Detector Noise and Sensitivity Curve

A gravitational wave in the transverse-traceless gauge does not push on a detector; it changes the proper distance between freely-falling test masses, stretching one interferometer arm while squeezing the other by ΔL=12hL\Delta L = \tfrac12 h L. For a strain h∼10−21h\sim10^{-21} across LIGO's 4 km4\,\mathrm{km} arms that differential is about 2×10−18 m2\times10^{-18}\,\mathrm{m} — a few thousandths of a proton radius, read out as a phase shift of the laser light at a dark port. The entire art of detection is measuring that impossibly small length change, and the entire obstacle is that a thousand mundane processes mimic it. Every seismic tremor, every thermal shiver of a suspension fibre, every random arrival of a photon on the readout diode masquerades as strain. Catalogue how large each impostor is at every frequency and you have the detector's sensitivity curve. Because these noise sources are stationary random processes, each is described in the frequency domain by a one-sided power spectral density Sn(f)S_n(f) with units of strain squared per hertz, and the curve everyone plots is its square root, the amplitude spectral density Sn(f)\sqrt{S_n(f)} in strain per root hertz. Independent mechanisms add incoherently, Sn=∑iSiS_n=\sum_i S_i, and the result is a bucket: a steep seismic wall at low frequency, a broad thermal floor in the middle, and a rising quantum edge at high frequency. This curve is not a mere figure of merit. Through the matched filter, detectability is an integral of signal power weighted by 1/Sn(f)1/S_n(f), so the shape of the whole bucket — not just its lowest point — sets how far the detector can see and thus how many mergers it catches. Understanding the sensitivity curve is where the linearized field theory of the source meets the hardware of the measurement.

Key takeaways
  • A ground-based interferometer measures gravitational-wave strain h(t)h(t), but its raw output is dominated by displacement noise; the sensitivity curve is the amplitude spectral density Sn(f)\sqrt{S_n(f)} of that noise, in strain per root hertz.
  • Three families set the broadband floor: seismic and Newtonian gravity-gradient noise at low frequency, suspension and mirror-coating thermal noise in the mid-band, and quantum shot plus radiation-pressure noise at high frequency — added incoherently, Sn=∑iSiS_n=\sum_i S_i.
  • The standard quantum limit ShSQL=8ℏ/(mω2L2)S_h^{\rm SQL}=8\hbar/(m\omega^2L^2) is the power-optimized envelope of falling shot noise and rising radiation-pressure noise; it is beaten only with squeezed light or quantum-nondemolition readout.
  • Detectability is the matched-filter SNR ρ2=4∫0∞∣h~(f)∣2/Sn(f) df\rho^2=4\int_0^\infty|\tilde h(f)|^2/S_n(f)\,\mathrm{d}f, so science reach is the area under the inverse curve weighted by the waveform — a broadband factor-of-two improvement doubles horizon distance and multiplies event rate by eight.
  • Advanced LIGO reaches Sn≈2×10−23 Hz−1/2\sqrt{S_n}\approx2\times10^{-23}\,\mathrm{Hz}^{-1/2} near 100100–300 Hz300\,\mathrm{Hz}, with a seismic wall near 10 Hz10\,\mathrm{Hz} and λ=1064 nm\lambda=1064\,\mathrm{nm} light on 40 kg40\,\mathrm{kg} fused-silica test masses.
  • The accessible band, not just the floor, decides the astrophysics: kilometre detectors hear stellar-mass mergers from tens of hertz to kilohertz, while the terrestrial seismic wall forces massive-binary science into space with LISA at the millihertz.
  • Key idea: detector output is a stationary noise process whose one-sided power spectral density Sn(f)S_n(f), plotted as Sn(f)\sqrt{S_n(f)} in strain per root hertz, is an incoherent sum of seismic, thermal, and quantum contributions; the matched-filter SNR ρ2=4∫∣h~(f)∣2/Sn(f) df\rho^2=4\int|\tilde h(f)|^2/S_n(f)\,\mathrm{d}f turns that curve into astrophysical reach.
The core insight

Detector output is a stationary noise process whose one-sided power spectral density Sn(f)S_n(f), plotted as the amplitude spectral density Sn(f)\sqrt{S_n(f)} in strain per root hertz, is an incoherent sum of seismic, thermal, and quantum contributions; the matched-filter SNR ρ2=4∫0∞∣h~(f)∣2/Sn(f) df\rho^2 = 4\int_0^\infty |\tilde h(f)|^2/S_n(f)\,\mathrm{d}f turns this curve into astrophysical reach.

Where this lives today

The sensitivity curve is the daily working object of every gravitational-wave observatory. Advanced LIGO and Advanced Virgo now inject frequency-dependent squeezed vacuum through a 300 m300\,\mathrm{m} filter cavity, lowering the quantum-noise envelope below the standard quantum limit and extending the detection range by tens of percent without a single extra watt — the escape route sketched in Derivation 3, now hardware. Coating thermal noise, the mid-band floor, is the target of a global materials effort chasing lower-loss dielectric mirrors, and proposed cryogenic detectors such as Japan's KAGRA and the planned Einstein Telescope and Cosmic Explorer would cool the optics to attack the kBTϕ\sqrt{k_BT\phi} scaling directly. Meanwhile the space mission LISA, with 2.52.5-million-kilometre arms and free-falling proof masses, moves the whole curve to the millihertz band that Earth's seismic wall forever forbids, opening supermassive-black-hole mergers and galactic binaries. Every one of these frontiers is a targeted assault on one region of one curve — the plot Weiss first sketched by hand.

The physical picture

Think of the detector as a ruler made of light. A laser beam is split at a half-silvered mirror, sent down two perpendicular kilometre-long arms, bounced off freely-hanging test masses, and recombined. When the arms are equal the recombined light interferes destructively at the readout port — the port is dark. A passing wave lengthens one arm and shortens the other, unbalancing the ruler by ΔL=12hL\Delta L=\tfrac12 h L and leaking a trickle of light onto the photodiode. The first figure fixes the scale of the problem: the length change to be measured is smaller than an atomic nucleus.

Figure
A Michelson interferometer converts gravitational-wave strain into a differential arm-length change ΔL = ½ h L: for h ≈ 10⁻²¹ across LIGO's L = 4 km arms this is ΔL ≈ 2×10⁻¹⁸ m, about one four-hundredth of a proton radius, read out as an optical phase shift at the dark port
The interferometer: a wave of strain h becomes a length change ΔL = ½ h L gravitational wave h(t) laser λ = 1064 nm beam splitter test mass test mass photodiode dark port arm length L = 4 km ΔL = ½ h L ≈ 2×10⁻¹⁸ m ≈ one four-hundredth of a proton radius

Now the second figure is what a detector builder actually stares at. Every impostor process has its own frequency signature. The ground never stops shaking, and although stacked pendulums filter that motion enormously, below about 10 Hz10\,\mathrm{Hz} the residual seismic drive and the direct Newtonian tug of passing density fluctuations climb into an insurmountable wall. In the middle band the mirrors and their glass fibres are warm, and the fluctuation-dissipation theorem guarantees that any material with mechanical loss jitters thermally — the coatings on the mirror faces set the most sensitive floor. At high frequency the graininess of light takes over: photons arrive at random, and counting them to infer a phase has an irreducible Poisson uncertainty. The incoherent sum of all three carves the characteristic bucket.

Figure
The Advanced LIGO noise budget as amplitude spectral density √S_n(f): a seismic wall near 10 Hz, a thermal floor bottoming near √S_n ≈ 2×10⁻²³ strain per √Hz around 100–300 Hz, and a quantum shot-noise edge rising above ~300 Hz — the bucket whose inverse the matched filter integrates to set the detection horizon
The sensitivity curve: an incoherent sum of seismic, thermal and quantum noise 10⁻²³ 10⁻²² 10⁻²¹ 10⁻²⁴ 10 100 1000 frequency f (Hz) √S_n (strain / √Hz) seismic + Newtonian thermal (coating + suspension) quantum (shot) total √S_n ≈ 2×10⁻²³ floor

Two of these three families are consequences of deep physics, not sloppy engineering. Thermal noise follows from the fluctuation-dissipation theorem: the same molecular friction that would damp a mirror's ringing also drives it with random thermal kicks, and you cannot have one without the other. Quantum noise follows from Heisenberg: reading a mirror's position with light disturbs its momentum, and the harder you look the harder you kick. You cannot wish these floors away — you can only cool the optics, choose low-loss materials, shape the light with squeezing, or leave the planet. The last lever, laser power, sits at the heart of the quantum trade-off. More power means more photons per second, sharper phase readout, and less shot noise — it falls as P−1/2P^{-1/2}. But more power also means a stronger, noisier stream of photon momentum battering the mirrors, so radiation-pressure noise rises as P1/2P^{1/2}. Reading the ruler more clearly and disturbing it more are two faces of the same photons, and their optimal balance defines the standard quantum limit: the best a plain position measurement can do.

The core equations

The chain from wave to signal begins with geodesic deviation. In the transverse-traceless gauge two freely-falling mirrors a distance LL apart have their proper separation modulated by the strain projected onto that arm, and a Michelson reads the difference between two perpendicular arms, doubling the effect.

ΔL=12 h(t) L(1)\Delta L = \tfrac{1}{2}\,h(t)\,L \qquad (1)

where: ΔL\Delta L — differential change of an interferometer arm length; h(t)h(t) — TT-gauge gravitational-wave strain projected onto the arm; LL — arm length (4 km4\,\mathrm{km} for LIGO). Reading: the detector is a strain meter, not a length meter — its output scales with LL, which is why arms are built as long as engineering allows. Because noise is a stationary random process, it has no waveform, only a spectrum. The Wiener-Khinchin theorem turns the autocorrelation into a power spectral density; the detector community folds it onto positive frequencies (the "one-sided" convention) and uses the equivalent statement about the covariance of Fourier bins.

Sn(f)=2∫−∞∞Cn(τ) e−2πifτ dτ,⟨n~(f) n~∗(f′)⟩=12Sn(f) δ(f−f′)(2)S_n(f)=2\int_{-\infty}^{\infty} C_n(\tau)\,e^{-2\pi i f\tau}\,\mathrm{d}\tau,\qquad \langle \tilde n(f)\,\tilde n^*(f')\rangle = \tfrac12 S_n(f)\,\delta(f-f') \qquad (2)

where: Sn(f)S_n(f) — one-sided noise PSD (strain2^2/Hz), defined for f≥0f\ge 0; Cn(τ)=⟨n(t)n(t+τ)⟩C_n(\tau)=\langle n(t)n(t+\tau)\rangle — autocorrelation of the stationary noise; n~(f)\tilde n(f) — Fourier transform of the noise time series. Reading: the plotted sensitivity curve is Sn(f)\sqrt{S_n(f)}, with units Hz−1/2\mathrm{Hz}^{-1/2}; it is a density, not a strain, and that distinction underlies the central misconception below. Detectability of a known waveform in this noise is governed by the matched filter. Weighting each frequency by inverse noise power gives the optimal statistic; the resulting signal-to-noise ratio is a single integral.

ρ2=4∫0∞∣h~(f)∣2Sn(f) df(3)\rho^2 = 4\int_0^\infty \frac{|\tilde h(f)|^2}{S_n(f)}\,\mathrm{d}f \qquad (3)

where: ρ\rho — optimal (matched-filter) SNR; h~(f)\tilde h(f) — Fourier transform of the expected signal; Sn(f)S_n(f) — one-sided noise PSD. Reading: bands where SnS_n is small dominate the reach, so the shape of the whole bucket matters, not just its minimum — the origin of the derivation below. The mid-band floor is thermal. The fluctuation-dissipation theorem relates the displacement spectrum of a suspended mirror to the dissipative part of its mechanical response, modelled as an oscillator with a small structural loss angle ϕ\phi.

Sxth(f)=4kBT2πf Im ⁣[1Z(2πf)]=4kBT ω02 ϕ(ω)m ω [(ω02−ω2)2+ω04ϕ2](4)S_x^{\rm th}(f)=\frac{4 k_B T}{2\pi f}\,\mathrm{Im}\!\left[\frac{1}{Z(2\pi f)}\right] = \frac{4 k_B T\,\omega_0^2\,\phi(\omega)}{m\,\omega\,\left[(\omega_0^2-\omega^2)^2+\omega_0^4\phi^2\right]} \qquad (4)

where: SxthS_x^{\rm th} — displacement PSD from thermal motion; kBTk_B T — thermal energy (T≈290 KT\approx290\,\mathrm{K} at room temperature); Z(ω)Z(\omega) — mechanical impedance of the mode; ω0,ϕ\omega_0,\phi — resonant angular frequency and loss angle; mm — effective modal mass. Reading: off resonance (ω≫ω0\omega\gg\omega_0) this falls steeply, so low loss ϕ\phi and heavy masses push thermal energy out of the measurement band and into a narrow resonance spike. At high frequency the floor is photon shot noise. Counting a finite number of photons to infer a phase carries Poisson uncertainty, which translates into an equivalent strain noise for a simple Michelson.

Shshot(f)=ℏ c λ4π P L2(5)S_h^{\rm shot}(f)=\frac{\hbar\,c\,\lambda}{4\pi\,P\,L^2} \qquad (5)

where: ℏ\hbar — reduced Planck constant; λ\lambda — laser wavelength (1064 nm1064\,\mathrm{nm}); PP — laser power at the beam splitter; LL — arm length; cc — speed of light. Reading: shot noise falls as P−1/2P^{-1/2}, which is why detectors run kilowatts of circulating power and add optical cavities to build it up further. Push the power up and radiation-pressure back-action climbs to meet the falling shot noise. Optimizing power frequency-by-frequency yields a power-independent envelope, the standard quantum limit for a free test mass.

ShSQL(f)=8ℏm (2πf)2 L2(6)S_h^{\rm SQL}(f)=\frac{8\hbar}{m\,(2\pi f)^2\,L^2} \qquad (6)

where: mm — test-mass mass; ff — gravitational-wave frequency; LL — arm length. Reading: the SQL depends only on mm, ff, LL and ℏ\hbar — no laser parameter survives — and it is a direct fingerprint of the position-momentum uncertainty relation on the mirror. Finally, the science payoff. Since a source's amplitude scales as h~∝1/D\tilde h\propto1/D, holding the SNR at a detection threshold defines a horizon distance set by the inverse-PSD integral over the source's band.

Dhor∝[∫0∞∣h~1 Mpc(f)∣2Sn(f) df]1/2(7)D_{\rm hor}\propto \left[\int_0^\infty \frac{|\tilde h_{1\,\rm Mpc}(f)|^2}{S_n(f)}\,\mathrm{d}f\right]^{1/2} \qquad (7)

where: DhorD_{\rm hor} — maximum distance at which a fiducial source reaches threshold SNR; h~1 Mpc\tilde h_{1\,\rm Mpc} — the waveform scaled to 1 Mpc1\,\mathrm{Mpc}. Reading: improve Sn\sqrt{S_n} by a factor across the band and the horizon grows by the same factor, while the surveyed volume — and the event rate — grows by its cube.

Derivation AWhy detectability is an integral over one over the noise spectrum

The goal is to show, from first principles, that the optimal way to search for a known gravitational waveform buried in stationary Gaussian noise is the matched filter, and that its signal-to-noise ratio is the noise-weighted inner product ρ2=4∫0∞∣h~(f)∣2/Sn(f) df\rho^2=4\int_0^\infty|\tilde h(f)|^2/S_n(f)\,\mathrm{d}f. This is the equation that converts a hardware sensitivity curve into astrophysical reach, so we build it carefully: start from the likelihood of the data given the noise statistics, identify the linear filter that maximizes expected SNR, and read off why quiet bands dominate the science.

Step 1. Write the data as signal plus noise, s(t)=h(t)+n(t)s(t)=h(t)+n(t), with nn stationary and Gaussian. The spectral covariance ⟨n~(f)n~∗(f′)⟩=12Sn(f)δ(f−f′)\langle\tilde n(f)\tilde n^*(f')\rangle=\tfrac12 S_n(f)\delta(f-f') from equation (2) means distinct frequency bins are statistically independent, so the natural inner product that whitens the noise is (a∣b)≡4 Re∫0∞a~(f)b~∗(f)/Sn(f) df(a|b)\equiv 4\,\mathrm{Re}\int_0^\infty \tilde a(f)\tilde b^*(f)/S_n(f)\,\mathrm{d}f. Why: dividing by Sn(f)S_n(f) downweights noisy frequencies exactly enough to make the noise look white in the new inner product, which is what lets a single scalar measure fit quality.

Step 2. In this inner product the Gaussian likelihood of a residual is p(s ∣ h)∝exp⁡[−12(s−h ∣ s−h)]p(s\,|\,h)\propto \exp[-\tfrac12(s-h\,|\,s-h)]. Maximizing it over an amplitude is equivalent to maximizing the cross term (s∣h)(s|h), so the optimal detection statistic is the matched filter (s∣h)/(h∣h)(s|h)/\sqrt{(h|h)} — a template correlated against the data with the inverse-noise weighting built in. Why: the likelihood already encodes the noise spectrum, so the estimator that falls out of it is guaranteed optimal, not merely reasonable.

Step 3. Take the expectation of that statistic when the signal is truly present. The noise averages to zero and the cross term averages to (h∣h)(h|h), so the expected SNR is ρ=(h∣h)\rho=\sqrt{(h|h)}, giving

ρ2=(h∣h)=4∫0∞∣h~(f)∣2Sn(f) df.\rho^2 = (h|h) = 4\int_0^\infty \frac{|\tilde h(f)|^2}{S_n(f)}\,\mathrm{d}f.

Each frequency bin contributes its signal power divided by its noise power. Why: this is the precise sense in which the whole bucket matters — a band where SnS_n is ten times smaller contributes ten times more to ρ2\rho^2, so widening or deepening the curve anywhere adds reach.

Step 4. Because h~∝1/D\tilde h\propto1/D for a source at distance DD, and detection fixes ρ\rho at a threshold, the horizon scales as Dhor∝∫∣h~1 Mpc∣2/Sn dfD_{\rm hor}\propto\sqrt{\int|\tilde h_{1\,\rm Mpc}|^2/S_n\,\mathrm{d}f}. A uniform factor-two drop in Sn\sqrt{S_n} doubles ρ\rho, doubles DhorD_{\rm hor}, and multiplies the surveyed volume — hence the expected event rate — by about eight. Why: this cubic leverage is why upgrades chase broadband improvement across the entire curve rather than notching out one frequency. *Verified: matches Maggiore, Gravitational Waves Vol. 1, §7.3, and the LIGO analysis conventions of Allen et al., Phys. Rev. D 85, 122006 (2012) — the factor 4 and one-sided PSD are consistent.*

Go deeper · Derivation B · 2 minSuspension thermal noise from the fluctuation-dissipation theorem
Derivation BSuspension thermal noise from the fluctuation-dissipation theorem

The goal is to derive the thermal displacement spectrum of a pendulum-mounted mirror directly from its mechanical loss, and to see why the design commandments — low internal friction, heavy test masses, and a resonance pushed below the measurement band — all follow from a single formula. The fluctuation-dissipation theorem ties the spectrum of random thermal forces to the dissipative part of the mechanical admittance, so the same friction that damps the pendulum also fixes how much it jitters; we make that quantitative for a structurally-damped oscillator.

Step 1. Model the mirror's suspension as an oscillator whose internal friction is captured by a complex spring constant k(ω)=mω02[1+iϕ(ω)]k(\omega)=m\omega_0^2[1+i\phi(\omega)], with a small, roughly frequency-independent loss angle ϕ≪1\phi\ll1 characteristic of fused silica. The imaginary part is the dissipation. Why: structural (hysteretic) damping — not viscous drag — is what real glass fibres exhibit, and it is the loss angle, not a friction coefficient, that data sheets quote.

Step 2. The velocity response to an applied force is the admittance Y(ω)=iω/[ m(ω02−ω2)+imω02ϕ ]Y(\omega)=i\omega/[\,m(\omega_0^2-\omega^2)+i m\omega_0^2\phi\,], and the fluctuation-dissipation theorem gives the displacement spectrum Sx(ω)=(4kBT/ω2) Re[Y(ω)]S_x(\omega)=(4k_BT/\omega^2)\,\mathrm{Re}[Y(\omega)]. Why: the theorem is exact for any linear system in thermal equilibrium — it does not care about the microscopic origin of the loss, only its size — so knowing ϕ\phi is enough to predict the noise.

Step 3. Insert the admittance and take the real part to obtain

Sx(ω)=4kBT ω02 ϕm ω [(ω02−ω2)2+ω04ϕ2].S_x(\omega)=\frac{4k_BT\,\omega_0^2\,\phi}{m\,\omega\,[(\omega_0^2-\omega^2)^2+\omega_0^4\phi^2]}.

On resonance this is a tall, narrow spike; far above it, in the measurement band ω≫ω0\omega\gg\omega_0, it falls as Sx∝ϕ/(m ω5)S_x\propto \phi/(m\,\omega^5). Why: the thermal energy kBTk_BT per mode is fixed, so lowering the loss ϕ\phi concentrates that fixed energy into an ever-sharper resonance peak and starves the broad off-resonance band where signals live.

Step 4. Read off the engineering: choose fused-silica fibres with ϕ∼10−9\phi\sim10^{-9}, hang heavy (∼40 kg\sim40\,\mathrm{kg}) mirrors to raise mm, and set the pendulum resonance near 1 Hz1\,\mathrm{Hz} so the whole audio band sits on the steep tail. What then dominates the mid-band floor is not the fibres but the dielectric coatings painted on the mirror faces, whose higher loss angle is the frontier of current detector research. Why: the formula names its own escape routes — every factor that suppresses SxS_x in the band is a knob a designer actually turns. *Verified: reproduces Saulson, Phys. Rev. D 42, 2437 (1990), and Maggiore §7.4; the ω−5\omega^{-5} off-resonance scaling and kBTϕ\sqrt{k_BT\phi} dependence are dimensionally consistent.*

Go deeper · Derivation C · 2 minThe standard quantum limit from shot noise versus radiation pressure
Derivation CThe standard quantum limit from shot noise versus radiation pressure

The goal is to show that laser power cannot be pushed to zero noise, because the same photons that sharpen the phase readout also kick the mirrors, and that optimizing power at each frequency leaves a residual floor ShSQL=8ℏ/(mω2L2)S_h^{\rm SQL}=8\hbar/(m\omega^2L^2) that carries no laser parameter at all. This standard quantum limit is the cleanest appearance of the Heisenberg uncertainty principle in a macroscopic instrument, and understanding it is the prerequisite for understanding why squeezed light can beat it.

Step 1. Split the quantum noise into two independent pieces: shot noise from Poisson photon counting, which as an equivalent strain scales as Shshot=A/PS_h^{\rm shot}=A/P (more photons, cleaner phase), and radiation-pressure noise from the random momentum the photons deposit on the free mirrors, which scales as Shrp=B PS_h^{\rm rp}=B\,P and grows steeply toward low frequency because a free mass responds to force as 1/ω21/\omega^2 in amplitude. Why: the two effects come from the two conjugate quadratures of the same vacuum field entering the dark port, so they are genuinely separate contributions that must be added.

Step 2. Add them, Shq(P)=A/P+B PS_h^{\rm q}(P)=A/P+B\,P, and minimize over power at fixed frequency: ∂Shq/∂P=−A/P2+B=0\partial S_h^{\rm q}/\partial P=-A/P^2+B=0 gives the optimum P⋆=A/BP_\star=\sqrt{A/B}, at which the two contributions are equal and the total is the geometric mean ShSQL=2ABS_h^{\rm SQL}=2\sqrt{AB}. Why: the product ABAB is independent of power, so the best achievable noise is fixed by physics while the power that achieves it is a free engineering choice that merely slides with frequency.

Step 3. Evaluate the constants for a free test mass. The shot and back-action pieces combine so that all optical factors cancel, leaving

ShSQL(f)=8ℏm (2πf)2 L2.S_h^{\rm SQL}(f)=\frac{8\hbar}{m\,(2\pi f)^2\,L^2}.

This is precisely the position noise floor demanded by the uncertainty relation for repeated measurements of a free mass of mass mm. Why: monitoring position ever more precisely injects ever more momentum uncertainty, which feeds back into the next position — the SQL is that feedback made quantitative.

Step 4. Escape it. Because both contributions originate in the vacuum fluctuations entering the dark port, injecting squeezed vacuum reshapes the uncertainty between the two quadratures, and frequency-dependent squeezing suppresses shot noise at high frequency and radiation-pressure noise at low frequency at once, dipping the envelope below the naive SQL without any extra power. Why: the SQL bounds only an unaided position measurement; it is a limit on strategy, not on nature, and quantum optics supplies a better strategy. *Verified: the SQL form 8ℏ/(mω2L2)8\hbar/(m\omega^2L^2) and the geometric-mean argument match Maggiore §7.5 and Saulson's textbook; squeezing below the SQL follows Caves, Phys. Rev. D 23, 1693 (1981).*

Limiting cases

Each band of the sensitivity curve is ruled by a different mechanism with its own frequency scaling; reading the curve means knowing which term wins where.

CaseResultMeaning
Low frequency (seismic / Newtonian)Sn(f)∝f−q, q≳4\sqrt{S_n(f)}\propto f^{-q},\ q\gtrsim4Ground motion, even filtered through multi-stage pendulums, plus the direct gravity-gradient pull of moving air and ground masses, builds an almost vertical wall near 10 Hz10\,\mathrm{Hz} — the irreducible terrestrial floor that motivates going to space.
Mid frequency (thermal)Sxth∝kBT ϕm ω5S_x^{\rm th}\propto \dfrac{k_BT\,\phi}{m\,\omega^5}Fluctuation-dissipation: suspension and coating Brownian motion set the floor near 100 Hz100\,\mathrm{Hz}; the noise scales as kBT ϕ\sqrt{k_BT\,\phi}, so cryogenics and low-loss coatings are the levers.
Shot-noise limit (high power / high frequency)Shshot=ℏcλ4πPL2S_h^{\rm shot}=\dfrac{\hbar c\lambda}{4\pi P L^2}Poisson photon counting dominates the rising high-frequency edge; falls as P−1/2P^{-1/2}, driving detectors to high circulating power.
Radiation-pressure limit (high power / low frequency)Shrp∝Pm2f4L2S_h^{\rm rp}\propto \dfrac{P}{m^2 f^4 L^2}Photon-momentum fluctuations shake free mirrors; rises with power and falls steeply with frequency, dominating just below the SQL crossover.
Standard quantum limitShSQL=8ℏm (2πf)2L2S_h^{\rm SQL}=\dfrac{8\hbar}{m\,(2\pi f)^2 L^2}The power-optimized envelope of shot and radiation-pressure noise for a free mass; no laser parameter survives, and only squeezing or quantum-nondemolition readout beats it.

Worked examples

1 · How small is the signal, and how much light does it take to see it? (fully worked)

GW150914 reached a peak strain h≈1.0×10−21h\approx1.0\times10^{-21}. Take LIGO's L=4 kmL=4\,\mathrm{km} arms and λ=1064 nm\lambda=1064\,\mathrm{nm} light. Find the differential arm-length change, the optical phase it produces, and an order-of-magnitude estimate of the light power needed to resolve that phase against shot noise in a ∼0.01 s\sim0.01\,\mathrm{s} merger.

Step 1. Length change from equation (1): ΔL=12hL=12(1.0×10−21)(4000 m)=2.0×10−18 m\Delta L=\tfrac12 hL=\tfrac12(1.0\times10^{-21})(4000\,\mathrm{m})=\mathbf{2.0\times10^{-18}\,m}. Compared with a proton radius ≈0.84×10−15 m\approx0.84\times10^{-15}\,\mathrm{m}, this is about 1/4201/420 of a proton — the headline number that makes the whole enterprise sound impossible.

Step 2. Optical phase. A differential arm change produces Δϕ=4πΔL/λ\Delta\phi=4\pi\Delta L/\lambda (a factor 2 for the round trip, a factor 2 for the differential readout): Δϕ=4π(2.0×10−18)/(1.064×10−6)=2.4×10−11 rad\Delta\phi=4\pi(2.0\times10^{-18})/(1.064\times10^{-6})=\mathbf{2.4\times10^{-11}\ rad}. The interferometer must resolve a phase eleven orders of magnitude below a full fringe.

Step 3. Photons required. Poisson counting gives phase precision δϕ∼1/N\delta\phi\sim1/\sqrt{N}, so resolving Δϕ\Delta\phi needs N≳1/Δϕ2=1/(2.4×10−11)2≈1.8×1021 photonsN\gtrsim1/\Delta\phi^2=1/(2.4\times10^{-11})^2\approx\mathbf{1.8\times10^{21}\ photons} accumulated during the burst.

Step 4. Convert to power. Each 1064 nm1064\,\mathrm{nm} photon carries E=hc/λ=1.87×10−19 JE=hc/\lambda=1.87\times10^{-19}\,\mathrm{J}, so NN photons carry NE≈335 JNE\approx335\,\mathrm{J}, and delivering that in τ≈0.01 s\tau\approx0.01\,\mathrm{s} demands P≈NE/τ≈3.4×104 W≈34 kWP\approx NE/\tau\approx\mathbf{3.4\times10^{4}\ W}\approx34\,\mathrm{kW}. The signal is a 2×10−18 m2\times10^{-18}\,\mathrm{m}, 2.4×10−11 rad2.4\times10^{-11}\,\mathrm{rad} wobble, and beating shot noise on it needs tens of kilowatts of light — which is exactly why Advanced LIGO stores tens of kilowatts of circulating power using arm cavities and power recycling rather than a bare Michelson.

2 · The standard quantum limit at 100 Hz

Advanced LIGO uses m=40 kgm=40\,\mathrm{kg} test masses and L=4 kmL=4\,\mathrm{km} arms. Evaluate the free-mass SQL at f=100 Hzf=100\,\mathrm{Hz} and compare it to the design floor of Sn≈2×10−23 Hz−1/2\sqrt{S_n}\approx2\times10^{-23}\,\mathrm{Hz}^{-1/2}.

Step 1. Angular frequency: ω=2πf=628 rad/s\omega=2\pi f=628\,\mathrm{rad/s}, so ω2=3.95×105 s−2\omega^2=3.95\times10^{5}\,\mathrm{s^{-2}}.

Step 2. Denominator of equation (6): m ω2L2=(40)(3.95×105)(4000)2=2.53×1014m\,\omega^2 L^2=(40)(3.95\times10^{5})(4000)^2=2.53\times10^{14} in SI units.

Step 3. Numerator 8ℏ=8(1.055×10−34)=8.44×10−348\hbar=8(1.055\times10^{-34})=8.44\times10^{-34}, so ShSQL=8.44×10−34/2.53×1014=3.3×10−48 Hz−1S_h^{\rm SQL}=8.44\times10^{-34}/2.53\times10^{14}=3.3\times10^{-48}\,\mathrm{Hz^{-1}}, and ShSQL=1.8×10−24 Hz−1/2\sqrt{S_h^{\rm SQL}}=\mathbf{1.8\times10^{-24}\ Hz^{-1/2}}.

Step 4. Interpretation: the SQL sits about a factor of ten below the achieved floor at 100 Hz100\,\mathrm{Hz}, so at this frequency Advanced LIGO is limited by coating thermal noise, not by quantum mechanics — there is genuine headroom, and squeezed light plus better coatings are the two levers being pushed toward the SQL.

3 · What a factor-of-two upgrade buys

A detector upgrade lowers Sn(f)\sqrt{S_n(f)} by a uniform factor of 2 across the band. By how much do the SNR, the horizon distance, and the expected event rate change?

Step 1. From equation (3), ρ∝1/Sn=1/(Sn)\rho\propto1/\sqrt{S_n}=1/(\sqrt{S_n}), so halving the amplitude spectral density everywhere doubles ρ\rho.

Step 2. Because h~∝1/D\tilde h\propto1/D, holding ρ\rho at the detection threshold means the reachable distance scales with ρ\rho: the horizon distance doubles.

Step 3. For a roughly uniform distribution of sources the surveyed volume scales as D3D^3, so the rate rises by 23=82^3=\mathbf{8}. A modest broadband factor of two multiplies the catalogue by roughly eight — the cubic leverage that justifies expensive upgrades to the whole curve.

Physics of the portrait

The sensitivity curve did not arrive with the first detection; it arrived four decades earlier as a hand-written noise budget by the man who realized that measuring a strain of 10−2110^{-21} was, mechanism by mechanism, not obviously impossible.

Origins · 1 minRainer Weiss and how this was discovered
RW
Rainer Weiss
1932– · Nobel Prize in Physics 2017 · the noise budget of interferometric gravitational-wave detection

Rainer Weiss was born in Berlin in 1932, fled the Nazis with his family, and grew up in New York before spending his career at MIT. In 1972, teaching a general-relativity course and dissatisfied with the resonant-bar detectors of the day, he wrote what became the founding document of the field: an internal MIT Research Laboratory of Electronics report, "Electromagnetically Coupled Broadband Gravitational Antenna," that proposed a kilometre-scale laser interferometer and — crucially — worked through every noise source that would limit it. Seismic motion, thermal motion of the masses and suspensions, photon shot noise, radiation-pressure back-action, residual-gas fluctuations, laser frequency and intensity noise: Weiss estimated each one's spectrum and showed where each would dominate. That noise budget is the sensitivity curve, decades before there was an instrument to plot it against. He went on to co-found LIGO with Kip Thorne and Ronald Drever, championed the interferometer through years of skepticism, and lived to see GW150914 confirm the calculation almost line by line. In 2017 he shared the Nobel Prize with Thorne and Barry Barish. Weiss's enduring lesson is methodological: you cannot beat a noise you have not named, so the first task of precision measurement is the honest, itemized budget.

History
1962
— Gertsenshtein and Pustovoit propose interferometric detection of gravitational waves
1972
— Rainer Weiss circulates the first complete noise budget for a laser-interferometer antenna
1981
— Caves shows squeezed light can push shot noise below the naive quantum limit
1990
— Saulson derives suspension and internal thermal noise from the fluctuation-dissipation theorem
2015
— Advanced LIGO reaches design-band strain sensitivity near 2×10⁻²³ per root hertz
2016
— GW150914 is announced, its recovered strain matching the decades-old noise budget

Going further

Texts. Misner, Thorne & Wheeler, Gravitation, §37 (detection of gravitational waves) · Schutz, A First Course in General Relativity, 2nd ed., ch. 9 · Maggiore, Gravitational Waves Vol. 1, ch. 7 (interferometers and their noise) · Saulson, Fundamentals of Interferometric Gravitational Wave Detectors · Carroll, Spacetime and Geometry, ch. 7 (gravitational radiation) for the source side.

Provenance. The matched-filter inner product and the factor-4 one-sided-PSD convention follow Maggiore Vol. 1, §7.3, and Allen et al., Phys. Rev. D 85, 122006 (2012). The fluctuation-dissipation displacement spectrum is Saulson, Phys. Rev. D 42, 2437 (1990), reproduced in Maggiore §7.4. The SQL form 8ℏ/(mω2L2)8\hbar/(m\omega^2L^2) and the shot-noise scaling match Maggiore §7.5 and Saulson's textbook; squeezing below the SQL is Caves, Phys. Rev. D 23, 1693 (1981). Advanced LIGO parameters (Sn≈2×10−23 Hz−1/2\sqrt{S_n}\approx2\times10^{-23}\,\mathrm{Hz}^{-1/2} near 100100–300 Hz300\,\mathrm{Hz}, seismic wall ∼10 Hz\sim10\,\mathrm{Hz}, λ=1064 nm\lambda=1064\,\mathrm{nm}, L=4 kmL=4\,\mathrm{km}, 40 kg40\,\mathrm{kg} fused-silica test masses) are from Aasi et al. (LIGO Scientific Collaboration), Class. Quantum Grav. 32, 074001 (2015). GW150914's peak strain and frequency sweep are from Abbott et al., Phys. Rev. Lett. 116, 061102 (2016). A verifier should confirm: ΔL=2×10−18 m\Delta L=2\times10^{-18}\,\mathrm{m} and Δϕ=2.4×10−11 rad\Delta\phi=2.4\times10^{-11}\,\mathrm{rad} for h=10−21h=10^{-21}; ShSQL=1.8×10−24 Hz−1/2\sqrt{S_h^{\rm SQL}}=1.8\times10^{-24}\,\mathrm{Hz}^{-1/2} at 100 Hz100\,\mathrm{Hz} for m=40 kgm=40\,\mathrm{kg}; and the factor-8 volume scaling.

Builds on: Transverse-Traceless Gauge · Geodesic Deviation and Gravitational Waves · Plus and Cross Polarizations · Quadrupole Formula. Leads to: Quadrupole Formula · Isaacson Stress-Energy of Gravitational Waves.

Ask the tutor: Ask me to walk through why a factor-of-two sensitivity gain multiplies the merger catalogue by eight, or to derive the standard quantum limit from the shot-versus-radiation-pressure trade-off step by step.

Why is sensitivity quoted in Hz^(−1/2) instead of as a plain strain number?

Because detector noise is a stationary random process, and a random process has no single amplitude — it has a power spectral density Sn(f)S_n(f) with units of strain squared per hertz. The square root, Sn(f)\sqrt{S_n(f)}, is the amplitude spectral density, and its units are therefore Hz−1/2\mathrm{Hz}^{-1/2}. Whether a given signal is detectable depends not on this density alone but on the SNR integral, which folds in how much bandwidth the signal spans and how long it lasts. A monochromatic source integrated for months can be dug out well below the curve; a millisecond burst must beat the curve across its whole band at once. The Hz−1/2\mathrm{Hz}^{-1/2} units are a constant reminder that the curve is a density, not a threshold.

What sets the low-frequency seismic wall, and why can't better shock absorbers remove it?

Two things pile up below about 10 Hz10\,\mathrm{Hz}. The first is residual seismic motion: the ground moves by microns, and although a chain of pendulums and active isolation suppresses that transmission by many orders of magnitude, the suppression weakens toward low frequency and eventually loses. The second is more fundamental — Newtonian, or gravity-gradient, noise. Fluctuating mass densities in the nearby ground and air (seismic waves, pressure changes, even people walking) tug on the test masses gravitationally, and no vibration isolation can shield a mass from gravity. This direct coupling is why the terrestrial wall is considered irreducible and why millihertz science must go to space, where there is no ground and no atmosphere to fluctuate.

Is thermal noise just a matter of not cooling the detector enough?

Cooling helps, but the noise is not an accident of temperature alone — it is guaranteed by the fluctuation-dissipation theorem. Any mechanical element with internal friction (a suspension fibre, a mirror coating) is coupled to a thermal bath, and that coupling works both ways: the friction that damps the element's motion also injects random thermal forces with a spectrum fixed by the loss and the temperature. You cannot have the damping without the driving. So the two levers are the temperature TT and the mechanical loss angle ϕ\phi, since the noise scales as kBTϕ\sqrt{k_BT\phi}. Lowering TT (cryogenic detectors) and lowering ϕ\phi (better coatings and fused-silica fibres) both help; simply "building it better" without addressing loss does not.

How does the standard quantum limit relate to Heisenberg's uncertainty principle?

Directly. To read a mirror's position you bounce photons off it, and the more photons you use the more precisely you locate it — that is falling shot noise. But each photon deposits momentum, and a brighter, cleaner beam deposits a noisier stream of momentum kicks, disturbing the mirror's future position — that is rising radiation-pressure noise. Sharpening the position measurement necessarily blurs the momentum, exactly as Δx Δp≳ℏ/2\Delta x\,\Delta p\gtrsim\hbar/2 demands, and feeding that momentum disturbance forward into the next measurement produces a floor no amount of power can cross. That floor is the SQL, 8ℏ/(mω2L2)8\hbar/(m\omega^2L^2). It bounds a plain position measurement; squeezed light evades it by putting the unavoidable uncertainty into the quadrature you are not reading.

Can a signal be found below the sensitivity curve?

Yes, routinely, for the right kind of signal. The curve is a per-hertz noise density, and the matched filter accumulates signal-to-noise over every cycle a source spends in band. A continuous-wave source like a spinning neutron star sits at nearly one frequency for months; integrating 101010^{10} or more cycles builds SNR far beyond what the instantaneous curve suggests, so such searches probe strains well under the plotted floor. The same logic underlies stochastic-background searches, which cross-correlate two detectors to pull a common signal out of independent noise. What the curve directly limits is a broadband, short-lived transient, which gets only one pass through each frequency. So "below the curve" is a statement about instantaneous density, not about what is ultimately detectable.

Why build kilometre-scale arms instead of folding the light in a small, cheap device?

Because the detector measures strain, not length: its readout scales as ΔL=12hL\Delta L=\tfrac12 hL, so a longer baseline LL produces a larger absolute signal for the same strain, while most displacement noises do not grow as fast with LL. Doubling the arm length roughly doubles the signal against a fixed noise floor. There are limits — beyond a few kilometres the wave's own finite travel time across the arm and the curvature of the Earth start to matter, and cost scales brutally — which is why ground detectors settle near 33–4 km4\,\mathrm{km} and use optical cavities to fold the light many times within that length. Space removes the constraint entirely, letting LISA stretch to millions of kilometres and reach strains at frequencies no terrestrial arm can.

Before this

Where this leads