode density and radiation pattern. They can also exert conservative Casimir–Polder forces. Separating resonant recoil from static or dispersive surface forces requires one consistent environment model.

For a known interaction time,

Δp=∫F(t) dt.\Delta\mathbf p = \int \mathbf F(t)\,dt.

Time of flight, cloud displacement, atomic-beam deflection, and momentum-resolved imaging can infer this impulse. The analysis must include the changing Doppler detuning and spatial intensity.

Detected fluorescence is proportional to

Rdet=ηdetbdetRsc,R_{\mathrm{det}} = \eta_{\mathrm{det}} b_{\mathrm{det}} R_{\mathrm{sc}},

where ηdet\eta_{\mathrm{det}} is the collection and detection efficiency and bdetb_{\mathrm{det}} is the branching fraction into the detected channel. Fluorescence can calibrate the internal scattering rate, but it does not by itself determine the recoil direction or net force.

The growth of momentum variance tests the diffusion model. A force model that fits the mean displacement but underpredicts the width may be missing emission anisotropy, state switching, beam noise, standing-wave structure, or reabsorption.

Strong diagnostics include:

  1. reverse the beam direction and test the odd force component;
  2. reverse detuning and test the Doppler slope;
  3. vary intensity through saturation;
  4. change polarization and prepared magnetic sublevel;
  5. compare fluorescence with mechanical impulse;
  6. measure both mean momentum and variance;
  7. vary interaction time to expose transient internal dynamics;
  8. block repumps to reveal leakage from the cycling manifold.
  1. Declare the system boundary. Include the atom, relevant optical modes, environment, and any momentum-absorbing hardware needed for the conservation statement.
  2. Specify the internal states. List transition frequencies, linewidths, dipole matrix elements, branching, and repumps.
  3. State conventions. Define detuning, wave-vector direction, Rabi-frequency factors, and whether rates are angular frequencies.
  4. Write the rest-frame detuning. Derive the Doppler sign from the optical phase.
  5. Choose transient or steady dynamics. Compare pulse, transit, and motional times with internal relaxation.
  6. Calculate the internal state. Use optical Bloch equations or a multilevel master equation before inserting a scattering rate.
  7. Compute the mean force. Include both incident and emitted momentum.
  8. Compute force noise. State the diffusion convention and radiation pattern.
  9. Add conservative forces. Derive dipole or surface potentials from the same declared model.
  10. Propagate motion self-consistently. Update position, velocity, Doppler shift, and local intensity.
  11. Map to observables. Include detection efficiency, finite imaging resolution, and preparation uncertainty.
  12. Test limits and reversals. Recover weak-field cross sections, saturation, zero-force symmetry, and measured scaling.

Its mean may vanish while its variance remains finite. Ignoring the variance removes recoil heating.

Adding absorption without stimulated emission

Section titled “Adding absorption without stimulated emission”

At saturation, stimulated return is essential. The net directed photon removal rate approaches Γ/2\Gamma/2, not an unbounded absorption rate.

This page uses Δ=ω0−ωL\Delta=\omega_0-\omega_L, so red detuning is positive and Δv=Δ+k⋅v\Delta_v=\Delta+\mathbf k\cdot\mathbf v.

Applying the steady force to a short pulse

Section titled “Applying the steady force to a short pulse”

If the internal state has not relaxed, use time-dependent dynamics and integrate the force.

Calling every optical force radiation pressure

Section titled “Calling every optical force radiation pressure”

The conservative dipole force follows the light-shift gradient. The dissipative scattering force follows momentum redistribution. A focused beam can contain both.

Treating a cross section as intensity independent

Section titled “Treating a cross section as intensity independent”

The linear cross section applies at weak drive. Saturation makes the effective response depend on intensity.

Assuming a two-level formula for an open transition

Section titled “Assuming a two-level formula for an open transition”

Branching and optical pumping can stop the cycle long before the predicted steady force is reached.

Adding saturated beam forces independently

Section titled “Adding saturated beam forces independently”

Multiple strong coherent beams share populations and coherences. Their forces are not generally independent Lorentzians.

Inferring force from total fluorescence alone

Section titled “Inferring force from total fluorescence alone”

The force also depends on incident and emitted directions. Directional emission can change the mean recoil without changing the total count rate.

Diffusion and technical force noise can invalidate a model that reproduces the mean trajectory.

For one absorption–emission cycle,

Δp=ℏ(k−ks).\Delta\mathbf p = \hbar \left( \mathbf k-\mathbf k_s \right).

For a closed two-level atom,

Rsc=Γ2s01+s0+(2Δv/Γ)2,R_{\mathrm{sc}} = \frac{\Gamma}{2} \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 },

with

Δv=ω0−ωL+k⋅v.\Delta_v = \omega_0-\omega_L + \mathbf k\mathbin{\cdot}\mathbf v.

If mean spontaneous recoil vanishes,

Fsc=ℏkRsc,\mathbf F_{\mathrm{sc}} = \hbar\mathbf k R_{\mathrm{sc}},

and

Fmax⁡=ℏkΓ2.F_{\max} = \frac{ \hbar k\Gamma }{ 2 }.

In the weak-field limit,

σ(Δv)=3λ2/(2π)1+(2Δv/Γ)2,\sigma(\Delta_v) = \frac{ 3\lambda^2/(2\pi) }{ 1+ \left( 2\Delta_v/\Gamma \right)^2 },

for an ideal closed cycling transition.

The recoil scales are

pr=ℏk,vr=ℏkm,Er=ℏ2k22m.p_r=\hbar k, \qquad v_r=\frac{\hbar k}{m}, \qquad E_r=\frac{\hbar^2k^2}{2m}.

For two weak counterpropagating red-detuned beams,

F(v)≃−αv,F(v) \simeq -\alpha v,

where

α=8ℏk2s0(Δ/Γ)[1+(2Δ/Γ)2]2\alpha = \frac{ 8\hbar k^2s_0 \left( \Delta/\Gamma \right) }{ \left[ 1+ \left( 2\Delta/\Gamma \right)^2 \right]^2 }

is positive for Δ>0\Delta>0 under this page’s convention.

  • Laser Cooling turns the force and recoil ledger into a distribution-level cooling theory, including friction–diffusion balance, capture, thermometry, and the map of sub-Doppler and sideband mechanisms.
  • Laser Cooling Simulation Notebook verifies the balanced two-beam force, numerical friction, declared recoil diffusion, Doppler temperature, and relaxation benchmark.
  • Sub-Doppler Cooling explains how multilevel light shifts, coherent dark states, and resolved motional sidebands evade the two-level Doppler assumptions.
  • Stimulated Emission explains the downward process that opposes absorption momentum in the driven beam.
  • Line Shapes and Broadening develops homogeneous, Doppler, transit, collision, and instrumental broadening.
  • Transition Rates connects internal branching and detector channels to measured photon counts.
  • Quantum Noise supplies the spectral and correlation language for force fluctuations.
  • Trapped Ions shows how photon recoil changes quantized motional states during cooling, control, and readout.
  • Momentum Eigenstates records the translation-generator and plane-wave conventions behind photon recoil.
  1. A. Ashkin, “Acceleration and Trapping of Particles by Radiation Pressure,” Physical Review Letters 24, 156–159 (1970).
  2. A. Ashkin, “Atomic-Beam Deflection by Resonance-Radiation Pressure,” Physical Review Letters 25, 1321–1324 (1970).
  3. J. P. Gordon and A. Ashkin, “Motion of atoms in a radiation trap,” Physical Review A 21, 1606–1617 (1980).
  4. T. W. Hänsch and A. L. Schawlow, “Cooling of gases by laser radiation,” Optics Communications 13, 68–69 (1975).
  5. J. Dalibard and C. Cohen-Tannoudji, “Dressed-atom approach to atomic motion in laser light: the dipole force revisited,” Journal of the Optical Society of America B 2, 1707–1720 (1985).
  6. C. N. Cohen-Tannoudji, “Nobel Lecture: Manipulating atoms with photons,” Reviews of Modern Physics 70, 707–719 (1998).
  7. W. D. Phillips, “Nobel Lecture: Laser cooling and trapping of neutral atoms,” Reviews of Modern Physics 70, 721–741 (1998).
  8. H. J. Metcalf and P. van der Straten, Laser Cooling and Trapping, Springer (1999).
  9. C. Cohen-Tannoudji, J. Dupont-Roc, and G. Grynberg, Atom–Photon Interactions: Basic Processes and Applications, Wiley (1992).
  10. C. J. Foot, Atomic Physics, Oxford University Press (2005).

An atom absorbs from a beam with wave vector kz^k\widehat{\mathbf z} and spontaneously emits a photon of the same wave-number magnitude in direction n^\widehat{\mathbf n}. Assume an isotropic emission distribution.

  1. Find the mean momentum transfer per cycle.
  2. Find the variance of the zz component of the cycle impulse.
  3. Find the mean squared three-dimensional impulse.
Solution

The cycle impulse is

Δp=ℏk(z^−n^).\Delta\mathbf p = \hbar k \left( \widehat{\mathbf z} - \widehat{\mathbf n} \right).

Isotropy gives

⟨n^⟩=0,\left\langle \widehat{\mathbf n} \right\rangle = 0,

so

⟨Δp⟩=ℏkz^.\left\langle \Delta\mathbf p \right\rangle = \hbar k \widehat{\mathbf z}.

The fluctuating zz component is

Δpz−⟨Δpz⟩=−ℏknz.\Delta p_z - \left\langle \Delta p_z \right\rangle = -\hbar k n_z.

Since ⟨nz2⟩=1/3\langle n_z^2\rangle=1/3,

Var⁡(Δpz)=ℏ2k23.\operatorname{Var}(\Delta p_z) = \frac{ \hbar^2k^2 }{ 3 }.

Finally,

⟨∣Δp∣2⟩=ℏ2k2⟨∣z^−n^∣2⟩=ℏ2k2(2−2⟨nz⟩)=2ℏ2k2.\begin{aligned} \left\langle |\Delta\mathbf p|^2 \right\rangle &= \hbar^2k^2 \left\langle |\widehat{\mathbf z}-\widehat{\mathbf n}|^2 \right\rangle \\ &= \hbar^2k^2 \left( 2 - 2\langle n_z\rangle \right) \\ &= 2\hbar^2k^2. \end{aligned}

The mean emitted recoil vanishes, but its fluctuations do not.

For a closed two-level atom,

ρeess=12s01+s0+(2Δv/Γ)2.\rho_{ee}^{\mathrm{ss}} = \frac12 \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 }.
  1. Derive RscR_{\mathrm{sc}} and Fsc\mathbf F_{\mathrm{sc}}.
  2. Maximize the force over detuning and intensity.
  3. Explain physically why the force saturates.
Solution

The spontaneous rate is

Rsc=Γρeess=Γ2s01+s0+(2Δv/Γ)2.R_{\mathrm{sc}} = \Gamma\rho_{ee}^{\mathrm{ss}} = \frac{\Gamma}{2} \frac{ s_0 }{ 1+s_0+ \left( 2\Delta_v/\Gamma \right)^2 }.

With zero mean emission recoil,

Fsc=ℏkRsc.\mathbf F_{\mathrm{sc}} = \hbar\mathbf k R_{\mathrm{sc}}.

For fixed s0s_0, the rate is largest at Δv=0\Delta_v=0. The resonant factor is s0/(1+s0)s_0/(1+s_0), which approaches one as s0→∞s_0\to\infty. Therefore

Rmax⁡=Γ2,R_{\max} = \frac{\Gamma}{2},

and

Fmax⁡=ℏkΓ2.F_{\max} = \frac{ \hbar k\Gamma }{ 2 }.

Under strong continuous resonant drive, the closed two-level steady state approaches equal populations. Stimulated emission balances much of the absorption, so the net directed photon-removal rate equals the spontaneous reset rate and cannot exceed Γ/2\Gamma/2.

Use

λ=780 nm,Γ/(2π)=6.0 MHz,m=1.44×10−25 kg.\begin{aligned} \lambda &= 780\ \mathrm{nm}, \\ \Gamma/(2\pi) &= 6.0\ \mathrm{MHz}, \\ m &= 1.44\times10^{-25}\ \mathrm{kg}. \end{aligned}

At resonance and s0=1s_0=1, calculate:

  1. the scattering rate;
  2. the force and acceleration;
  3. the recoil velocity;
  4. the number of cycles and constant-force speed change in 5.0 μs5.0\ \mathrm{\mu s}.
Solution

At resonance with s0=1s_0=1,

Rsc=Γ4.R_{\mathrm{sc}} = \frac{\Gamma}{4}.

Numerically,

Γ=2π(6.0×106)≃3.77×107 s−1,\Gamma = 2\pi \left( 6.0\times10^6 \right) \simeq 3.77\times10^7\ \mathrm{s^{-1}},

so

Rsc≃9.42×106 s−1.R_{\mathrm{sc}} \simeq 9.42\times10^6\ \mathrm{s^{-1}}.

The recoil momentum is

ℏk=hλ≃8.49×10−28 kg m s−1.\hbar k = \frac{h}{\lambda} \simeq 8.49\times10^{-28}\ \mathrm{kg\,m\,s^{-1}}.

Therefore

F=ℏkRsc≃8.00×10−21 N,a=Fm≃5.56×104 m s−2.\begin{aligned} F &= \hbar kR_{\mathrm{sc}} \simeq 8.00\times10^{-21}\ \mathrm N, \\ a &= \frac{F}{m} \simeq 5.56\times10^4\ \mathrm{m\,s^{-2}}. \end{aligned}

The recoil velocity is

vr=ℏkm≃5.90×10−3 m s−1.v_r = \frac{\hbar k}{m} \simeq 5.90\times10^{-3}\ \mathrm{m\,s^{-1}}.

In 5.0 μs5.0\ \mathrm{\mu s},

N=Rsct≃47.1,N = R_{\mathrm{sc}}t \simeq 47.1,

and

Δv=Nvr≃0.278 m s−1.\Delta v = Nv_r \simeq 0.278\ \mathrm{m\,s^{-1}}.

The Doppler shift should be checked before extending the constant-force estimate to longer times.

For an ideal cycling transition, use

Isat=πhcΓ3λ3I_{\mathrm{sat}} = \frac{ \pi h c\Gamma }{ 3\lambda^3 }

and the weak resonant rate

Rsc≃Γ2IIsat.R_{\mathrm{sc}} \simeq \frac{\Gamma}{2} \frac{I}{I_{\mathrm{sat}}}.

Show that Rsc=Φγσ0R_{\mathrm{sc}}=\Phi_\gamma\sigma_0 with Φγ=I/(ℏω)\Phi_\gamma=I/(\hbar\omega) and find σ0\sigma_0.

Solution

Substitution gives

Rsc=Γ2I3λ3πhcΓ=I3λ32πhc.\begin{aligned} R_{\mathrm{sc}} &= \frac{\Gamma}{2} I \frac{ 3\lambda^3 }{ \pi h c\Gamma } \\ &= I \frac{ 3\lambda^3 }{ 2\pi h c }. \end{aligned}

The photon flux is

Φγ=Iℏω=Iλhc.\Phi_\gamma = \frac{I}{\hbar\omega} = \frac{ I\lambda }{ h c }.

Therefore

σ0=RscΦγ=3λ22π.\sigma_0 = \frac{ R_{\mathrm{sc}} }{ \Phi_\gamma } = \frac{ 3\lambda^2 }{ 2\pi }.

This equality relies on the same ideal cycling-transition and polarization conventions used to define IsatI_{\mathrm{sat}}.

5. Derive the Doppler friction coefficient

Section titled “5. Derive the Doppler friction coefficient”

Two equal weak beams counterpropagate along xx. Use

F(v)=ℏkΓs02[11+[2(Δ+kv)/Γ]2−11+[2(Δ−kv)/Γ]2].\begin{aligned} F(v) = \frac{\hbar k\Gamma s_0}{2} \Bigg[ & \frac{ 1 }{ 1+ \left[ 2(\Delta+kv)/\Gamma \right]^2 } \\ &- \frac{ 1 }{ 1+ \left[ 2(\Delta-kv)/\Gamma \right]^2 } \Bigg]. \end{aligned}

Expand to first order in vv and determine which detuning gives damping.

Solution

Define

f(x)=11+(2x/Γ)2.f(x) = \frac{ 1 }{ 1+ \left( 2x/\Gamma \right)^2 }.

Then

f′(x)=−8x/Γ2[1+(2x/Γ)2]2.f'(x) = - \frac{ 8x/\Gamma^2 }{ \left[ 1+ \left( 2x/\Gamma \right)^2 \right]^2 }.

For small velocity,

f(Δ+kv)−f(Δ−kv)≃2kvf′(Δ).f(\Delta+kv) - f(\Delta-kv) \simeq 2kv f'(\Delta).

Using the derivative above,

2kvf′(Δ)=−16kvΔ/Γ2[1+(2Δ/Γ)2]2.2kv f'(\Delta) = - \frac{ 16kv\Delta/\Gamma^2 }{ \left[ 1+ \left( 2\Delta/\Gamma \right)^2 \right]^2 }.

Hence

F(v)≃−αv,F(v) \simeq -\alpha v,

with

α=8ℏk2s0(Δ/Γ)[1+(2Δ/Γ)2]2.\alpha = \frac{ 8\hbar k^2s_0 \left( \Delta/\Gamma \right) }{ \left[ 1+ \left( 2\Delta/\Gamma \right)^2 \right]^2 }.

This page uses Δ=ω0−ωL\Delta=\omega_0-\omega_L. Red detuning has Δ>0\Delta>0, so α>0\alpha>0 and the force opposes velocity. Blue detuning gives antidamping.

6. Convert recoil noise to a diffusion coefficient

Section titled “6. Convert recoil noise to a diffusion coefficient”

An incident beam propagates along zz. Scattering events form a Poisson process of rate RscR_{\mathrm{sc}}, and spontaneous emission is isotropic. Use the convention

ddtVar⁡(pz)=2Dp,z.\frac{d}{dt} \operatorname{Var}(p_z) = 2D_{p,z}.

Find Dp,zD_{p,z}. Also find the average three-dimensional recoil-energy injection rate.

Solution

Poisson fluctuations in the number of absorption kicks contribute ℏ2k2Rsc\hbar^2k^2R_{\mathrm{sc}} to the variance-growth rate. Isotropic spontaneous emission contributes

13ℏ2k2Rsc.\frac13 \hbar^2k^2 R_{\mathrm{sc}}.

Thus

ddtVar⁡(pz)=43ℏ2k2Rsc,\frac{d}{dt} \operatorname{Var}(p_z) = \frac43 \hbar^2k^2 R_{\mathrm{sc}},

and

Dp,z=23ℏ2k2Rsc.D_{p,z} = \frac23 \hbar^2k^2 R_{\mathrm{sc}}.

The mean squared three-dimensional cycle impulse is 2ℏ2k22\hbar^2k^2. Its recoil-energy contribution per cycle is 2Er2E_r, so

E˙rec=2ErRsc.\dot E_{\mathrm{rec}} = 2E_r R_{\mathrm{sc}}.

This is the independent-cycle result. Dipole-pattern anisotropy and correlated resonance fluorescence change the detailed coefficients.

A far-detuned Gaussian beam has local Rabi frequency

∣Ω(r)∣2=Ω02exp⁡(−2r2w02).|\Omega(r)|^2 = \Omega_0^2 \exp \left( - \frac{2r^2}{w_0^2} \right).

Assume Δ>0\Delta>0 and ∣Δ∣≫Γ,∣Ω∣|\Delta|\gg\Gamma,|\Omega|.

  1. Find the radial dipole force.
  2. Find the local scattering rate.
  3. State the direction of each force near the beam axis.
Solution

The ground-state potential is

Ug(r)=−ℏΩ024Δexp⁡(−2r2w02).U_g(r) = - \frac{ \hbar\Omega_0^2 }{ 4\Delta } \exp \left( - \frac{2r^2}{w_0^2} \right).

Differentiating,

Frdip=−ℏΩ02Δrw02exp⁡(−2r2w02).F_r^{\mathrm{dip}} = - \frac{ \hbar\Omega_0^2 }{ \Delta } \frac{r}{w_0^2} \exp \left( - \frac{2r^2}{w_0^2} \right).

For Δ>0\Delta>0 and r>0r>0, this is negative: the red-detuned dipole force points toward the beam axis.

The scattering rate is

Rsc(r)≃ΓΩ024Δ2exp⁡(−2r2w02).R_{\mathrm{sc}}(r) \simeq \frac{ \Gamma\Omega_0^2 }{ 4\Delta^2 } \exp \left( - \frac{2r^2}{w_0^2} \right).

Its mean force points mainly along the beam propagation direction, not radially, if the spontaneous recoil averages to zero. The focused beam therefore provides radial conservative confinement and longitudinal dissipative push at the same time.

An experiment drives a nominally cycling transition and infers Rsc=8×106 s−1R_{\mathrm{sc}}=8\times10^6\ \mathrm{s^{-1}} from fluorescence. The measured acceleration is only half of ℏkRsc/m\hbar kR_{\mathrm{sc}}/m, and the momentum width grows three times faster than an isotropic independent-cycle model predicts.

List plausible physical and instrumental causes and design a compact validation program.

Solution

The discrepancies need not have one cause. Plausible mechanisms include:

  • an incorrect collection efficiency or detected branching fraction;
  • optical pumping into weakly pushed or dark states;
  • repump photons arriving from other directions;
  • directional spontaneous emission;
  • standing-wave or retroreflection effects;
  • spatial averaging over intensity and detuning;
  • Doppler detuning during the pulse;
  • laser amplitude, pointing, or frequency noise;
  • reabsorption and multiple scattering;
  • preparation or momentum-imaging calibration errors;
  • extra diffusion from state switching or dipole-force fluctuations.

A compact validation program should:

  1. reverse the pushing beam and verify reversal of the mean impulse;
  2. measure fluorescence, mean momentum, and momentum variance in the same sequence;
  3. scan intensity through saturation and detuning across resonance;
  4. vary pulse duration to distinguish transients from steady force;
  5. resolve final internal-state populations and block each repump in turn;
  6. change polarization and magnetic bias field;
  7. remove retroreflections and map the beam profile;
  8. repeat at several optical depths;
  9. calibrate collection efficiency with an independent lifetime or photon standard;
  10. fit a multilevel master equation coupled to stochastic recoil.

Agreement requires one model to explain the internal count rate, directed momentum, and diffusion. Matching fluorescence alone does not validate the mechanical force.