Numerical and experimental study of the mode tuning technique effects. Application to the cavity ring-down spectroscopy. J. Remy, G.M.W. Kroesen, W.W.

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Numerical and experimental study of the mode tuning technique effects. Application to the cavity ring-down spectroscopy. J. Remy, G.M.W. Kroesen, W.W. Stoffels Eindhoven University of Technology, Applied Physics Department, P.O. Box 513, 5600 MB EINDHOVEN, The Netherlands - EU The Helium cooled CW infrared laser diode:  Mode tuning range: 0.5 to 2 cm -1 (6 to 15 GHz)  Mode spacing: 1 to 3 cm -1 (3 to 9 GHz)  Power: 0.1 mW; Wavelength: 2 – 6  m  Mode linewidth: cm -1 (9 MHz)  N 2 cooled InSb photodiode detector (1 mm 2 active area) The CRDS cavity:  Effective absorption path length: 350 m  Cavity beam waist: 1.72 mm  Spot size on the cavity mirrors: 2.4 mm  FSR :150 MHz; Fundamental mode FWHM: 100 kHz  Plano-concave ZnSe mirrors (R>99.7 %, radius of curvature 1 m). Note that entrance mirror is coupled to a piezoelectric transducer. Project Objective  Study dust formation in Ar- SiH 4 plasmas with CRDS  Define the collective behaviour of a dust cloud  We have developed a new simple ring-down technique that does not require the laser to be turned on and off at the right moment. That new method, called “mode tuning”, uses the ring-down cavity mode structure as well as the optical properties of the laser diode itself in order to control the ring-down effect. We numerically analyzed the Fabry-Pérot (FP) cavity behavior in terms of changes in scanning rates, mirror reflectivity and laser detuning. CRDS schematic The detuning concept  Resonance when laser modes match cavity modes  Out of resonance zone when changed  changes when laser current changes (tens of MHz or mA)  Pulse generator with a high repetition rate (hundreds of MHz) Ø reaction time in the ns Simulated Fabry-Pérot fundamental mode structure, with r=0.9985, L=1 m and =5  m. The x axis measures the cavity length deviation from its standard 1 meter value, the y axis measures the relative transmitted intensity (I out _max=1). The laser line width is unknown to us and is not represented at scale here. FP cavity behavior vs mirror reflectivity =5  m, L=1 m, v=0.8 mm.s -1 Photons keep being injected into the cavity. For high reflectivity, some secondary oscillations appear in one of the feet of the Airy peaks. The ring-up time decreases when the mirrors are more reflective. Airy peak secondary oscillations study Ø m oscillations minima, =5  m, Ø L=1 m, v=0.8 mm.s -1 (*) From An et al. Optics Letters/ Vol.20, No.9 FP cavity behavior vs piezoelectric translator speed =5  m, L=1 m, r= Photons keep being injected into the cavity. For the high speeds (v > 0.5 mm/s), the ring-up time is faster and oscillations can be noticed in one of the feet of the Airy peak. =5  m, L=1 m, r= The oscillations become more visible as the transducer speed gets higher from curves (a) to (f). I 1 and I 2 are the first two maxima of each Airy peak and Dt the time delay between them. FP cavity behavior vs piezoelectric translator speed when laser switched off =5  m, L=1 m, r= The laser is switched off 1.5  s after the light intensity in the cavity reaches its maximum. The logarithmic scale on the vertical axis shows that the cavity ring-down times are strictly identical. Cavity finesse (F) (*) From Poirson et al. J.Opt.Soc.Am.B/ Vol.14, No11 FP cavity behavior vs laser detuning R=0.9985, L=1 m, v=0.16 mm.s -1 Experimental ring-down when laser is detuned Transmitted signal through CRDS cavity (a) without and (b) with detuning of the laser. Detuning the laser or switching it off generate identical numerical results Laser is shifted to half the cavity FSR