Physics · Book 4 · Bachelor Year 2

University Physics — Year 2

University Physics — Year 2 · Bachelor Year 2

20The Michelson Interferometer

In 1887 Michelson and Morley split a beam of light in two, sent the halves along perpendicular arms, recombined them, and watched the fringes for the shift that the Earth’s motion through the ether should produce: nothing moved, and physics changed. In 2015 the same instrument — two arms, now four kilometres long and folded to a thousand — recorded a gravitational wave that changed their lengths by a thousandth of a proton’s diameter. Between those two dates the Michelson interferometer measured the metre in wavelengths, resolved spectral lines, and became the standard tool of precision optics. This chapter describes it in its two configurations — the air wedge and the parallel plate — and shows how its fringes measure lengths, indices and spectra.

20.1 The instrument

Definition 20.1 (The Michelson interferometer)

A beam splitter SpSp — a glass plate with a semi-reflecting face — at 4545{}^{\circ} divides an incident beam into two: one goes to the mirror M1M_1, the other to M2M_2, both perpendicular to their beams; after reflection each returns to SpSp, where half of it is sent toward the observer, where the two halves interfere. A compensating plate CC, identical to the splitter and parallel to it, is put in the arm that would otherwise cross the splitter’s glass only once, so that both beams cross the same thickness of glass: the path difference is then a pure difference of air paths, the same for every wavelength — which white-light fringes require. The mirrors’ distances from SpSp are d1d_1 and d2d_2; one mirror is mounted on a micrometer screw and on tilt screws.

Proposition 20.2 (Equivalent arrangement)

Seen from the observer, the interferometer is equivalent to the mirror M2M_2 and the image M1M_1' of M1M_1 in the splitter: a thin layer of air between two reflecting surfaces, of thickness e=d1d2e = |d_1 - d_2|, whose two reflections interfere (division of amplitude):

  • M1M2M_1' \parallel M_2: an air plate of thickness eerings of equal inclination, localized at infinity, δ=2ecosi\delta = 2e\cos i;
  • M1M_1' slightly tilted by α\alpha relative to M2M_2: an air wedge — straight fringes of equal thickness, localized on the mirrors (near the wedge), δ=2αx\delta = 2\alpha x at normal incidence, spacing λ/2α\lambda/2\alpha.

At contact (e=0e = 0, α=0\alpha = 0) the field is uniform, and for white light it is the one place where the colours agree: the "white fringe".

Proof. Folding the M1M_1 arm onto the M2M_2 arm by reflection in SpSp maps the two beams onto one line with two mirrors ee apart; the two returning waves are those reflected by the two faces of the air layer (no extra λ/2\lambda/2: both reflect on metal, and the splitter treats them symmetrically, up to a constant phase that shifts the whole pattern). The thin-film results of Chapter 19 then apply with n=1n = 1.

Left: the Michelson interferometer — splitter, compensating plate, two mirrors, one beam recombined toward the observer. Right: the equivalent air layer between M_2 and the image M_1' of M_1, parallel (rings) or tilted (straight fringes).
Left: the Michelson interferometer — splitter, compensating plate, two mirrors, one beam recombined toward the observer. Right: the equivalent air layer between M2M_2 and the image M1M_1' of M1M_1, parallel (rings) or tilted (straight fringes).

20.2 The two fringe systems

Proposition 20.3 (Rings of the air plate)

With M1M2M_1' \parallel M_2 and an extended source, the observer (or a lens of focal length ff and a screen in its focal plane) sees concentric rings; the ring at the angle ii has the order p=2ecosi/λp = 2e\cos i/\lambda; bright rings where pp is an integer. The centre has the highest order, p0=2e/λp_0 = 2e/\lambda; near it, cosi1i2/2\cos i \approx 1 - i^2/2, so the kk-th bright ring from the centre (counted from the first one, at ε=p0p0\varepsilon = p_0 - \lfloor p_0\rfloor below the centre’s order) has the radius

rk=fik=f(k1+ε)λe:r_k = f\,i_k = f\sqrt{\frac{(k - 1 + \varepsilon)\lambda}e} :

rings tighter with larger ee (more, thinner rings), spreading as e0e \to 0 until, at contact, one uniform field. Moving a mirror by λ/2\lambda/2 changes p0p_0 by one: a ring is born at (or swallowed by) the centre for every half wavelength of displacement.

Proof. δ=2ecosi\delta = 2e\cos i for the parallel plate (Chapter 19, n=1n = 1, no extra λ/2\lambda/2 for two metallic reflections); 2e(1i2/2)=(p0k+1ε)λ2e(1 - i^2/2) = (p_0 - k + 1 - \varepsilon)\lambda with 2e=p0λ2e = p_0\lambda gives ei2=(k1+ε)λei^2 = (k - 1 + \varepsilon)\lambda.

Proposition 20.4 (Fringes of the air wedge)

With M1M_1' tilted by a small angle α\alpha and near-normal incidence, the path difference at the point of the mirrors at distance xx from the line of contact is δ=2αx\delta = 2\alpha x: straight fringes parallel to that line, spaced λ/2α\lambda/2\alpha, localized on the mirrors (they are viewed by focusing on M2M_2, or projected on a screen with a lens conjugating M2M_2 and the screen). The zero-order fringe lies on the contact line, the same for every wavelength: with white light it is white (or black, according to the splitter’s phases), flanked by a few coloured fringes — the signature by which the contact is found.

Proof. Equal-thickness fringes of a wedge of air, e(x)=αxe(x) = \alpha x. Localization: for an extended source the rays through a given point of the wedge recombine there, with the same δ\delta at near-normal incidence.

The two fringe systems of the Michelson, and the contrast of the sodium doublet’s fringes against the plate thickness: it vanishes every 0.29\, mm (first at 0.145\, mm), when the two lines’ fringes are in opposition.
The two fringe systems of the Michelson, and the contrast of the sodium doublet’s fringes against the plate thickness: it vanishes every 0.29mm0.29\,\mathrm{mm} (first at 0.145mm0.145\,\mathrm{mm}), when the two lines’ fringes are in opposition.

20.3 Measuring with the Michelson

Proposition 20.5 (Lengths, indices, spectra)

Counting NN fringes passing the centre while a mirror moves by Δe\Delta e gives Δe=Nλ/2\Delta e = N\lambda/2: lengths in wavelengths (a micrometre screw calibrated to 0.1µm0.1\,\text{µ}\mathrm{m}; the metre itself was so measured). A transparent plate of thickness \ell and index nn inserted in one arm adds 2(n1)2(n - 1)\ell to δ\delta and shifts the pattern by 2(n1)/λ2(n - 1)\ell/\lambda fringes: indices (and their variations with pressure or temperature, in a gas cell). With a doublet of wavelengths λ\lambda and λ+Δλ\lambda + \Delta\lambda, the two fringe systems fall out of step and back in step as ee grows, the contrast vanishing every

Δe=λ22Δλ:\Delta e = \frac{\lambda^2}{2\Delta\lambda} :

the splitting of close lines. More generally the contrast as a function of ee maps out the spectrum of the source (the contrast decays over ec/2e \sim \ell_c/2): recording the intensity at the centre while ee scans is Fourier transform spectroscopy, the method of infrared spectrometers.

Proof. The order at the centre is 2e/λ2e/\lambda; each line has its own. The two systems coincide again when 2e/λ2e/(λ+Δλ)=12e/\lambda - 2e/(\lambda + \Delta\lambda) = 1, i.e. 2eΔλ/λ2=12e\Delta\lambda /\lambda^2 = 1; they are in opposition half-way. The general statement is the contrast formula of Exercise 18.10.

Example 20.6 (Sodium, and the metre)

The sodium doublet (Δλ=0.6nm\Delta\lambda = 0.6\,\mathrm{nm} at 589nm589\,\mathrm{nm}): the rings blur and sharpen every Δe=5892/(2×0.6)\Delta e = 589^2/(2 \times 0.6) nm =0.29mm= 0.29\,\mathrm{mm} — a classic measurement of Δλ\Delta\lambda to a few percent with a screw. Michelson (1892) counted the fringes of the red cadmium line over the length of the standard metre: 1553163.51\,553\,163.5 wavelengths, the first tie between the metre and an atom; today the metre is defined through cc and the second, and interferometers check gauge blocks in production to nanometres.

The intensity at the centre of the rings as the plate thickness grows, for a source of finite coherence length: the fringes fade over e _c/2; the envelope is the Fourier transform of the spectrum.
The intensity at the centre of the rings as the plate thickness grows, for a source of finite coherence length: the fringes fade over ec/2e \sim \ell_c/2; the envelope is the Fourier transform of the spectrum.

Remark 20.7 (The arms that measured nothing, and those that measured a wave)

Michelson and Morley expected the Earth’s velocity vv through the ether to change the round-trip time along the arm parallel to it by (L/c)(v/c)2(L/c)(v/c)^2 relative to the perpendicular arm, a fringe shift of 2L(v/c)2/λ0.42L(v/c)^2/\lambda \approx 0.4 fringe for L=11mL = 11\,\mathrm{m} and v=30km/sv = 30\,\mathrm{km}/\mathrm{s}; rotating the apparatus should have swung the pattern by that much. They could see 0.010.01 fringe; they saw nothing. The gravitational-wave detectors of today are Michelsons with 4km4\,\mathrm{km} arms, light bouncing some three hundred times in each, and a laser stable enough to read a change of arm length ΔL/L1021\Delta L/L \sim 10^{-21}101810^{-18} m, a thousandth of a proton — against the noise of seismic motion and of the photons themselves.

Method 20.8 (Using a Michelson)

(1) Identify the configuration: parallel plate (rings at infinity; observe with a lens or the eye at infinity) or wedge (fringes on the mirrors; focus on M2M_2). (2) Write δ=2ecosi\delta = 2e\cos i or 2αx2\alpha x and the order. (3) Translate each measurement into fringes: Δe=Nλ/2\Delta e = N\lambda/2, 2(n1)2(n - 1)\ell for a plate, λ2/2Δλ\lambda^2/2\Delta\lambda for a doublet. (4) Use the contact position (e=0e = 0, white fringe) as the absolute reference; note that the rings’ radii shrink as ee grows. (5) Coherence limits: rings are visible while 2e<c2e < \ell_c; the wedge needs near-normal incidence.

20.4 Exercises

Exercise 20.1

A Michelson in sodium light (λ=589nm\lambda = 589\,\mathrm{nm}): the mirror is moved by 0.10mm0.10\,\mathrm{mm}: number of rings passing the centre; displacement corresponding to 250250 fringes; precision on ee if a tenth of a fringe can be read.

Solution

Solution of Exercise 20.1.

N=2Δe/λ=340N = 2\Delta e/\lambda = 340; 250250 fringes: Δe=125λ=74µm\Delta e = 125\lambda = 74\,\text{µ}\mathrm{m}; a tenth of a fringe is λ/20=30nm\lambda/20 = 30\,\mathrm{nm}.

Exercise 20.2

Parallel plate of thickness e=0.50mme = 0.50\,\mathrm{mm}, lens f=1.0mf = 1.0\,\mathrm{m}, λ=589nm\lambda = 589\,\mathrm{nm}: order at the centre; is the centre bright? Radii of the first three bright rings; what happens to the rings as ee is reduced to 0.05mm0.05\,\mathrm{mm}?

Solution

Solution of Exercise 20.2.

p0=2e/λ=1697.8p_0 = 2e/\lambda = 1697.8: not an integer, the centre is not bright (ε=0.8\varepsilon = 0.8). rk=f(k1+ε)λ/er_k = f\sqrt{(k - 1 + \varepsilon)\lambda/e}: 3.13.1, 4.64.6, 5.7cm5.7\,\mathrm{cm}. At 0.05mm0.05\,\mathrm{mm} the radii grow by 10\sqrt{10}: few, broad rings.

Exercise 20.3

Air wedge with α=1.0×104rad\alpha = 1.0 \times 10^{-4}\,\mathrm{rad}, λ=633nm\lambda = 633\,\mathrm{nm}: fringe spacing; number of fringes across 2cm2\,\mathrm{cm} of mirror; the wedge angle is doubled: what happens? How is the contact found with white light?

Solution

Solution of Exercise 20.3.

λ/2α=3.2mm\lambda/2\alpha = 3.2\,\mathrm{mm}; six fringes across 2cm2\,\mathrm{cm}; doubling α\alpha halves the spacing. Contact: translate the mirror until the white-light fringes (a white one flanked by coloured ones) appear — they exist only within a micrometre of δ=0\delta = 0.

Exercise 20.4

A glass plate 0.10mm0.10\,\mathrm{mm} thick is inserted in one arm: fringe shift for n=1.52n = 1.52 at 589nm589\,\mathrm{nm}; the shift is measured to 0.20.2 fringe: precision on nn. Why could the same measurement not be made with white light if the plate were 1cm1\,\mathrm{cm} thick?

Solution

Solution of Exercise 20.4.

2(n1)e/λ=1772(n - 1)e/\lambda = 177 fringes; 0.20.2 fringe gives Δn=0.2λ/2e=6×104\Delta n = 0.2\lambda/2e = 6 \times 10^{-4}\,. A centimetre of glass adds millimetres of dispersive path: the colours no longer agree anywhere, no white fringe.

Exercise 20.5 ★★

Sodium doublet. (a) Thickness ee between two successive disappearances of the rings, for Δλ=0.597nm\Delta\lambda = 0.597\,\mathrm{nm}. (b) A student measures 1717 disappearances over 5.00mm5.00\,\mathrm{mm}: Δλ\Delta\lambda and its precision. (c) Orders of the two lines at e=0.29mme = 0.29\,\mathrm{mm}: check they differ by 12\tfrac12. (d) Why is the contrast never exactly zero (the two lines have intensities in the ratio 2:12 : 1): minimum contrast.

Solution

Solution of Exercise 20.5.

(a) λ2/2Δλ=0.291mm\lambda^2/2\Delta\lambda = 0.291\,\mathrm{mm}. (b) 5.00/17=0.294mm5.00/17 = 0.294\,\mathrm{mm}: Δλ=λ2/2Δe=0.590nm\Delta\lambda = \lambda^2/2\Delta e = 0.590\,\mathrm{nm}; 0.1%0.1\%: ±0.0006nm\pm0.0006\,\mathrm{nm}. (c) At e=0.145mme = 0.145\,\mathrm{mm} (the first disappearance): p1=492.4p_1 = 492.4, p2=491.9p_2 = 491.9 — half an order apart; at 0.29mm0.29\,\mathrm{mm} they differ by one. (d) The weaker fringes survive: Vmin=(I1I2)/(I1+I2)=1/3V_{\min} = (I_1 - I_2)/(I_1 + I_2) = 1/3.

Exercise 20.6 ★★

Index of air. A 10.0cm10.0\,\mathrm{cm} cell in one arm is evacuated, then slowly filled with air at 1bar1\,\mathrm{bar}; 9494 fringes pass (λ=589nm\lambda = 589\,\mathrm{nm}). (a) n1n - 1 for air. (b) Fringes passing for a 1%1\,\% change of pressure; temperature coefficient if n1ρn - 1 \propto \rho. (c) Why does this matter for the stability of any interferometer in air? (d) Precision on n1n - 1 from a tenth of a fringe.

Solution

Solution of Exercise 20.6.

(a) 2(n1)=94λ2(n - 1)\ell = 94\lambda: n1=2.77×104n - 1 = 2.77 \times 10^{-4}\,. (b) 0.940.94 fringe per percent;  ⁣d(n1)/ ⁣dT=(n1)/T=9.5×107K1\dd(n - 1)/\dd T = -(n - 1)/T = -9.5 \times 10^{-7}\,\mathrm{K}^{-1}. (c) A few millibars or a degree in one arm move the fringes: hence vacuum or equal arms. (d) 0.1/940.1/94: ±3×107\pm3 \times 10^{-7}\,.

Exercise 20.7 ★★

Coherence length. With a low-pressure mercury lamp (green line, 546nm546\,\mathrm{nm}, width 0.01nm0.01\,\mathrm{nm}) the rings fade as ee grows. (a) Coherence length; thickness ee at which the contrast becomes negligible. (b) Same with a high-pressure lamp (Δλ=1nm\Delta\lambda = 1\,\mathrm{nm}). (c) With a He–Ne laser (Δν=1MHz\Delta\nu = 1\,\mathrm{MHz}): can one still see rings with e=10me = 10\,\mathrm{m}? (d) What limits white-light fringes to ±2\pm2 orders around contact?

Solution

Solution of Exercise 20.7.

(a) c=λ2/Δλ=3cm\ell_c = \lambda^2/\Delta\lambda = 3\,\mathrm{cm}: rings fade beyond e1.5cme \approx 1.5\,\mathrm{cm}. (b) 0.3mm0.3\,\mathrm{mm}, e0.15mme \approx 0.15\,\mathrm{mm}. (c) c=300m\ell_c = 300\,\mathrm{m}: yes. (d) c1µm\ell_c \approx 1\,\text{µ}\mathrm{m}: 2e<1µm2e < 1\,\text{µ}\mathrm{m}, a couple of orders.

Exercise 20.8 ★★

Compensating plate. Without CC, one beam crosses the splitter’s glass (eg=5mme_g = 5\,\mathrm{mm}, n=1.52n = 1.52) three times and the other once. (a) Extra optical path; can it be compensated by moving a mirror for monochromatic light? (b) Why not for white light (dispersion: nn varies by 0.010.01 across the visible)? (c) What tolerance on the parallelism of CC and SpSp keeps the white fringe (take a residual difference of thickness <0.3µm< 0.3\,\text{µ}\mathrm{m})? (d) Modern splitters are thin pellicles or cubes: why is CC unnecessary then?

Solution

Solution of Exercise 20.8.

(a) 2(n1)eg=5.2mm2(n - 1)e_g = 5.2\,\mathrm{mm}; yes, by 2.6mm2.6\,\mathrm{mm} of mirror travel. (b) The glass path varies with λ\lambda by 2egΔn=100µmc2e_g\Delta n = 100\,\text{µ}\mathrm{m} \gg \ell_c: no wavelength-independent zero. (c) 2(n1)Δeg<0.3µm2(n - 1)\Delta e_g < 0.3\,\text{µ}\mathrm{m}: Δeg<0.3µm\Delta e_g < 0.3\,\text{µ}\mathrm{m} — a relative tilt below 1.5×105rad1.5 \times 10^{-5}\,\mathrm{rad} over 2cm2\,\mathrm{cm}. (d) A pellicle is micrometres thick; a cube is symmetric: both beams see the same glass.

Exercise 20.9 ★★

Michelson–Morley. Arms of L=11mL = 11\,\mathrm{m} (folded), λ=550nm\lambda = 550\,\mathrm{nm}, Earth’s orbital speed v=30km/sv = 30\,\mathrm{km}/\mathrm{s}. (a) In the ether theory the round trip along the arm parallel to v\vect v takes 2L/c(1v2/c2)2L/c(1 - v^2/c^2) and the perpendicular one 2L/c1v2/c22L/c\sqrt{1 - v^2/c^2}: difference, to lowest order. (b) Fringe shift expected on rotating the apparatus by 9090{}^{\circ} (the roles of the arms swap). (c) They could detect 0.010.01 fringe: upper bound on vv. (d) What does a null result say, and what did Einstein conclude?

Solution

Solution of Exercise 20.9.

(a) ΔtLv2/c3=4.1×1015s\Delta t \approx Lv^2/c^3 = 4.1 \times 10^{-15}\,\mathrm{s}, a path of 1.2µm1.2\,\text{µ}\mathrm{m}. (b) Swapping the arms doubles it: 2Lv2/c2λ=0.42Lv^2/c^2\lambda = 0.4 fringe. (c) v<300.01/0.4=4.7km/sv < 30\sqrt{0.01/0.4} = 4.7\,\mathrm{km}/\mathrm{s}. (d) No motion through an ether is seen; the speed of light is the same along both arms — the postulate of relativity.

Exercise 20.10 ★★★

Fourier spectroscopy. The intensity at the centre of the rings is I(e)=S(ν)[1+cos(4πνe/c)] ⁣dνI(e) = \int S(\nu)[1 + \cos(4\pi\nu e/c)]\dd\nu for a source of spectrum S(ν)S(\nu). (a) For a single line: I(e)I(e); period in ee. (b) For a Gaussian line of width Δν\Delta\nu: show the fringes have a Gaussian envelope of width c/2Δν\sim c/2\Delta\nu in ee (admit the Fourier transform of a Gaussian is a Gaussian). (c) Resolution: two lines Δν\Delta\nu apart are separated if the scan reaches emaxc/2Δνe_{\max} \approx c/2\Delta\nu; for emax=10cme_{\max} = 10\,\mathrm{cm}, the resolving power λ/Δλ\lambda/\Delta\lambda at 1µm1\,\text{µ}\mathrm{m}. (d) Why is this method preferred in the infrared (signal, "multiplex" advantage)?

Solution

Solution of Exercise 20.10.

(a) I=S0[1+cos(4πν0e/c)]I = S_0[1 + \cos(4\pi\nu_0e/c)], period λ/2\lambda/2 in ee. (b) Each frequency gives a fringe of slightly different period; a Gaussian band of width Δν\Delta\nu sums to fringes with a Gaussian envelope of width c/2Δν\sim c/2\Delta\nu. (c) R=ν/Δν=2emax/λ=2×105R = \nu/\Delta\nu = 2e_{\max}/\lambda = 2 \times 10^5. (d) All wavelengths fall on one detector at once (Fellgett) through a wide aperture (Jacquinot): far more signal than a slit spectrometer in the photon-starved infrared.

Exercise 20.11 ★★★

Gravitational-wave detector. Arms L=4kmL = 4\,\mathrm{km}, light recycled to N=300N = 300 round trips, λ=1064nm\lambda = 1064\,\mathrm{nm}, the wave changes the arms by ΔL/L=1021\Delta L/L = 10^{-21} in opposite directions. (a) Change of path difference; phase shift. (b) The instrument is held on a dark fringe and measures the small intensity I=I0sin2(Δφ/2)I = I_0\sin^2(\Delta\varphi/2): intensity change for the signal. (c) With 100W100\,\mathrm{W} of circulating light at 1064nm1064\,\mathrm{nm}, photons per second; the photon noise in 1ms1\,\mathrm{ms} (N\sqrt N) against the signal: is it detectable? What does more power buy? (d) Why are the arms kilometres long, and why the mirrors suspended?

Solution

Solution of Exercise 20.11.

(a) Each arm’s path changes by 2NΔL2N\Delta L, in opposite senses: Δδ=4NΔL=4.8×1015m\Delta\delta = 4N\Delta L = 4.8 \times 10^{-15}\,\mathrm{m}, Δφ=2πΔδ/λ=2.8×108rad\Delta\varphi = 2\pi\Delta\delta/\lambda = 2.8 \times 10^{-8}\,\mathrm{rad}. (b) Near a dark fringe the detector sees an intensity proportional to Δφ2\Delta\varphi^2 — or, with a small offset, to Δφ\Delta\varphi: a relative change of order 10810^{-8}. (c) 5×10205 \times 10^{20} photons per second, 5×10175 \times 10^{17} per millisecond, relative noise 1.4×1091.4 \times 10^{-9}: the signal is twenty times the noise; more power lowers the noise as 1/P1/\sqrt P. (d) ΔLL\Delta L \propto L; the pendulum suspensions filter the ground’s motion above their resonance.

Exercise 20.12 ★★★

Localization. (a) Show that for the wedge the two rays leaving a point PP of M2M_2 for an observer at infinity (incidence ii) have the path difference 2e(P)cosi2e(P)\cos i plus a term αi\propto\alpha i that cancels for i=0i = 0: the fringes are on the mirrors at normal incidence only. (b) An extended source illuminates the wedge with incidences up to imaxi_{\max}: what must imaxi_{\max} satisfy for the fringes to stay sharp (2eimax2/2<λ/42e\,i_{\max}^2/2 < \lambda/4 at the edge of the field, e=20µme = 20\,\text{µ}\mathrm{m})? (c) For the parallel plate the rings do not move when the eye moves: why? (d) A student sees fringes that drift when she moves her head: which configuration is she in, and what should she adjust?

Solution

Solution of Exercise 20.12.

(a) For a point PP at depth e(P)e(P) and incidence ii, δ=2e(P)cosi\delta = 2e(P)\cos i plus a term αi\propto\alpha i from the tilted second reflection, which vanishes at normal incidence: only there do both rays from PP reach the eye — localization on the mirrors. (b) ei2<λ/4ei^2 < \lambda/4: imax<λ/4e=0.09radi_{\max} < \sqrt{\lambda/4e} = 0.09\,\mathrm{rad}. (c) The rings depend on ii alone: any eye position sees the same angular pattern. (d) The wedge viewed off the mirrors; focus on M2M_2 or reduce the tilt.

A Michelson interferometer on a teaching bench: laser, splitter cube, two mirrors, and on the screen the rings of equal inclination of the air plate.
A Michelson interferometer on a teaching bench: laser, splitter cube, two mirrors, and on the screen the rings of equal inclination of the air plate.
The LIGO interferometer at Hanford: a Michelson interferometer with arms four kilometres long, which in 2015 recorded a change of arm length of a thousandth of a proton’s diameter — the passage of a gravitational wave (LIGO Laboratory).
The LIGO interferometer at Hanford: a Michelson interferometer with arms four kilometres long, which in 2015 recorded a change of arm length of a thousandth of a proton’s diameter — the passage of a gravitational wave (LIGO Laboratory).

20.5 Problem: The sodium doublet and the index of air

Problem 20.1

Weekend problem — a complete measurement session on a Michelson interferometer: finding contact, reading lengths, splitting the yellow line, weighing the air

The interferometer has a micrometer screw reading 1µm1\,\text{µ}\mathrm{m}; the sodium lamp gives λ1=589.0nm\lambda_1 = 589.0\,\mathrm{nm} and λ2=589.6nm\lambda_2 = 589.6\,\mathrm{nm} with intensities 2:12 : 1; a white lamp and a He–Ne laser (632.8nm632.8\,\mathrm{nm}) are also available.

Part I — Setting up.

  1. With the laser, the student sees two spots of the two arms on a card; she superposes them with the tilt screws and then sees straight fringes: which configuration is this, and what does their spacing tell about the residual tilt (spacing 2mm2\,\mathrm{mm})?
  2. Turning the tilt screws, the fringes curve and then become rings: why do rings appear, and where is M1M_1' now?
  3. She translates the mirror and counts 158158 rings swallowed by the centre: displacement; in which direction is ee changing?
  4. As she goes on, the rings spread and the central spot grows to fill the field: what has she reached? The sodium lamp replaces the laser and she sees nothing special: why not, and why does white light show a bright central fringe flanked by coloured ones at that point?
  5. She tilts M1M_1 very slightly at contact and sees, in white light, straight coloured fringes: explain, and say how many she can expect on each side of the white one.
  6. The laser spots are 10mm10\,\mathrm{mm} across and she wants ten rings in the field of a lens of f=20cmf = 20\,\mathrm{cm} (λ=632.8nm\lambda = 632.8\,\mathrm{nm}): thickness ee needed (use the radius of the kk-th ring).
  7. Why must the compensating plate be parallel to the splitter, and what would she see in white light if it were removed?

Part II — The doublet.

  1. Starting from contact with the sodium lamp, she increases ee: the rings’ contrast falls, vanishes, returns. Thickness of the first disappearance; of the nn-th.
  2. She records 1212 disappearances between e=0.15mme = 0.15\,\mathrm{mm} and e=3.35mme = 3.35\,\mathrm{mm} (the first and the last read on the screw): Δλ\Delta\lambda; precision if each reading is good to 5µm5\,\text{µ}\mathrm{m}.
  3. Orders p1p_1 and p2p_2 of the two lines at the first disappearance; at the first return of full contrast.
  4. Minimum contrast at a disappearance, given the 2:12 : 1 intensity ratio (the weaker line’s fringes remain).
  5. How many disappearances can she count before the natural width of the lines (0.02nm0.02\,\mathrm{nm} each) washes everything out?
  6. What would a lamp with three lines of equal spacing show?

Part III — The air. A cell of length =5.00cm\ell = 5.00\,\mathrm{cm} with glass windows is placed in one arm and pumped down; air is let in slowly while the laser fringes are counted.

  1. Optical path difference created by filling the cell to 1atm1\,\mathrm{atm} if n1=2.9×104n - 1 = 2.9 \times 10^{-4}\,; number of fringes.
  2. She counts 4646 fringes: her value of n1n - 1.
  3. She lets in only 0.20bar0.20\,\mathrm{bar}: fringes expected (n1n - 1 \propto pressure).
  4. The room warms by 3K3\,\mathrm{K} during the measurement, and the 40cm40\,\mathrm{cm} of open air path in each arm change index by 1×106-1 \times 10^{-6}\, per kelvin: fringe drift; is it a problem for Part II, for Part III?
  5. Why do the cell’s windows not shift the measurement (they are there during the whole count)?
  6. The experiment is repeated with CO2_2 (n1=4.5×104n - 1 = 4.5 \times 10^{-4}\,): fringes for a full cell; how could the gas be identified from the count alone?

Part IV — Limits.

  1. The screw is read to 1µm1\,\text{µ}\mathrm{m}: precision of a length measured by fringe counting over 1cm1\,\mathrm{cm}, versus by the screw alone.
  2. A vibration of 50nm50\,\mathrm{nm} amplitude at 100Hz100\,\mathrm{Hz} shakes one mirror: fringe motion; what does the eye see, what does a camera at 2525 frames per second see?
  3. The laser’s frequency drifts by 1×1081 \times 10^{-8}\, in relative value during a count over e=1cme = 1\,\mathrm{cm}: error in fringes.
  4. A 10mm10\,\mathrm{mm} gauge block is certified to λ/20\lambda/20 by interferometry: absolute and relative precision.
  5. Why is the Michelson the instrument of choice for lengths, and the grating (next chapter) for spectra?
  6. Sum up the four quantities measured (a length, a doublet splitting, an index, a coherence length) and the fringe observation that gave each.
Solution

Solution of Problem 20.1.

1. Wedge fringes; λ/2α=2mm\lambda/2\alpha = 2\,\mathrm{mm}: α=1.6×104rad\alpha = 1.6 \times 10^{-4}\,\mathrm{rad}.

2. M1M_1' has become parallel to M2M_2: the air plate, whose fringes of equal inclination are rings.

3. 158λ/2=50µm158\lambda/2 = 50\,\text{µ}\mathrm{m}; rings swallowed at the centre: ee decreasing.

4. Contact, e=0e = 0. Sodium light has no feature there (one wavelength, uniform field either way); white light shows the one position where every colour has δ=0\delta = 0, flanked by colours as the orders separate.

5. δ=2αx\delta = 2\alpha x: a white fringe on the contact line and one or two coloured ones on each side (2αx<c1µm2\alpha x < \ell_c \approx 1\,\text{µ}\mathrm{m}).

6. r10=f10λ/e=5mmr_{10} = f\sqrt{10\lambda/e} = 5\,\mathrm{mm}: e=10λf2/r2=1.0cme = 10\lambda f^2/r^2 = 1.0\,\mathrm{cm}.

7. Parallel, the two beams cross equal glass at every wavelength; without CC, the dispersion of 5mm5\,\mathrm{mm} of glass leaves no common zero: no white fringe.

8. λ2/4Δλ=0.145mm\lambda^2/4\Delta\lambda = 0.145\,\mathrm{mm}; then every λ2/2Δλ=0.291mm\lambda^2/2\Delta\lambda = 0.291\,\mathrm{mm}.

9. 1111 intervals over 3.20mm3.20\,\mathrm{mm}: 0.291mm0.291\,\mathrm{mm}, Δλ=0.597nm\Delta\lambda = 0.597\,\mathrm{nm}; ±10µm\pm10\,\text{µ}\mathrm{m} on 3.2mm3.2\,\mathrm{mm}: ±0.002nm\pm0.002\,\mathrm{nm}.

10. 492.4492.4 and 491.9491.9 (half an order apart); at the return, 984.7984.7 and 983.7983.7.

11. 1/31/3.

12. c=λ2/Δλ=1.7cm\ell_c = \lambda^2/\Delta\lambda = 1.7\,\mathrm{cm}: 2e<1.7cm2e < 1.7\,\mathrm{cm}, about 2929.

13. Three fringe systems: full contrast every λ2/2Δλ\lambda^2/2\Delta\lambda, with two partial dips between — the pattern of three slits.

14. 2(n1)=29µm2(n - 1)\ell = 29\,\text{µ}\mathrm{m}: 4646 fringes.

15. n1=46λ/2=2.91×104n - 1 = 46\lambda/2\ell = 2.91 \times 10^{-4}\,.

16. 9.29.2 fringes.

17. Equal arms: the drift is common to both and cancels; a 1cm1\,\mathrm{cm} inequality gives 2×0.01×3×106=0.1fringe2 \times 0.01 \times 3 \times 10^{-6} = 0.1\,\mathrm{fringe} — harmless for both parts.

18. They are present, unchanged, throughout the count: a constant offset.

19. 7171 fringes; the count gives n1n - 1, a signature of the gas.

20. 3160031\,600 fringes over a centimetre, read to a tenth: 30nm30\,\mathrm{nm}, 3×1063 \times 10^{-6}; the screw gives a micrometre.

21. δ\delta swings by ±100nm\pm100\,\mathrm{nm}, ±0.16\pm0.16 fringe at 100Hz100\,\mathrm{Hz}: the eye sees lowered contrast; at 2525 frames per second the camera samples four periods per frame and sees a frozen or slowly beating pattern.

22. 108×31600=3×10410^{-8} \times 31\,600 = 3 \times 10^{-4} fringe: nothing.

23. λ/20=32nm\lambda/20 = 32\,\mathrm{nm} on 10mm10\,\mathrm{mm}: 3×1063 \times 10^{-6}.

24. It compares a length directly with a wavelength, fringe by fringe; the grating spreads all wavelengths at once over a wide range.

25. Length: rings counted at the centre. Doublet: the periodic loss of contrast. Index: fringes passing while the cell fills. Coherence length: the thickness at which the rings fade.

Terms defined in this chapter

See all 393 terms in the glossary