Virgo change request

Similar documents
Virgo status and commissioning results

Installation and Characterization of the Advanced LIGO 200 Watt PSL

Advanced Virgo commissioning challenges. Julia Casanueva on behalf of the Virgo collaboration

DESIGN OF COMPACT PULSED 4 MIRROR LASER WIRE SYSTEM FOR QUICK MEASUREMENT OF ELECTRON BEAM PROFILE

VIRGO. The status of VIRGO. & INFN - Sezione di Roma 1. 1 / 6/ 2004 Fulvio Ricci

The VIRGO injection system

REFLECTION THROUGH LENS

The VIRGO detection system

Adaptive Optics for LIGO

Some Progress In The Development Of An Optical Readout System For The LISA Gravitational Reference Sensor

The Virgo detector. L. Rolland LAPP-Annecy GraSPA summer school L. Rolland GraSPA2013 Annecy le Vieux

Interferometer signal detection system for the VIRGO experiment. VIRGO collaboration

Commissioning of Advanced Virgo

NON-AMPLIFIED PHOTODETECTOR USER S GUIDE

CMS Note Mailing address: CMS CERN, CH-1211 GENEVA 23, Switzerland

ALIGNMENT METHODS APPLIED TO THE LEP MAGNET MEASUREMENTS. J. Billan, G. Brun, K. N. Henrichsen, P. Legrand, 0. Pagano, P. Rohmig and L. Walckiers.

SOLEIL Libera Performance

Polarization Experiments Using Jones Calculus

EE119 Introduction to Optical Engineering Fall 2009 Final Exam. Name:

The 34th International Physics Olympiad

NON-AMPLIFIED HIGH SPEED PHOTODETECTOR USER S GUIDE

Optical lever for KAGRA

Angular control of Advanced Virgo suspended benches

Phys 531 Lecture 9 30 September 2004 Ray Optics II. + 1 s i. = 1 f

Criteria for Optical Systems: Optical Path Difference How do we determine the quality of a lens system? Several criteria used in optical design

This experiment is under development and thus we appreciate any and all comments as we design an interesting and achievable set of goals.

Broadband Photodetector

Development of Optical lever system of the 40 meter interferometer

Mirrors and Lenses. Images can be formed by reflection from mirrors. Images can be formed by refraction through lenses.

Technical Brief #5. Power Monitors

PSD Characteristics. Position Sensing Detectors

Optical Telescope Design Study Results

Arm Cavity Finesse for Advanced LIGO

Measure the roll-off frequency of an acousto-optic modulator

LISA AIV/T. N. Dinu Jaeger ARTEMIS. [joint work with APC and CNES]

Department of Physics & Astronomy Undergraduate Labs. Thin Lenses

High-Power, Passively Q-switched Microlaser - Power Amplifier System

Effects of Incident Optical Power on the Effective Reverse Bias Voltage of Photodiodes This Lab Fact demonstrates how the effective reverse bias

80-MHz Balanced Photoreceivers Model 18X7

Thulium-Doped Fiber Amplifier Development for Power Scaling the 2 Micron Coherent Laser Absorption Instrument for ASCENDS

Variable Gain Photoreceiver - Fast Optical Power Meter

Quantum Efficiency Measurement System with Internal Quantum Efficiency Upgrade

Physics 1442 and 1444 Questions and problems Only

Laser Telemetric System (Metrology)

International Conference on Space Optics ICSO 2000 Toulouse Labège, France 5 7 December 2000

Amplified High Speed Photodetectors

Non-amplified Photodetectors

Amplified Photodetectors

AP Physics Problems -- Waves and Light

Receiver Design for Passive Millimeter Wave (PMMW) Imaging

Nano Beam Position Monitor

Highly Reliable 40-mW 25-GHz 20-ch Thermally Tunable DFB Laser Module, Integrated with Wavelength Monitor

AIM payload OPTEL-D. Multi-purpose laser communication system. Presentation to: AIM Industry Days ESTEC, 22nd February 2016

HIGH SPEED FIBER PHOTODETECTOR USER S GUIDE

FIBER OPTICS. Prof. R.K. Shevgaonkar. Department of Electrical Engineering. Indian Institute of Technology, Bombay. Lecture: 24. Optical Receivers-

Calibration of AO Systems

80-MHz Balanced Photoreceivers Model 18X7

Chapter 23. Light Geometric Optics

880 Quantum Electronics Optional Lab Construct A Pulsed Dye Laser

P202/219 Laboratory IUPUI Physics Department THIN LENSES

Practical Considerations for Radiated Immunities Measurement using ETS-Lindgren EMC Probes

Design parameters Summary

Introduction. Laser Diodes. Chapter 12 Laser Communications

Non-amplified High Speed Photodetectors

A 3 Mpixel ROIC with 10 m Pixel Pitch and 120 Hz Frame Rate Digital Output

General Physics Experiment 5 Optical Instruments: Simple Magnifier, Microscope, and Newtonian Telescope

Two- Stage Control for CubeSat Optical Communications

photodiodes Description PerkinElmer Optoelectronics offers a broad array of Silicon and InGaAs PIN and APDs.

Laboratory 7: Properties of Lenses and Mirrors

ENSC 470/894 Lab 3 Version 6.0 (Nov. 19, 2015)

Physics 309 Lab 2 Faraday Effect

EXPERIMENT 10 Thin Lenses

04. REFRACTION OF LIGHT AT CURVED SURFACES

Deep- Space Optical Communication Link Requirements

Performance of the MCP-PMTs of the TOP counter in the first beam operation of the Belle II experiment

EVLA Memo 105. Phase coherence of the EVLA radio telescope

Practice Problems (Geometrical Optics)

125-MHz Photoreceivers Models 1801 and 1811

TNI mode cleaner/ laser frequency stabilization system

OBIS CellX. The Universal Light Engine FEATURES

Optical generation of frequency stable mm-wave radiation using diode laser pumped Nd:YAG lasers

Tilt sensor and servo control system for gravitational wave detection.

The VIRGO suspensions

Difrotec Product & Services. Ultra high accuracy interferometry & custom optical solutions

Back-Reflected Light and the Reduction of Nonreciprocal Phase Noise in the Fiber Back-Link on LISA

RECOMMENDATION ITU-R S Technical and operational characteristics of satellites operating in the range THz

Assembly and Experimental Characterization of Fiber Collimators for Low Loss Coupling

Optimization of coupling between Adaptive Optics and Single Mode Fibers ---

Noise Performance Application Note

Digital Radiography : Flat Panel

Wavefront Sensing In Other Disciplines. 15 February 2003 Jerry Nelson, UCSC Wavefront Congress

CXI 1 micron Precision Instrument Stand

Final Reg Optics Review SHORT ANSWER. Write the word or phrase that best completes each statement or answers the question.

Orbit Stability Challenges for Storage Rings. Glenn Decker Advanced Photon Source Beam Diagnostics March 8, 2012

AgilEye Manual Version 2.0 February 28, 2007

PHYS 160 Astronomy. When analyzing light s behavior in a mirror or lens, it is helpful to use a technique called ray tracing.

Chapter 3 Mirrors. The most common and familiar optical device

Determination of Focal Length of A Converging Lens and Mirror

Information for Physics 1201 Midterm 2 Wednesday, March 27

AIDA-2020 Advanced European Infrastructures for Detectors at Accelerators. Deliverable Report. CERN pixel beam telescope for the PS

Transcription:

Virgo change request Quadrants photodiodes for BMS and MC end mirror Responsible: Name: Cleva Email Cleva.at.obs-nice.fr Institution: CNRS / OCA Artemis Procedure start date: 21/12/2006 Procedure end date: dd/mm/yyyy Document version v0r01 Version date 21/12/2006 Page: 1/11

Authors Name Institution email Cleva CNRS OCA Artemis cleva@obs-nice.fr Index Authors...2 Index...2 Abstract...3 Motivations...3 Technical description...3 Task 1... Errore. Il segnalibro non è definito. Task 2... Errore. Il segnalibro non è definito. Deliverable 1...7 Involved Virgo sub-systems...8 Involved EGO infrastructures...8 Planning...9 Budget... Errore. Il segnalibro non è definito. Short description... Errore. Il segnalibro non è definito. Detailed description of the requested items... Errore. Il segnalibro non è definito. Document/Procedure history...11 Annexes... Errore. Il segnalibro non è definito. Automatic information fields...11 Page: 2/11

1. Abstract From the origin, the two quadrants photodiodes (PHD) used in the Beam Monitoring System (BMS) and one quadrants photodiode involved in the mode cleaner automatic alignment (located in transmission of the mode cleaner mirror) are "temporary" ones. Indeed one quadrants PHD has been loaned by Nice group and the two others are the ones which will be used for Pre-Mode Cleaner. 2. Motivations Motivations are triple: - Pre mode Cleaner is supposed to be delivered at the end of this year; the loaned quadrant photodiodes will then be required for the "PMC alignment monitor" purpose they were designed for. - The dark noise of the quadrant photodiodes needs to be improved - It will make some spare photodiodes available 3. Technical description on Task 1: BMS and mode cleaner end mirror quadrant photodiodes design 1. Summary Three quadrant photodiodes are required, BMS_QN, BMS_QF (located on the external injection bench) and MC_QT (located behind the mode cleaner end mirror). All of them are of equivalent kind, description is given below. 2. Requirements a. SPOT-15-YAG silicon quadrants photodiode from UDT have been selected, and are already available as light sensitive devices. There is still a doubt on their ability to support more than 1mW; if not, one may consider to select other quadrant diodes. b. Photodiodes are used in the"+" configuration (see Annex 4 figure 1) c. One DC channel delivering the overall power (sum of 4 quadrants), assuming the incident power is about 6mW, and detector efficiency is 0.45A/W (silicium). d. 2 channels giving two combinations of quarter of quadrants, relative to vertical/horizontal displacement of beam on the quadrant: Sv = Q1+Q2-Q3-Q4 (vertical) and Sh = Q1+Q3-Q2-Q4 (horizontal). e. Those channels (Sh and Sv) will be filtered with a pre-shaping filter and connected on rio23 ADC cards. Signals transmitted through those channels will not be spoiled when connected to ADC cards. Pre-shaping filters are also part of the request. Remark: pre-shaping filter proposal: 0dB below 1Hz, gain 20dB above 10Hz; it is compatible with signals levels (see figure 5), since rms signal before is always lower than 0,1Vrms. f. Enclosure is a metallic box compatible with size requirements on external input bench; box height must be adjustable in order to keep detector centered on beam height (100mm axis). Adjustable system could be copied from what already used for PMC photodiode (mechanical schemes from Nice-OCA-ARTEMIS group given to EGO). Page: 3/11

3. Noise specifications for both BMS_QF, BMS_QN (see Annex 1 & 2) (*) a. Dark noise for channels Sh and Sv should be negligible with respect to 216pA/sqrt(Hz) (evaluated at photodiode output); spec. is set by minimum optical signal to be detected. b. DC offsets (evaluated at photodiode output) should be less than 32uA for both Sh and Sv signals c. Overall DC output (sum of 4quadrants) should be below 10V saturation, assuming 2.7mA overall current; hence R_dc_overall = 3kohms. d. Sh and Sv should be below saturation for a beam fully non-centered on the quadrant (with 2.7mA current, we take R_dc = 3.0 kohms) to ease the lock acquisition. e. Assuming R_dc = 3 kohms gives Sh/v floor of 0.65μV/sqrt(Hz) which is below ADC floor; one needs 20db amplification above 10Hz to not be spoiled by ADC noise. Pre-shaping filter, see 3.2.e.remark. (*) Remark - BMS_QN_ BMS_QF, MC_QT could be designed on the basis of the most stringent specifications, that is specifications for MC_QT. - In case UDT photo-detector accept only 1mW (instead of 6mW), one has to re-adjust preshaping filter amplification and also the spec. in 3.3.a becomes 216/6=36 pa/sqrt(hz). Is it then worth to move to centronix sensors (since QD100-4X accepts 10mA)? 4. Noise specifications for MC_QT (see Annex 3) a. Dark noise for channels Sh and Sv should be negligible with respect to 278pA/sqrt(Hz) (evaluated at photodiode output). b. DC offsets (evaluated at photodiode output) should be kept lower than 19uA c. Overall DC output (sum of 4quadrants) should be below 10V saturation, assuming 2.7mA overall current; hence R_dc_overall = 3kohms. d. Sh and Sv should be below saturation for a beam fully non-centered on the quadrant (with 2.7mA current, we take R_dc = 3.0 kohms) to ease the lock acquisition e. Assuming R_dc = 3 kohms gives Sh/v floor of 0.8uV/sqrt(Hz) which is below ADC floor; one needs 20db amplification above 10Hz to not be spoiled by ADC noise. Pre-shaping filter, see 3.2.e.remark. (*) Remark In case UDT photo-detector accept only 1mW (instead of 6mW), one has to re-adjust preshaping filter amplification and also the spec. in 3.4.a becomes 278/6=46 pa/sqrt(hz). Is it then worth to move to centronix sensors (since QD100-4X accepts 10mA)? 4. Task 2: Integration of quadrants photodiodes. 5. Annexes Annex 1 noise specifications for BMS_QF * Beam jitter level is supposed to reach 1e-5 urad/sqrt(hz) at 5kHz (extrapolation with 1/f slope from 1kHz, see Annex 4 - figure 2). One needs to be able to detect beam jitter noise up to 5kHz. Page: 4/11

Sensitivity for BMS_QF signal is S = 2*sqrt(2/pi)/w*a*(i_dc) with a = 8.θ, where, 8 is equivalent focal length of telescope, in meter θ is the beam jitter in radians, w = 800um is the beam size on the quadrant, i_dc is the overall dc current (about 2.7mA, or 6mW), -> S = 43. A/rad, we need to detect 430pA/sqrt(Hz) (that is 1e-5 urad/sqrt(hz)) * A specification on the residual offset comes from the fact that we cannot rely on their stability over time. We choose the offset to induce equivalent error signal less than 1/100 of the IMC divergence (0.75urad). That is 32uA residual offset. Annex 2 noise specifications for BMS_QN * Beam jitter level is supposed to reach 1e-4 um/sqrt(hz) at 5kHz (extrapolation with 1/f slope from 1kHz, see Annex 4 - figure 3). One needs to be able to detect beam jitter noise up to 5kHz, Sensitivity for BMS_QN signal is S = 2*sqrt(2/pi)/w*a*i_dc with a = 1,51.δ 1,51 accounts for optical magnification of NF telescope, δ is the beam jitter in meters, w = 3000um is the beam size on the quadrant, i_dc is the overall dc current (about 2.7mA, or 6mW), -> S = 2,17 A/m, we need to detect 216pA/sqrt(Hz) (that is 1e-4 um/sqrt(hz)) * A specification on the residual offset comes from the fact that we cannot rely on their stability over time. We choose the offset to induce equivalent error signal less than 1/100 of the IMC waist (50um). That is 108uA residual offset. Annex 3 noise specifications for MC_QT MC_QT quadrant is used to control mode cleaner end mass. a. Vertical error signal Figure 4 shows the error signal Sc_IB_MC_tx (linear combination of Sc_MC_QT_DCv and Bs_IMC_QF_ACv signals). Sc_IB_MC_tx reaches a floor above 1kHz at 40prad/sqrt(Hz); we fix the specification for that signal to be 4prad/sqrt(Hz). Lets call this signal "θx", then [θx*180/7] is the displacement seen on the MC_QT photo-detector (180m is the mode cleaner mirror radius of curvature, 1/7 is the MC_QT quadrant telescope magnification) Assuming the MC_QT sensitivity to be S = 2*sqrt(2/pi)/1.6mm*i_dc = 2.7 A/m (for 2.7mA overall current, or 6mW incident optical power) The specification of 4prad/sqrt(Hz) on θx is then reached for 278pA/sqrt(Hz) at the output of the photo-detector. Page: 5/11

* A specification on the residual offset comes from the fact that we cannot rely on offset stability over time/temperature. We choose then the offset to induce equivalent error signal to be less than 1/100 of the IMC waist (5mm). That is 19uA residual offset. b. Horizontal error signal * Sc_IB_MC_ty reaches a floor above 1kHz at 40prad/sqrt(Hz); we fix the specification for that signal to be 4prad/sqrt(Hz). Lets call this signal "θy", then [θy*180*4.5/7] is the displacement seen on the MC_QT photodetector (180m is the mode cleaner mirror radius of curvature, 4.5 comes from the geometry of IMC, 1/7 is the telescope magnification) Assuming MC_QT sensitivity of 2.7A/m, The specification of 4prad/sqrt(Hz) on θ is then reached for 1250pA/sqrt(Hz) at the output of the photo-detector. * A specification on the residual offset comes from the fact that we cannot rely on offset stability over time/temperature. We choose then the offset to induce equivalent error signal to be less than 1/100 of the IMC divergence (0.75urad). That is 184uA residual offset (i.e. 0.75urad*4.5*142m/7*2.7A/m). Remark: From UDT data sheet, N.E.P = 3e-14W/sqrt(Hz) is compatible with 1pA/sqrt(Hz) level. Annex 4 - figures Figure 1 Q1 Q3 Q2 Q4 Page: 6/11

Figure 2 Figure 3 Figure 4 Page: 7/11

Figure 5 BMS_FFh & v expressed in urad/sqrt(hz) with 9urad/V calibration BMS_NFh & v expressed in um/sqrt(hz) with 540um/V calibration MC_QT_DCh & v expressed in V/sqrt(Hz). Rms value (red curve) are always much lower than 0.1Vrms 6. Deliverable 1-3+1 quadrant photodiodes, assuming one common design for the three photodiodes (one will be a spare) - Associated pre-shaping filters - Associated mechanical mounts and feet. 7. Involved Virgo sub-systems # Subsystem Name Description of the involvement 1 Injection alignment Quadrant photodiode integration Page: 8/11

8. Involved EGO infrastructures # Infrastructure Description of the involvement 1 Electronic Electronic realization, test 2 Mechanical workshop Mount realization Page: 9/11

9. Planning Implementation Plan February 2007 March 2007 April 2007 Tasks and Deliverables W1 W2 W3 W4 W1 W2 W3 W4 W1 W2 W3 W4 Tasks Task #1 Task #2 Deliverables Deliverable #1. Page: 10/11

10. Budget # Item Contractor / Cost ( ) supplier (taxes incl.) 4 Electronic + mechanics <2000? EGO Total cost ( ): Request to EGO ( ) 11. Document/Procedure history Date Event Comment dd/mm/yyyy Start of the procedure dd/mm/yyyy Presentation to the detector meeting dd/mm/yyyy New release of the document dd/mm/yyyy Submission to the VSC Charged to EGO/Virgo lab. 12. Automatic information fields Description Value Last saved by: cleva Last saved time: 21/12/2006 10.23 Automatic versioning 1 Automatic title Quadrants photodiodes for BMS and MC end mirror Filename CRE_PHD_BMS&MC_2.doc Page: 11/11