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ID Date Author Type Category Subject
59   Mon Feb 4 00:39:08 2013 KojiOpticsCharacterizationWedge measurement with the autocollimator and the rotation stage

Method:

• Mount the tombstone prism on the prism mount. The mount is fixed on the rotation stage.
• Locate the prism in front of the autocollimator.
• Find the retroreflected reticle in the view. Adjust the focus if necessary.
• Confirm that the rotation of the stage does not change the height of the reticle in the view.
If it does, rotate the AC around its axis to realize it.
This is to match the horizontal reticle to the rotation plane.
• Use the rotation stage and the alignment knobs to find the reticle at the center of the AC. Make sure the reticle corresponds to the front surface.
• Rotate the micrometer of the rotation stage until the retroreflected reticle for the back surface.
• There maybe the vertical shift of the reticle due to the vertical wedging. Record the vertical shi
• Record the micrometer reading. Take a difference from the previous value.

Measurement:

• A1: α = 0.68 deg, β = 0 arcmin (0 div)
• A2: α = 0.80 deg, β = -6 arcmin (3 div down)
• A3: α = 0.635 deg, β = -1.6 arcmin (0.8 div down)
• A4: α = 0.650 deg, β = 0 arcmin (0div)
• A5: α = 0.655 deg, β = +2.4 arcmin (1.2 div up)

Analysis:

• \theta_H = ArcSin[Sin(α) / n]
• \theta_V = ArcSin[Sin(β) / n]/2

• A1: \theta_H = 0.465 deg, \theta_V = 0.000 deg
• A2: \theta_H = 0.547 deg, \theta_V = -0.034 deg
• A3: \theta_H = 0.434 deg, \theta_V = -0.009 deg
• A4: \theta_H = 0.445 deg, \theta_V = 0.000 deg
• A5: \theta_H = 0.448 deg, \theta_V = 0.014 deg

60   Wed Feb 6 02:34:10 2013 KojiOpticsCharacterizationWedge measurement with the autocollimator and the rotation stage

Measurement:

• A6:   α = 0.665 deg, β = +3.0 arcmin (1.5 div up)
• A7:   α = 0.635 deg, β =   0.0 arcmin (0.0 div up)
• A8:   α = 0.623 deg, β = - 0.4 arcmin (-0.2 div up)
• A9:   α = 0.670 deg, β = +2.4 arcmin (1.2 div up)
• A10: α = 0.605 deg, β = +0.4 arcmin (0.2 div up)
• A11: α = 0.640 deg, β = +0.8 arcmin (0.4 div up)
• A12: α = 0.625 deg, β = - 0.6 arcmin (-0.3 div up)
• A13: α = 0.630 deg, β = +2.2 arcmin (1.1 div up)
• A14: α = 0.678 deg, β =   0.0 arcmin (0.0 div up)
• B1:   α = 0.665 deg, β = +0.6 arcmin (0.3 div up)
• B2:   α = 0.615 deg, β = +0.2 arcmin (0.1 div up)
• B3:   α = 0.620 deg, β = +0.9 arcmin (0.45 div up)
• B4:   α = 0.595 deg, β = +2.4 arcmin (1.2 div up)
• B5:   α = 0.635 deg, β = - 1.8 arcmin (-0.9 div up)
• B6:   α = 0.640 deg, β = +1.6 arcmin (0.8 div up)
• B7:   α = 0.655 deg, β = +2.5 arcmin (1.25 div up)
• B8:   α = 0.630 deg, β = +2.8 arcmin (1.4 div up)
• B9:   α = 0.620 deg, β = - 4.0 arcmin (-2.0 div up)
• B10: α = 0.620 deg, β = +1.2 arcmin (0.6 div up)
• B11: α = 0.675 deg, β = +3.5 arcmin (1.75 div up)
• B12: α = 0.640 deg, β = +0.2 arcmin (0.1 div up)

Analysis:

• \theta_H = ArcSin[Sin(α) * n]
• \theta_V = ArcSin[Sin(β) / n]/2

• A6:   \theta_H = 0.490 deg, \theta_V =  0.017 deg
• A7:   \theta_H = 0.534 deg, \theta_V =  0.000 deg
• A8:   \theta_H = 0.551 deg, \theta_V = -0.0023 deg
• A9:   \theta_H = 0.482 deg, \theta_V =  0.014 deg
• A10: \theta_H = 0.577 deg, \theta_V =  0.0023 deg
• A11: \theta_H = 0.526 deg, \theta_V =  0.0046 deg
• A12: \theta_H = 0.548 deg, \theta_V = -0.0034 deg
• A13: \theta_H = 0.541 deg, \theta_V =  0.013 deg
• A14: \theta_H = 0.471 deg, \theta_V =  0.000 deg
• B1:   \theta_H = 0.490 deg, \theta_V =  0.0034 deg
• B2:   \theta_H = 0.563 deg, \theta_V =  0.0011 deg
• B3:   \theta_H = 0.556 deg, \theta_V =  0.0051 deg
• B4:   \theta_H = 0.592 deg, \theta_V =  0.014 deg
• B5:   \theta_H = 0.534 deg, \theta_V = -0.010 deg
• B6:   \theta_H = 0.526 deg, \theta_V =  0.0091 deg
• B7:   \theta_H = 0.504 deg, \theta_V =  0.014 deg
• B8:   \theta_H = 0.541 deg, \theta_V =  0.016 deg
• B9:   \theta_H = 0.556 deg, \theta_V = -0.023 deg
• B10: \theta_H = 0.556 deg, \theta_V =  0.0068 deg
• B11: \theta_H = 0.475 deg, \theta_V =  0.020 deg
• B12: \theta_H = 0.526 deg, \theta_V =  0.0011 deg

 Quote: Measurement: A1: α = 0.68 deg, β = 0 arcmin (0 div) A2: α = 0.80 deg, β = -6 arcmin (3 div down) A3: α = 0.635 deg, β = -1.6 arcmin (0.8 div down) A4: α = 0.650 deg, β = 0 arcmin (0div) A5: α = 0.655 deg, β = +2.4 arcmin (1.2 div up) Analysis: \theta_H = ArcSin[Sin(α)*n] \theta_V = ArcSin[Sin(β) / n]/2   A1: \theta_H = 0.465 deg, \theta_V = 0.000 deg A2: \theta_H = 0.547 deg, \theta_V = -0.034 deg A3: \theta_H = 0.434 deg, \theta_V = -0.009 deg A4: \theta_H = 0.445 deg, \theta_V = 0.000 deg A5: \theta_H = 0.448 deg, \theta_V = 0.014 deg

66   Fri Mar 1 23:52:18 2013 KojiOpticsCharacterizationWedge measurement with the autocollimator and the rotation stage

Measurement:

• E1:   α = 0.672 deg, β = +0.0 arcmin (0 div up)
• E2:   α = 0.631 deg, β = - 0.3 arcmin (-0.15 div down)
• E3:   α = 0.642 deg, β = +0.0 arcmin (0 div up)
• E4:   α = 0.659 deg, β = +1.4 arcmin (0.7 div up)
• E5:   α = 0.695 deg, β = +0.5 arcmin (0.5 div up)
• E6:   α = 0.665 deg, β = - 0.4 arcmin (-0.2 div down)
• E7:   α = 0.652 deg, β = +1.0 arcmin (0.5 div up)
• E8:   α = 0.675 deg, β = +2.0 arcmin (1.0 div up)
• E9:   α = 0.645 deg, β = - 2.4 arcmin (-1.2 div down)
• E10: α = 0.640 deg, β = +2.2 arcmin (1.1 div up)
• E11: α = 0.638 deg, β = +1.6 arcmin (0.8 div up)
• E12: α = 0.660 deg, β = +1.6 arcmin (0.8 div up)
• E13: α = 0.638 deg, β = +0.8 arcmin (0.4 div up)
• E14: α = 0.655 deg, β = +0.4 arcmin (0.2 div up)
• E15: α = 0.640 deg, β = +1.4 arcmin (0.7 div up)
• E16: α = 0.655 deg, β = +0.6 arcmin (0.3 div up)
• E17: α = 0.650 deg, β = +0.8 arcmin (0.4 div up)
• E18: α = 0.640 deg, β = +2.4 arcmin (1.2 div up)

Analysis:

• \theta_H = ArcSin[Sin(α) / n]
• \theta_V = ArcSin[Sin(β) / n]/2

• E1:   \theta_H = 0.460 deg, \theta_V =   0.000 deg
• E2:   \theta_H = 0.432 deg, \theta_V =  -0.0034 deg
• E3:   \theta_H = 0.439 deg, \theta_V =   0.000 deg
• E4:   \theta_H = 0.451 deg, \theta_V =  0.016 deg
• E5:   \theta_H = 0.475 deg, \theta_V =  0.011 deg
• E6:   \theta_H = 0.455 deg, \theta_V =  -0.0046 deg
• E7:   \theta_H = 0.446 deg, \theta_V =  0.011 deg
• E8:   \theta_H = 0.462 deg, \theta_V =  0.023 deg
• E9:   \theta_H = 0.441 deg, \theta_V =  -0.027 deg
• E10:   \theta_H = 0.438 deg, \theta_V = 0.025 deg
• E11:   \theta_H = 0.436 deg, \theta_V = 0.018 deg
• E12:   \theta_H = 0.451 deg, \theta_V = 0.018 deg
• E13:   \theta_H = 0.436 deg, \theta_V = 0.0091 deg
• E14:   \theta_H = 0.448 deg, \theta_V = 0.0046 deg
• E15:   \theta_H = 0.438 deg, \theta_V = 0.016 deg
• E16:   \theta_H = 0.448 deg, \theta_V = 0.0068 deg
• E17:   \theta_H = 0.444 deg, \theta_V = 0.0091 deg
• E18:   \theta_H = 0.438 deg, \theta_V = 0.027 deg
53   Thu Jan 10 18:37:50 2013 KojiOpticsCharacterizationWedging of the PZTs

Yesterday I measured the thickness of the PZTs in order to get an idea how much the PZTs are wedged.

For each PZT, the thickness at six points along the ring was measured with a micrometer gauge.
The orientation of the PZT was recognized by the wire direction and a black marking to indicate the polarity.

A least square fitting of these six points determines the most likely PZT plane.
Note that the measured numbers are assumed to be the thickness at the inner rim of the ring
as the micrometer can only measure the maximum thickness of a region and the inner rim has the largest effect on the wedge angle.
The inner diameter of the ring is 9mm.

The measurements show all PZTs have thickness variation of 3um maximum.
The estimated wedge angles are distributed from 8 to 26 arcsec. The directions of the wedges seem to be random
(i.e. not associated with the wires)

As wedging of 30 arcsec causes at most ~0.3mm spot shift of the cavity (easy to remember),
the wedging of the PZTs is not critical by itself. Also, this number can be reduced by choosing the PZT orientations
based on the estimated wedge directions --- as long as we can believe the measurements.

Next step is to locate the minima of each curved mirror. Do you have any idea how to measure them?

373   Thu Aug 29 11:51:49 2019 shrutiOpticsCharacterizationWedging of the debonded PZTs - Calculation

Using the measurements of PZTs 12,13 taken by Stephen, I estimated the wedging angle and orientation following Section 2.3.1 of T1500060. The results can be found in Attachment1 and is summarised as follows.

For PZT 12, PZT 13 respectively:

Avg. height = 2.0063 mm, 2.0035 mm

Wedge direction (from the same direction as in the doc: positive right) = 120 deg, 120 deg

Wedge angles = 45.8 arcsec, 30.6 arcsec

This was done assuming that the measurements were taken uniformly at intervals of 60deg along the inner rim of the PZT. The diameter (2r) of the inner rim, according to T1500060, is 9mm. The measured heights were fitted with the function

$h = h_0 + \tan(\Omega)\text{ }r(1-\cos(\theta - \alpha))$

as depicted in Attachment2 to find wedging angle $(\Omega)$ and orientation $(\alpha)$.

Quote:

Wedge and thickness measurements of PZTs 12 and 13 took place after debonding and cleaning - results are shown in the first image (handwritten post-it format).

These thickness measurements seem to have come back thinner than previous measurements. It is possible that I have removed some PZT material while mechanically removing glue. It is also possible that there is systematic error between the two sets of measurements. I did not run any calculations of wedge ange or orientation on these data.

Note that cleaning of debonded PZTs involved mechanically separating glue from the planar faces of PZTs. The second image shows the razer blade used to scrape the glue away.

There were thick rings of glue where there had been excess squeezed out of the bond region, and there was also a difficult-to-remove bond layer that was thinner. I observed the presence of the thin layer by its reflectivity. The thick glue came off in patches, while the thin glue came off with a bit of a powdery appearance. It was hard to be certain that all of the thin bond layer came off, but I made many passes on each of the faces of the 2 PZTs that had been in the bonded CM assemblies. I found it was easiest to remove the glue in the bonded

I was anticipating that the expected 75-90 micron bond layer would affect the micrometer thickness measurements if it was still present, but I did not notice any irregularities (and certainly not at the 10 micron level), indicating that the glue was removed successfully (at least to the ~1 micron level).

 Quote: Yesterday I measured the thickness of the PZTs in order to get an idea how much the PZTs are wedged. For each PZT, the thickness at six points along the ring was measured with a micrometer gauge. The orientation of the PZT was recognized by the wire direction and a black marking to indicate the polarity. A least square fitting of these six points determines the most likely PZT plane. Note that the measured numbers are assumed to be the thickness at the inner rim of the ring as the micrometer can only measure the maximum thickness of a region and the inner rim has the largest effect on the wedge angle. The inner diameter of the ring is 9mm.   The measurements show all PZTs have thickness variation of 3um maximum.  The estimated wedge angles are distributed from 8 to 26 arcsec. The directions of the wedges seem to be random (i.e. not associated with the wires)   As wedging of 30 arcsec causes at most ~0.3mm spot shift of the cavity (easy to remember), the wedging of the PZTs is not critical by itself. Also, this number can be reduced by choosing the PZT orientations based on the estimated wedge directions --- as long as we can believe the measurements.   Next step is to locate the minima of each curved mirror. Do you have any idea how to measure them?

371   Thu Aug 22 12:35:53 2019 StephenOpticsCharacterizationWedging of the debonded PZTs 2019 August

Wedge and thickness measurements of PZTs 12 and 13 took place after debonding and cleaning - results are shown in the first image (handwritten post-it format).

These thickness measurements seem to have come back thinner than previous measurements. It is possible that I have removed some PZT material while mechanically removing glue. It is also possible that there is systematic error between the two sets of measurements. I did not run any calculations of wedge ange or orientation on these data.

Note that cleaning of debonded PZTs involved mechanically separating glue from the planar faces of PZTs. The second image shows the razer blade used to scrape the glue away.

There were thick rings of glue where there had been excess squeezed out of the bond region, and there was also a difficult-to-remove bond layer that was thinner. I observed the presence of the thin layer by its reflectivity. The thick glue came off in patches, while the thin glue came off with a bit of a powdery appearance. It was hard to be certain that all of the thin bond layer came off, but I made many passes on each of the faces of the 2 PZTs that had been in the bonded CM assemblies. I found it was easiest to remove the glue in the bonded

I was anticipating that the expected 75-90 micron bond layer would affect the micrometer thickness measurements if it was still present, but I did not notice any irregularities (and certainly not at the 10 micron level), indicating that the glue was removed successfully (at least to the ~1 micron level).

 Quote: Yesterday I measured the thickness of the PZTs in order to get an idea how much the PZTs are wedged. For each PZT, the thickness at six points along the ring was measured with a micrometer gauge. The orientation of the PZT was recognized by the wire direction and a black marking to indicate the polarity. A least square fitting of these six points determines the most likely PZT plane. Note that the measured numbers are assumed to be the thickness at the inner rim of the ring as the micrometer can only measure the maximum thickness of a region and the inner rim has the largest effect on the wedge angle. The inner diameter of the ring is 9mm.   The measurements show all PZTs have thickness variation of 3um maximum.  The estimated wedge angles are distributed from 8 to 26 arcsec. The directions of the wedges seem to be random (i.e. not associated with the wires)   As wedging of 30 arcsec causes at most ~0.3mm spot shift of the cavity (easy to remember), the wedging of the PZTs is not critical by itself. Also, this number can be reduced by choosing the PZT orientations based on the estimated wedge directions --- as long as we can believe the measurements.   Next step is to locate the minima of each curved mirror. Do you have any idea how to measure them?

361   Wed May 15 19:07:53 2019 KojiCleanGeneralWhat is this???

Suddenly something dirty emerged in the lab. What is this? It looks like an insulation foam or similar, but is quite degraded and emits a lot of particulates.

This does not belong to the lab. I don't see piping above this area which shows broken insulation or anything. All the pipes in the room are painted white.

The only possibility is that it comes from the hole between the next lab (CRIME Lab). I found that the A.C. today is much stronger and colder than last week. And there is a positive pressure from CRIME Lab. Maybe the foam was pushed out from the hole due to the differential pressure (or any RF cable action).

418   Thu Jul 21 13:21:27 2022 KojiGeneralConfigurationWindows laptop for WincamD Beam'R2 recovery

The Windows laptop for WincamD/Beam'R2 (DELL Vostro3300) was not functional.
- Windows 7 got stuck in the starting up process (Google "startup repair loop")
- The battery can't charge and the adapter connection is flaky

I decided to newly install Win10.
I made a new bootable Win10 DVD from the ISO downloaded from IMSS. The ISO file was converted to CDR using Disk Utility on Mac.
This deleted the past disk partitions. The installation process has no trouble and Win10 ran successfully. The machine is slow but still acceptable for our purpose.
The devices ran as expected by connecting the heads and selecting the proper device in the software.

Then, the Win10 fell into "Hibernation Loop" and "Shutdown loop" (after disabling hibernation in the safe mode).
This is probably the combination of extremely slow windows update (feature update i.e. beta OS update) and the occasional shutdown due to the flakiness of the AC connection

Win10 was reinstalled and automatic Win update was disabled via windows policy manager or something like that. Still, it tries to download and update some of the updates (what's happening there!?

Here are my strong recommendations on how to use this laptop

• Do not use any network connection. It will enable Windows Update kicks in and destroy the machine.
• Use a USB stick for data transportation if necessary
• The laptop should always be connected to the power supply at a stable location. (The adapter connection is flaky and the battery is dead)
• Buy a replacement battery (maybe a 3rd-party cheap one
• The Win10 DVD should always be inserted into the laptop's drive so that we can reinstall the windows anytime.
463   Tue Nov 29 15:54:47 2022 KojiGeneralConfigurationWindows laptop for WincamD Beam'R2 recovery

Aaron took the set to Cryo lab

28   Tue Oct 16 15:50:09 2012 KojiGeneralGeneralWork completed in August/September [!]
• Work done
• Things ordered
• Office Depot
• [delivered] Office Depot(R) Brand Stretch Wrap Film, 20 x 1000 Roll, Clear / 445013
• [delivered] Eveready(R) Gold AA Alkaline Batteries, Pack Of 24 / 158448
• [delivered] Rubbermaid(R) Roller Sponge Mop / 921841
• [delivered] Rubbermaid(R) Roller Sponge Mop Replacement / 921858
• [delivered] Rubbermaid(R) Sanitizing Caddy, 10 Quarts, Yellow / 674125
• [delivered] Glad(R) Tall Kitchen Trash Bags, 13 Gallon, White, Box Of 28 / 269268
• Global Industrial Equipment
• [delivered] Extended Surface Pleated Cartridge Filter Serva-Cell Mp4 Slmp295 12X24X2 Gl    WBB431699
• Global Industrial Equipment
• [delivered] Nexel Poly-Z-Brite Wire Shelving 30"W x 21"D x 63"H Nexel Poly-Z-Brite™ Wire Shelving Starter Unit WB189209
• [delivered] Stem Casters Set of (4) 5" Polyurethane Wheel, 2 With Brakes 1200 lb. Capacity WB500592
• Rack Solutions
• [delivered] Open Frame Server Racks
1 x 20" Depth Kit (Ideal for Audio/Video or Networking Racks) P/N: 111-1779
1 x 36U, Rack-111 Post Kit P/N: 111-1728
1 x Caster Kit for Open Frame RACK-111 P/N: 111-1731
• [delivered] 36U Side Panel Kit \$199.99 P/N: 102-1775
• Rack shelf
• [delivered] 1 RMS 19 X 15 SINGLE SIDED NON-VENTED SHELF 70121637
• Work bench, Stools
• [not yet] 72"L X 30"W Production Bench - Phenolic Resin Square Edge-Blue Form attached WB237381LBL
• [not yet] 72"W Lower Shelf For Bench - 15"D- Blue Form attached WB606951
• [not yet] ESD-Safe Vinyl Clean Room Stool with Nylon Base with Drag Chain Blue Form attached WBB560852
• P Touch
• [delivered] Brother PT-2030 Desktop Office Labeler Punch-out product 672828
• [delivered] Brother(R) TZe-241 Black-On-White Tape, 0.75 x 26.2 Punch-out product 239384
• [delivered] Brother(R) TZe-231 Black-On-White Tape, 0.5 x 26.2 Punch-out product 239400
• UV light guide
• [delivered] Fiber Optic Single Light Guide 5mm OD X 3mm ID X 1M L Note: This light guide can be used with MKIII UV Cure unit. OLB1081
• Gloves (7.5, 8.0)
• [delivered] GLOVE ACCTCH NR-LTX SZ7.5 PK25 Punch-out product 79999-306
• [delivered] GLOVE ACCTCH NR-LTX SZ8 PK25 Punch-out product 79999-308
• Lab coat (L,XL), Sticky Mat, Shoe Covers (L, XL), Cap, Mask
• [delivered] LAB XP WH EL WR.COLL. NP L30EA Punch-out product 82007-618
• [delivered] LAB XPWH EL WR.COLL. NP XL30EA Punch-out product 82007-620
• [delivered] VWR MAT ADHESIVE 30L 18X36 BLU Punch-out product 21924-110 (This was too small)
• [delivered] VWR SHOECVR NSKID AP 2XL 150PR Punch-out product 414004-651
• [delivered] VWR SHOECVR NSKID AP XL 150PR Punch-out product 414004-650
• [delivered] CAP BOUFFANT 24IN RAYON CS500 Punch-out product 10843-053
• [delivered] MASK VLTC TIES N/STRL PK50 Punch-out product 10869-020
• VWR
• [delivered] FACE SHIELD UVC-803 Supplier: UVP 33007-151

• [Delivered] Laser safety glasses

12   Tue Jul 31 21:29:43 2012 KojiGeneralGeneralWork completed in July [!]

47   Mon Dec 31 01:45:04 2012 KojiGeneralGeneralWork completed in Nov and Dec [!]

Completed work of the previous months: [Jul] [Aug] [Sep] [Oct] [Nov] [Dec]

• Work done
• Things delivered
• The ionized gun used in the clean room at Downs: made by Terra Universal.com (Jeff's room)
http://www.terrauniversal.com/static-control/ionizing-blow-off-guns.php
• Flow path: N2 cylinder - Filter - Gun (Jeff's room)
• Power strips Tripp Lite PS3612 (Ordered Nov. 8, Delivered Nov. 12)
• Kapton tapes (1in x 6, 1/2in x 12 Delivered Nov. 15)
• Sticky Mats (VWR 18888-216 Delivered Nov. 12 and 21992-042)
• Duck tape (PK3) (Delivered Nov. 12)
• Wipers 12"x12" 2ply x 119 pairs x case15 (Delivered Nov. 12)
• Syringes (1mL&2mL) & Needles (20G x dozen)
• Stainless trays with cover (Steve Delivered Nov. 12)
• Gold Plated allen keys (Steve Delivered Nov. 12)
• Forceps (Delivered Nov. 12) / Tweezers / Scissors (Delivered Nov. 12)
• OMC testing optics / opto-mechanics
• SolidWorks raytracing model
• Mode design for HAM6 layout [Zach]

• Black Glass / Black Glass holder / AR ==> Some at the 40m, some from LLO
• Ionized air blow
• N2 or Air cylinder: 4N - UHP or 5N - Research Grade.  (... steal from Downs)
33   Wed Nov 7 20:21:42 2012 KojiGeneralGeneralWork completed in October [!]

Completed work of the previous months: [Jul] [Aug] [Sep] [Oct] [Nov] [Dec]

300   Mon Jul 2 15:27:31 2018 Rich AbbottElectronicsGeneralWork on EOM (3rd IFO unit)

Koji, Rich

We took apart the unit removed from the 3rd IFO (Unit serial number aLIGO #3, XTAL 10252004) to see what makes it tick.  Koji has done a fine job of adding the plots of the impedance data to this log book.  Attached are some details of the physical construction showing the capacitor values used in shunt before the coils.

19   Wed Aug 22 20:16:43 2012 KojiFacilityGeneralWorkbenches have been installed / Clean room stools

Last Friday, new workbenches were installed. Vladimir got a new table and a cleanroom stool.

The other two workbenches were also nicely set.

144   Fri Jun 14 06:35:21 2013 JeffGeneralGeneral[LLO] L1 OMC status

https://alog.ligo-la.caltech.edu/aLOG/index.php?callRep=7410

Weights:

Suspension cage and transportation box: 250.8lb
Suspension cage and transportation box: 150.2lb ==> 100.6lb ==> 45,630 g

Glass Breadboard and transportation fixture: 16382 g
Transportation fixture only: 9432 g ==> 6950 g
Added mass (up to now): 300 g ==> 7250 g

Preamp arrangement

142   Thu Jun 13 12:04:57 2013 KojiGeneralGeneral[LLO] OMC Optical Test - completed

https://alog.ligo-la.caltech.edu/aLOG/index.php?callRep=7373

141   Mon Jun 10 10:04:37 2013 KojiGeneralGeneral[LLO] OMC Test

[Koji Zach]

We worked on the OMC test over the weekend.

- At the beginning, the measured OMC transmission was ~85% even after subtracting the junk light and sidebands from the calculation.

- A pretty visible (by eye) dust were on CM1. Also a small residue of First Contact was found on the same mirror.

- We applied FC only on CM1 to remove these.

- The measued transmission went up to the level of 96%.

- We swept the incident power from 0.3mW to 30mW in order to see the dependence of the transmission against the incident power.

- The variation of the transmission ~10% was observed (attached figure 1, Red). This was compared with the similar dependence measured at Caltech (Magenta)

- So, the reduction of the transmission was observed as in eLIGO, although the measurements at Caltech and LLO are not consistent.

- Can this be attributed to the dependence of the PD efficiency? We measured the incident power on the PDs together with the preamp DC output. (Figure.2)
This gives us how the responsivity changes with the incident power.

- Nevertheless, the dependence remains. We'll make more accurate measurement today.

143   Thu Jun 13 12:12:20 2013 ZachGeneralGeneral[LLO] OMC and OMCS in LVEA

https://alog.ligo-la.caltech.edu/aLOG/index.php?callRep=7395

140   Fri Jun 7 16:04:44 2013 KojiGeneralGeneral[LLO] OMC arrived

[Koji Zach Suresh]

The OMC arrived at LLO without any destruction!

• We found that one shock sensor on the box turned red, the other stayed white.
• We brought the Perican case to the changing room and the wrapping was opened in the optics lab.
• The OMC was discovered without any obvious damage. Successful shipment!
• The inspection with a halogen light indicated some amount of particules on the breadboard.
The both sides of the breadboard were wiped with the cleanroom cloth.
• The First Contact layers on the optics were removed while the ionized nitrogen gas was brew.

146   Tue Jun 18 15:45:38 2013 KojiGeneralGeneral[LLO] OMC installation in HAM6

OMC installed in HAM6!
https://alog.ligo-la.caltech.edu/aLOG/index.php?callRep=7486

74   Wed Mar 20 09:38:02 2013 ZachOpticsCharacterization[LLO] OMC test bench modified

For various reasons, I had to switch NPROs (from the LightWave 126 to the Innolight Prometheus).

I installed the laser, realigned the polarization and modulation optics, and then began launching the beam into the fiber, though I have not coupled any light yet.

A diagram is below. Since I do not yet have the AOM, I have shown that future path with a dotted line. Since we will not need to make AMTFs and have a subcarrier at the same time, I have chosen to overload the function of the PBS using the HWP after the AEOM. We will operate in one of two modes:

1. AMTF mode: The AOM path is used as a beam dump for the amplitude modulation setup. A razor dump should physically be placed somewhere in the AOM path.
2. Subcarrier mode: The AEOM is turned off and the HWP after it is used to adjust the carrier/subcarrier power ratio. I chose a 70T / 30R beamsplitter for the recombining, since we want to be able to provide ~100 mW with the carrier for transmission testing, and we don't need a particularly strong subcarrier beam for probing.

One thing that concerns me slightly: the Prometheus is a dual-output (1064nm/532nm) laser, with separate ports for each. I have blocked and locked out the green path physically, but there is some residual green light visible in the IR output. Since we are planning to do the OMC transmission testing with a Si-based Thorlabs power meter---which is more sensitive to green than IR---I am somewhat worried about the ensuing systematics. I *think* we can minimize the effect by detuning the doubling crystal temperature, but this remains to be verified.

EDIT (ZK): Valera says there should be a dichroic beam splitter in the lab that I can borrow. This should be enough to selectively suppress the green.

153   Fri Aug 16 17:21:38 2013 KojiGeneralGeneral[OMC002] Build started

[Jeff Koji]

The laser side template was installed and the cavity mirrors were placed.

The laser beam will be resonated in the cavity next week.

291   Thu Feb 22 20:21:02 2018 KojiOpticsCharacterizationaLIGO EOM test

POSTED to 40m ELOG

292   Mon Apr 2 17:27:04 2018 KojiOpticsCharacterizationaLIGO EOM test

2nd optical test http://nodus.ligo.caltech.edu:8080/40m/13725

456   Tue Nov 15 07:46:58 2022 Camille MakaremOpticsGeneralcleaning OMC #1

Monday, November 14, 2022

Camille and Koji did a "deep cleaning" of OMC#1:
1) Applied First Contact to the mirror surfaces. Removed first contact after ~10 minutes.
2) Acetone scrub of the mirror surfaces with a cotton swab.
3) Applied First Contact again. Removed after ~10 minutes. We left the FC paint on for the work on Thu.

The foggy spot on the input mirror was unchanged after the first round of First Contact. But the foggy spot came off during the acetone scrub.

67   Tue Mar 5 19:37:00 2013 ZachOpticsCharacterizationeLIGO OMC visibility vs. power measurement details

EDIT (ZK): Koji points out that (1 - Ti) should really be the non-resonant reflectivity of the aligned cavity, which is much closer to 1. However, it should *actually* be the non-resonant reflectivity of the entire OMC assembly, including the steering mirror (see bottom of post). The steering mirror has T ~ 0.3%, so the true results are somewhere between my numbers and those with (1 - Ti) -> 1. In practice, though, these effects are swamped by the other errors.

As a blanket statement, this measurement was done by exact analogy to those made by Sam and Sheon during S6 (c.f. LHO iLog 11/7/2011 and technical note T1100562), since it was supposed to be a verification that this effect still remains. There are absolutely better ways to do (i.e., ways that should give lower measurement error), and these should be investigated for our characterization. Obviously, I volunteer.

All measurements were made by reading the output voltages produced by photodetectors at the REFL and TRANS ports. The REFL PD is a BBPD (DC output), and the TRANS is a PDA255. Both these PDs were calibrated using a Thorlabs power meter (Controller: PM100D; Head: S12XC series photodiode-based---not sure if X = 0,2... Si or Ge) at the lowest and highest power settings, and these results agreed to the few-percent level. This can be a major source of error.

The power was adjusted using the HWP/PBS combination towards the beginning of the experiment. For reference, an early layout of the test setup can be seen in LLO:5978 (though, as mentioned above, the REFL and TRANS PDs have been replaced since then---see LLO:5994). This may or may not be a "clean" way to change the power, but the analysis should take the effect of junk light into account.

Below is an explanation of the three traces in the plot. First:

• TRANS: TRANS signal calibrated to W
• REFL_UL: REFL signal while cavity is unlocked, calibrated to W
• REFL_L: REFL signal while cavity is locked, calibrated to W
• Psb: Sideband power (relative to carrier)
• Ti: Input mirror transmission (in power)

Now, the traces

1. Raw transmission: This measurement is simple. It is just the raw throughput of the cavity, corrected for the power in the sidebands which should not get through. I had the "AM_REF" PD, which could serve as an input power monitor, but I thought it was better to just use REFL_UL as the input power monitor and not introduce the error of another PD. This means I must also correct for the reduction in the apparent input power as measured at the REFL PD due to the finite transmission of the input coupler. This was not reported by Sam and Sheon, but can be directly inferred from their data.
• trans_raw = TRANS ./ ( REFL_UL * (1 - Psb) * (1 - Ti) )
• Equivalently, trans_raw = (transmitted power) ./ (input power in carrier mode)
2. Coupling: This is how much of the power incident on the cavity gets coupled into the cavity (whether it ends up in transmission or at a loss port). Sheon plots something like (1 - coupling) in his reply to the above-linked iLog post on 11/8/2011.
• coupling = ( REFL_UL * (1 - Ti) - REFL_L ) ./ ( REFL_UL * (1 - Psb) * (1 - Ti) )
• Equivalently, coupling = [ (total input power) - (total reflected power on resonance) ] ./ (input power in carrier mode)
3. Visibility: How much of the light that is coupled into the cavity is emerging from the transmitted port? This is what Sam and Sheon call "throughput" or "transmission" and is what is reported in the majority of their plots.
• visibility = TRANS ./ ( REFL_UL * (1 - Ti) - REFL_L )
• Equivalently, visibility = (transmitted power) ./ [ (total input power) - (total reflected power on resonance) ]
• Also equivalently, visibility = trans_raw ./ coupling

The error bars in the measurement were dominated, roughly equally, by 1) systematic error from calibration of the PDs with the power meter, and 2) error from noise in the REFL_L measurement (since the absolute AC noise level in TRANS and REFL_L is the same, and TRANS >> REFL_L, the SNR of the latter is worse).

(1) can be helped by making ALL measurements with a single device. I recommend using something precise and portable like the power meter to make measurements at all the necessary ports. For REFL_L/UL, we can place a beam splitter before the REFL PD, and---after calibrating for the T of this splitter very well using the same power meter---both states can be measured at this port.

(2) can probably be helped by taking longer averaging, though at some point we run into the stability of the power setting itself. Something like 30-60s should be enough to remove the effects of the REFL_L noise, which is concentrated in the few-Hz region in the LLO setup.

One more thing I forgot was the finite transmission of the steering mirror at the OMC input (the transmission of this mirror goes to the QPDs). This will add a fixed error of 0.3%, and I will take it into account in the future.

68   Wed Mar 6 23:24:58 2013 ZachOpticsCharacterizationeLIGO OMC visibility vs. power measurement details

I found that, in fact, I had lowered the modulation depth since when I measured it to be 0.45 rads --> Psb = 0.1.

Here is the sweep measurement:

This is Psb = 0.06 --> gamma = 0.35 rads.

This changes the "raw transmission" and "coupling", but not the inferred visibility:

I also measured the cavity AMTF at three powers today: 0.5 mW, 10 mW, and 45 mW input.

They look about the same. If anything, the cavity pole seems slightly lower with the higher power, which is counterintuitive. The expected shift is very small (~10%), since the decay rate is still totally dominated by the mirror transmissions even for the supposed high-loss state (Sam and Sheon estimated the roundtrip loss at high power to be ~1400 ppm, while the combined coupling mirrors' T is 1.6%). I have not been able to fit the cavity poles consistently to within this kind of error.

107   Wed Apr 10 00:40:30 2013 ZachOpticsConfigurationfauxMC locked

[Koji, Zach]

Tonight, we locked the "fauxMC". We obtained a visibility of >99%.

Koji had aligned it roughly last night, but we wanted to have a couple steering mirrors in the path for this practice cavity (the periscope mirrors will serve this function in the real setup), so we marked the alignment with irises and installed two extra mirrors.

After obtaining flashes with the WinCam placed at the output coupler, we removed the WinCam and put a CCD camera at one of the curved mirror transmissions and used this to get a strong TEM00 flash. Then, we installed the REFL PD/CCD, swept the laser PZT and optimized the alignment by minimizing the REFL dips. Finally, we connected the RF electronics and locked the cavity with the LB box. We used whatever cables we had around to trim the RF phase, and then Koji made some nice SMA cables at the 40m.

One thing we noticed was that we don't have enough actuation range to keep the cavity locked for very long---even with the HV amp (100V). We are going to offload to the NPRO temperature using an SR560 or pomona box circuit. We may also make an enclosure for the cavity to protect it from the HEPA blasting.

Tomorrow, after we do the above things, we will practice measuring the transmission, length (FSR) and mode spectrum of the cavity before moving on to the real McCoy.

362   Thu May 16 12:41:28 2019 ChubGeneralGeneralfire pillow found on optics table

That is an expanding fire pillow, also known as firebrick.  It is used to create a fire block where holes in fire-rated walls are made and prevents lab fires from spreading rapidly to adjacent labs.  I had to pull cable from B254 to our labs on either side during a rather narrow window of time.  Some of the cable holes are partially blocked, making it difficult to reach the cable to them. The cable is then just guided to the hole from a distance.  With no help, it's not possible to see this material getting shoved out of the hole.  I can assure you that I took great pains not to allow the CYMAC coax to fall into any equipment, or drag against any other cables.

454   Mon Nov 14 08:34:45 2022 CamilleOpticsCharacterizationtransmission measurements through OMC #1 (before cleaning)

[Camille, Koji]

Friday, Nov 11th, 2022

Setting up OMC #1 for transmission measurements:

The laser beam was aligned to the OMC cavity. The OMC cavity was locked and the transmission measurements were recorded.

455   Mon Nov 14 09:27:13 2022 KojiOpticsCharacterizationtransmission measurements through OMC #1 (before cleaning)

The measured total optical loss of the OMC was

1st:   0.015 +/- 0.003
2nd: 0.085  +/- 0.005
3rd:  0.0585+/- 0.0008
4th:  0.047  +/- 0.002

In avegrage the estimated loss is
Loss = 0.055 +/- 0.014

This is unchanged from the measurement at LLO after the FC cleaning
Loss = 0.053 +/- 0.010

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