Casimir effect and the MIR experiment D. Zanello INFN Roma 1 G. Carugno INFN Padova Summary • The quantum vacuum and its microscopic consequences • The static Casimir effect: theory and experiments • Friction effects of the vacuum and the dynamical Casimir effect • The MIR experiment proposal The quantum vacuum • Quantum vacuum is not empty but is defined as the minimun of the energy of any field • Its effects are several at microscopic level: – Lamb shift – Landè factor (g-2) – Mean life of an isolated atom The static Casimir effect • This is a macroscopic effect of the quantum vacuum, connected to vacuum geometrical confinement • HBG Casimir 1948: the force between two conducting parallel plates of area S spaced by d FC h c S 1.3 10 S 480 d 4 27 d 4 N Experimental verifications • The first significant experiments were carried on in a sphere-plane configuration. The relevant formula is FC 2 hcR R is the sphere radius 3 720d Investigators R Range (mm) Precision (%) Van Blokland and Overbeek (1978) 1m 0.13-0.67 25 at small distances 50 average Lamoreaux (1997) 12.5 cm 0.6-6 5 at very small distance, larger elsewhere Mohideen et al (1998) 200 mm 0.1-0.8 1 Chan et al (2001) 100 mm 0.075-2.2 1 Results of the Padova experiment (2002) K C (1.22 0.18) 1027 N m2 2 Residual square frequency shift (Hz KC F 4 S d ) First measurement of the Casimir effect between parallel metallic surfaces 0 -1000 -2000 -3000 0.5 1 1.5 2 d ( mm) 2.5 3 Friction effects of the vacuum • Fulling and Davies (1976): effects of the vacuum on a moving mirror – Steady motion (Lorentz invariance) – Uniformly accelerated motion (Free falling lift) – Non uniform acceleration (Friction!): too weak to be detectable Nph ~ W T (v/c)2 Amplification using an RF cavity • GT Moore (1970): proposes the use of an RF EM cavity for photon production • Dodonov et al (1989), Law (1994), Jaeckel et al (1992): pointed out the importance of parametric resonance condition in order to multiply the effect wm = 2 w0 wm = excitation frequency w0 = cavity resonance frequency Parametric resonance • The parametric resonance is a known concept both in mathematics and physics • In mathematics it comes from the Mathieu equations • In physics it is known in mechanics (variable length swing) and in electronics (oscillating circuit with variable capacitor) Theoretical predictions 1. Linear growth A.Lambrecht, M.-T. Jaekel, and S. Reynaud, Phys. Rev. Lett. 77, 615 (1996) 2. 2 Wt v N Q 2 c Exponential growth V. Dodonov, et al Phys. Lett. A 317, 378 (2003); M. Crocce, et al Phys. Rev. A 70, (2004); M. Uhlmann et al Phys. Rev. Lett. 93, 19 (2004) v N sinh Wt c 2 t is the excitation time Is energy conserved? E Eout Ein E Eout Ein Eout t t Srivastava (2005): dn an bn 2 dt Resonant RF Cavity In a realistic set-up a 3-dim cavity has an oscillating wall. Wm Cavity with dimensions ~ 1 -100 cm have resonance frequency varying from 30 GHz to 300 MHz. (microwave cavity) Great experimental challenge: motion of a surface at frequencies extremely large to match cavity resonance and with large velocity (b=v/c) Surface motion • Mechanical motion. Strong limitation for a moving layer: INERTIA Very inefficient technique: to move the electrons giving the reflectivity one has to move also the nuclei with large waste of energy Maximum displacement obtained up to date of the order of 1 nm • Effective motion. Realize a time variable mirror with driven reflectivity (Yablonovitch (1989) and Lozovik (1995) Resonant cavity with time variable mirror MIR Experiment Time variable mirror The Project MIR – RD 2004-2005 Dino Zanello Rome Caterina Braggio Gianni Carugno Padova R & D financed by National Institute for Nuclear Physics (INFN) Giuseppe Messineo Federico Della Valle Trieste MIR 2006 APPROVED AS Experiment. Giacomo Bressi Antonio Agnesi Federico Pirzio Alessandra Tomaselli Giancarlo Reali Pavia Giuseppe Galeazzi Giuseppe Ruoso Legnaro Labs Our approach Taking inspiration from proposals by Lozovik (1995) and Yablonovitch (1989) we produce the boundary change by light illumination of a semiconductor slab placed on a cavity wall Semiconductors under illumination can change their dielectric properties and become from completely transparent to completely reflective for selected wavelentgh. Time variable mirror A train of laser pulses will produce a frequency controlled variable mirror and thus if the change of the boundary conditions fulfill the parametric resonance condition this will result in the Dynamical Casimir effect with the combined presence of high frequency, large Q and large velocity Expected results Complete characterization of the experimental apparatus has been done by V. Dodonov et al (see talk in QFEXT07). V V Dodonov and A V Dodonov “QED effects in a cavity with time-dependent thin semiconductor slab excited by laser pulses” J Phys B 39 (2006) 1-18 Calculation based on realistic experimental conditions, • t semiconductor recombination time , t 10-30 ps • m semiconductor mobility , m 1 m 2 / (V s) •() semiconductor light absorption coefficient • t semiconductor thickness , t 1 mm •laser: 1 ps pulse duration, 200 ps periodicity, 10-4 J/pulse •(a, b, L) cavity dimensions N ph 0.85exp(2 F n) 3 Expected photons N > 103 per train of shots Photon generation plus damping N ph 0.85exp(23 F n) A0 = 10 D = 2 mm m = b = 3 104 cm2/Vs = 2.5 GHz = 12 cm (b = 7 cm, L = 11.6) t (ps) Z 23F ( )10-4 N (n=105pulses) N (n=104pulses) 25 0.4 12 9750 7800 28 0.45 8 14600 11800 32 0.5 3 44000 35000 Measurement set-up The complete set-up is divided into Laser system Resonant cavity with semiconductor Receiver chain Data acquisition and general timing Cryostat wall Experimental issues Effective mirror • the semiconductor when illuminated behaves as a metal (in the microwave band) • timing of the generation and recombination processes • quality factor of the cavity with inserted semiconductor • possible noise coming from generation/recombination of carriers Laser system Detection system • possibility of high frequency switching • minimum detectable signal • pulse energy for complete reflectivity • noise from blackbody radiation • number of consecutive pulses Semiconductor as a reflector Reflection curves for Si and Cu Light pulse Experimental set-up Results: • Perfect reflectivity for microwave • Light energy to make a good mirror Time (ms) Si, GaAs: R=1; ≈ 1 mJ/cm2 Semiconductor I The search for the right semiconductor was very long and stressful, but we managed to find the right material Requests: t ~ 10 ps , m ~ 1 m2/ (V s) Neutron Irradiated GaAs Irradiation is done with fast neutrons (MeV) with a dose ~ 1015 neutrons/cm2 (performed by a group at ENEA - ROMA). These process while keeping a high mobility decreases the recombination time in the semiconductor High sensitivity measurements of the recombination time performed on our samples with the THz pump and probe technique by the group of Prof. Krotkus in Vilnius (Lithuania) Semiconductor II: recombination time Results obtained from the Vilnius group on Neutron Irradiated GaAs Different doses and at different temperatures The technique allows to measure the reflectivity from which one calculate the recombination time 2. Same dose (7.5E14 N/cm2) 1. Same temperature T = 85 K 1.2 10-10 1.2 10-10 1 10-10 1 10-10 11 K 85 K Reflecitivity (a.u.) Reflectivity (a.u.) Dose = 1E15 N/cm^2 Dose = 2E15 N/cm^2 Dose = 7.5E14 N/cm^2 8 10-11 6 10-11 4 10-11 8 10-11 6 10-11 4 10-11 2 10-11 2 10-11 0 0 20 40 60 time (ps) 80 100 120 140 0 -20 0 20 40 60 Time (ps) Estimated t = 18 ps 80 100 Semiconductor III: mobility Mobility can be roughly estimated for comparison with a known sample from the previous measurements and from values of non irradiated samples. m ~ 1 m2 / (V s) We are setting up an apparatus for measuring the product mt using the Hall effect. From literature one finds that little change is expected between irradiated and non irradiated samples at our dose Cavity with semiconductor wall Fundamental mode TE101: the electric field E Computer model of a cavity with a semiconductor wafer on a wall a = 7.2 cm b = 2.2 cm l = 11.2 cm 2 2 c 1 1 fr 2.4899 GHz 2 a l QL= tmeasured ≈ 3 · 106 600 mm thick slab of GaAs Superconducting cavity Cavity geometry and size optimized after Dodonov’s calculations Niobium: 8 x 9 x 1 cm3 Antenna hole Cryostats old new Semiconductor holding top Q value ~ 107 for the TE101 mode resonant @ 2.5 GHz No changes in Q due to the presence of the semiconductor The new one has a 50 l LHe vessel Working temperature 1 - 8 K Electronics I Final goal is to measure about 103 photons @ 2.5 GHz Use a very low noise cryogenic amplifier and then a superheterodyne detection chain at room temperature Picture of the room temperature chain The cryogenic amplifier CA has 37 dB gain allowing to neglect noise coming from the rest of the detector chain Special care has to be taken in the cooling of the amplifier CA and of the cable connecting the cavity antenna to it CA PA (Cryogenic) Electronics II: measurements Motorized control of the pick-up antenna Superconducting cavity Cryogenic amplifier ~ 10 cm Electronics III: noise measurement Using a heated 50 W resistor it is possible to obtain noise temperature of the first amplifier and the total gain of the receiver chain 2. Complete chain 1. Amplifier + PostAmplifier LO 5 0 ohm 5 0 ohm FFT CA FFT CA PA 8 10-12 4 10-6 6 10-12 3 10-6 Measured power (W) Measured power (W) heat er Tn = - T0 = 7.2 ± 0.1 K 4 10-12 From slope Total Gain G = 72 dB 2 10-12 0 -10 PA heat er 0 10 20 30 Temperature of the 50 ohm resistance (K) 40 Tn = -T0 = 7.1 ± 0.2 K 2 10-6 From slope total gain G = 128 dB 1 10-6 0 -10 0 10 20 30 Temperature of the 50 ohm resistance (K) 40 Sensitivity The power P measured by the FFT is: P kBGB(TN TR ) Results: TN1 = TN2 kB - Boltmann’s constant G - total gain B - bandwidth TN - amplifier noise temperature TR - 50 W real temperature No extra noise added in the room temperature chain G1 = 72 dB = 1.6 107 Gtot = 128 dB = 6.3 1012 The noise temperature TN = 7.2 K corresponds to 1 10-22 J For a photon energy = 1.7 10-24 J sensitivity ~ 100 photons Black Body Photons in Cavity at Resonance Noise 50 Ohm Resistor at R.T. Noise Signal from TE101 Cavity at R.T. Cavity Noise vs Temperature Laser system I Pulsed laser with rep rate ~ 5 GHz, pulse energy ~100 mJ, train of 103 - 104 pulses, slightly frequency tunable ~ 800 nm Laser master oscillator Pulse picker Optical amplifier 5 GHz, low power Total number of pulses limited by the energy available in the optical amplifier Each train repeated every few seconds Optics Express 13, 5302 (2005) Laser system II Diode preamplifier Master oscillator Pulse picker Current working frequency: 4.73 GHz Pulse picker: ~ 2500 pulses, adjustable Diode preamplifier gain: 60 dB Final amplifier gain: > 20 dB Total energy of the final bunch: > 100 mJ Flash lamp final amplifier Detection scheme N pulses Steps 1. Find cavity frequency r 2. Wait for empty cavity 3. Set laser system to 2 r 4. Send burst with > 1000 pulses 5. Look for signal with t ~ Q / 2r t p = 1 / 2 r Expected number of photons: Niobium cavity with TE101 r = 2.5 GHz (22 x 71 x 110 mm3) Semiconductor GaAs with thickness dx = 1 mm Single run with ~ 5000 pulses N ≥ 103 photons Charg ed cavit y. Will decay wit h it s t ime co nst ant Check list Several things can be employed to disentangle a real signal from a spurious one Change temperature of cavity Effect on black body photons Loading of cavity with real photons (is our system a microwave amplifier?) Change laser pulse rep. frequency 1.6 1.4 12 10 8 6 4 Determine vacuum effect from several measurements with pre-loaded cavity 2 0 1.2 Signal (a.u.) Power inside cavity at end of laser pulses (a.u.) 14 0 1 2 3 4 Power inside cavity at t = t0 (a.u.) 5 6 1 0.8 0.6 0.85 0.9 0.95 Laser pulse frequency (a.u) 1 1.05 1.1 -change recombination time of semiconductor -change width of semiconductor layer Conclusions We expect to complete assembly Spring this year. First measure is to test the amplification process with preloaded cavity, then vacuum measurements Loading of cavity with real photons and measure Gain Several things can be employed to disentangle a real signal from a spurious one Carry on measurements at different temperatures and extrapolate to T = 0 Kelvin Change laser pulse rep. frequency 1.6 1.4 12 10 1.2 Signal (a.u.) Power inside cavity at end of laser pulses (a.u.) 14 8 6 4 1 0.8 Determine vacuum effect from several measurements with pre-loaded cavity 0.6 0.85 2 0.9 0.95 Laser pulse frequency (a.u) 1 1.05 1.1 0 0 1 2 3 4 Power inside cavity at t = t0 (a.u.) 5 6 - change recombination time of semiconductor - change thickness of semiconductor Frequency shift Problem: derivation of a formula for the shift of resonance in the MIR em cavity and compare it with numerical calculations and experimental data. -L complex dielectric function 0 G transparent background D Result: a thin film is an ideal mirror (freq shift) even if G ds L D d A2 GD ds2 s , mirror if A 1 MIR experiment: 800 nm light impinging on GaAs + 1 mm abs. Length = plasma thickness + mobility 104 cm2/Vs mWcm A>1 n = WT/2 Nph = sinh2(n) = sinh2(T0) ideal case •unphysically large number of photons dissipation effects (instability removed) •T 0 non zero temperature experiment? Nph = sinh2(n)(1+2 <N1>0) Nb = kT / h thermal photons are amplified as well Surface effective motion II Met al plat e Generate periodic motion by placing the reflecting surface in two distinct positions alternatively Position 1 Position 2 Variab le mirror Micro wave - metallic plate - microwave mirror with driven reflectivity USE P1 P2 Semiconductors under illumination can change their dielectric properties and become from completely transparent to completely reflective for microwaves. Light with photon energy h > E band gap of semiconductor Enhances electron density in the conduction band Laser ON - OFF On semiconductor Time variable mirror