There is half as much jitter attenuation as we expect from the PMC. Since broad band jitter noise from the HPO has been limiting our sensitivity (in addition to acoustic jitter peaks which are imposed after the PMC), it is worth understanding the jitter attenuation we get from the PMC and fixing it if possible. I originally wrote this alog after looking at data from September 11th, however the bullseye QPD seems to have been misaligned or somehow otherwise changed while people were in the PSL for maintenance period on August 29th. This lead me to the seemingly impossible conclusion that the PMC was letting 33 times more jitter through than it should.
I looked at a period of time when the mode cleaner was misaligned and unlocked on July 18th 2017, starting around 2:05:00.
One possible explanation would be that the coherence is explained by something other than jitter coupling through the PMC, like residual intensity noise or acoustics on the table, but neither of these seem to be the case (second attachment, bottom left). There is no coherence of the WFS PIT with the SUM, which rules out intensity noise, and the table accelerometers have good coherence at the frequencies where the bullseye is not coherent (at resonant frequencies of optical mounts table acoustics explain the jitter, but not at the frequencies where the bullseye coherence is highest).
The third attachment shows that the spectrum of IMC WFS B (uncalibrated, taken with the IMC locked) has gotten noisier towards the end of O2.
It would be good to realign the bullseye or replace it with the new version and check that it is well aligned and that the beam size is correct. After the in chamber work with the IMC bypass is finished, we can repeat this measurement with more power.
It looks like our PMC does not attenuate jitter as much as it should, I think about 33 times less than it should.
The PMC should attenuate pointing jitter by 0.0163 for yaw and 0.0144 for pitch according to T0900616.
The first plot shows spectra and coherences from a time (only about a minutes and a half long) when there was 2 W into the IMC but MC2 was misalinged. The IMC WFS DC are then calibrated in to beam widths. The bullseye QPD is calibrated in to beam widths in the front end, (34625) in this plot I've added a factor for the attenuation we expect from the PMC. The bullseye shows jitter that comes from the HPO with a smooth spectrum, which should be well below the measured noise on the IMC WFS with the attenuation from the PMC. In the lower panel you can see that the Bullseye has rather high coherence with IMC WFS B PIT, suggesting that the jitter is not attenuated as much as it should be by the PMC.
At 200 Hz,it looks like the PMC is only attenuating the jitter by about 0.47. The WFS B PIT has 1.2e-6 1/rt Hz at 200 Hz, and a coherence of 0.5 with the bullseye, so the noise seen by the bullseye is at about the level of 8.5e-7. The bullseye pit is 1.8e-6 /rt Hz at 200 Hz (without the rescaling I've done in the attached plot).
Edit: The coherence of the WFS B Pit with the bullseye cannot be explained by residual intensity noise in the pit signal which is coherent with the jitter noise. I've updated the plot to include a trace that shows no coherence between WFS B sum and WFS B pit.
Second edit: The bullseye QPD was misalinged during the maintence window on August 29th, so this result be misleading.
I ran a couple of PMC scans. Some good data should start at around 15/11/2017 at 2:50:57 UTC. The largest higher order mode is a 20 mode, with about 1/4th the power that is in the 00 mode.
It should be noted that the only maintenance on the PSL on August 29th was done entirely from the control room, no PSL incursion was made. Looking into it further, there are no alogs from that day indicating a PSL incursion was made (or on the preceeding Monday or following Wednesday), and the operator's daily activity log also indicates that no incursion was made. At this point in time we do not know why the bulls-eye PD became misaligned. Peter King is going into the enclosure tomorrow (11/17/2017) for something unrelated and has agreed to take a look at the bulls-eye PD to see if anything is amiss.
WP7220: Daniel, Sheila, Patrick, Dave:
Daniel's latest h1sqz, h1sqzwfs, h1asc and h1ascimc models were loaded by restarted these models.
H1EDCU_HPIPUMPCTRLEX.ini was modified to add four pressure monitor channels which had been rewired from the old purple-box ADC to the replacement Beckhoff ADC (channel names are slightly different allowing old and new to run side-by-side).
We discovered a duplicate channel name in PLC4 and h1sqz (H1:SQZ-SEED_PZT_OFFSET). Sheila made a naming change in the h1sqz model to resolve this. After this model was restarted the DAQ was restarted.
Due to an out-of-date safe.snap file for h1ascimc, the alignment did not recover correctly. Keita manually recovered some settings and I performed a full burt restore to 14:10 PST.
Actually the safe.snap was not too out-of-date (it was snapped 7th November) but the rapid change to this system meant settings had changed since that time. In cases such as this here are two snapshots which can be used to restore settings: the hourly autoburt, and the snap file generated when the model is shutdown. The latter is located in the target burt directory. Note it may contain errors because the 'new' autoBurt.req file is used to snapshot the 'old' system.
TITLE: 11/16 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:
LOG:
16:45 Hugh to HAM3
17:00 Ed to CER
17:00 Chandra and two guest to MY
17:30 Terry to SQZ
17:45 Greg to LVEA to work on TCS viewports
18:15 Gerardo & TJ to optics lab to move OFI
18:15 Robert to LVEA to look at TCS viewports
18:30 Bubba to EY
18:45 Travis Betsy to biergarten, out 20:00
19:45 Kyle MX
21:30 Betsy, Travis, Arnab, Rakesh to HAM6
22:00 Keita, Ed transition LVEA to laser hazard
22:30 Dave restarts some models, including ASC, driving PSL PZT nutso, which apparently hoses alignment crew
23:30 Betsy, Keita, Travis, Ed, Jason out
many models showed a DAQ-CRC error ramp-up around 11:35PST. Trend and overview attached. I will investigate further if it re-occurs.
S Cooper, J Warner, S Dwyer,
As part of the work we've been doing to try and understand how large earthquakes affect the interferometer, I've written MATLAB script that searches for the lock state of the interferometer as well as searching for watchdog trips in HEPI, the ISI and the suspension to try and narrow down the number of events that we need to do in depth analysis of.
The attached images show the interferometer lock loss as a function of earthquake velocity across O1 and O2.There is 11 bins ranging from 400nm/s to 2000nm/s peak velocity, using the 0.03-0.1mHz ground BLRMS channel. To account for the different arrival times of different waves during an earthquake I added a start buffer of an hour to the data search to avoid more events going in the 'previous lock loss' bin.
From this we find that work done during the O1-O2 break has enabled H1 to remain locked in earthquakes up to 1.5 um/s peak velocity, whereas during O1 the interferometer locked in only two earthquakes at 400nm/s peak velocity, obviously the number of datapoints is quite small, so these numbers may change with more earthquakes.
Here are a couple of photos of the BS AR elliptical baffle before alignment and after alignment. Hopefully this is stating the obvious, but the 2 photos that show the largest beam not well centered on the target are the 'before' pics and the more centered beam photos are the 'after' pics.
[Maddie W., Aaron V., Greg M.]
Here is a summary of the filters and command line arguments that should be used for the C02 frame generation using the DCS calibration pipeline. This information is compiled from configurations wiki page and aLOGs linked from that wiki page. The command line arguments should be the same as for C01 except for changes noted in the table below. (Additionally, the frame names and channel names should be changed appropriately to C02.)
GPS times | Filters files | Special command line arguments | Change from previous epoch |
---|---|---|---|
1163173888 - 1167436818 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1163173888.npz |
--expected-fcc=347.2 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
N/A |
1167436818 - 1169326080 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1167436818.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Calibration model changes New H1 params file created on 1/3/2017 Coupled cavity pole frequency changed in reference model |
1169326080 - 1173225472 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1169326080.npz | same as above | New H1 params file created on 1/24/2017 (see aLOG 33585) |
1173225472 - end of run |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1173225472.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Include EPICS to compute SRC detuning parameters NOTE: Starting with these frames there will be additional channels in the frames for the SRC detuning parameters |
After a discussion with the review team, we are just going to use a taper length of 32768 for both LHO and LLO. I have therefore just made this the default in the code. You do not need to set the --fcc-filter-taper-length option for C02 frame generation.
We have finished our rounds of testing and are settling on the options used to produce the X05 test frames (summary page here). Below is an updated table of the command lines to be used:
GPS times | Filters files | Special command line arguments | Change from previous epoch |
---|---|---|---|
1163173888 - 1167436818 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1163173888.npz |
--expected-fcc=347.2 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
n/a |
1167436818 - 1169326080 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1167436818.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Calibration model changes New H1 params file created on 1/3/2017 Coupled cavity pole frequency changed in reference model |
1169326080 - 1173225472 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1169326080.npz | same as above | New H1 params file created on 1/24/2017 (see aLOG 33585) |
1173225472 - end of run |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1173225472.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Include EPICS to compute SRC detuning parameters NOTE: Starting with these frames there will be additional channels in the frames for the SRC detuning parameters |
[Gerardo, Koji]
The isolation measurement of the OFI was repeated today to confirm the stability of the optical isolation performance. For the confirmation, we have used the usual photodiode technique, as well as the power meter. Also we made the dry run of the in-situ isolation test setup [LHO ALOG 39357]. All the measurements showed the consistent isolation better than 40dB. We are going to install the OFI optical table to HAM5 tomorrow.
Methods
Results
LHO OFI 2017/11/13 After the adjustment [LHO ALOG 39418] |
LHO OFI 2017/11/14 PD measurement |
LHO OFI 2017/11/14 Power meter measurement |
LHO OFI 2017/11/14 In-situ measurement |
|
Temperature of the faraday rotator body |
N/A | N/A | 73degF = 22.8degC | 76degF = 24.4degC |
Transmission From the input port to the output port |
0.967 +/- 0.002 (3.3% loss) |
--- | --- | --- |
Back-scatter isolation S-pol From the input port to the squeezer port |
1300 +/- 10 ppm | --- | --- | --- |
TFP AR reflection From the input port to the squeezer port |
890 +/- 10 ppm | --- | --- | --- |
Isolation From the output port to the input port |
52 +/- 13 ppm ( = 43 +/- 1 dB isolation) |
48.4 +/- 0.7 ppm ( = 43.15 +/- 0.05 dB isolation) |
42 +/- 2 ppm ( = 43.7 +/- 0.3 dB isolation) |
34.5 +/- 0.4 ppm ( = 44.6 +/- 0.5 dB isolation) |
Back-scattering From the input port to the input port |
3.0 +/- 0.5 ppm | 0.5 +/- 0.2 ppm | 2 +/- 3 ppm | --- |
Squeezer transmission From the squeezer port to the input port |
0.978 +/- 0.002 (2.2% loss) |
--- | --- | --- |
Keita, Jason, Ed, Betsy
After the IO group installed the MC bypass today, Keita, Jason, Ed and I embarked on the beam pointing from the PR to the ITMs. We centered PR2 to PR3, then PR3 to ITMx-CP. We utilized the new target that was already on PR3, but the beam is many inches in diameter and viewing was difficult (as anticipated). Still we think we could see it well enough to have it centered to within ~1cm on the target. We then removed this target and the iris in front of PR2 (which likely was clipping the diameter a bit), and looked down at the BS and then CPX. Again this was difficult, but also doable to within ~1cm. Jason and Keita were inside the BSC chamber and used a series of rulers and IR viewers to find reference of the beam placement on the optic centerline.
Attached is the snapshot of the IFO alignment slider settings as we've left it for the night. We'll resume the BS to SR cavity optics tomorrow. (We'll also continue on the Elliptical baffle alignments when the newly fabbed target is out of clean and bake tomorrow morning.
Note, we had to ask Chandra to turn down the purge a tad in order to quiet the beam a bit.
Ed talked to Kyle and Ed is turning the purge back up.
[Kyle, Chandra]
We opened back up GV6 this afternoon after closing it last Friday to leak hunt. Recap: we checked the annulus systems on GV 5,6 & all in between for inner o-ring leaks (no leaks). We discovered 10" GV on CP1 was not tight and the volume capped by ISO flange was up to air, likely causing a slow leak into main volume. We did not spray GV 5,6, CP1, spool with helium.
We replaced the ISO with conflat reducing cross that can accommodate a turbo pump plus full range gauge and pump port. There seems to be a small (e-9 Torr-L/s) leak somewhere in this reducer cross but results are ambiguous and should not affect performance since it's behind the closed 10" valve.
The pressure reading on PT-124 (beam tube side of GV6) has dropped since tightening 10" GV, but value hasn't fallen below 5e-9 Torr which is where it is when isolated from leak. We may revisit this when we have access to the main YBM turbo for He leak checking. I would like to check the 10" GV gate seal and gappy flange at bottom of CP1.
TITLE: 11/14 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC STATE of H1: Planned Engineering LOG: Dust alarms in optics labs in morning, likely due to AHU-3 work. 15:49 UTC Email from Bubba reporting that he is taking AHU-3 down 15:50 UTC Larry M. through gate 15:59 UTC Jeff B. to YBM and resetting dust monitor 4 16:10 UTC Bubba, Richard, Larry M., Victor C. to LVEA to look at TCS table 16:18 UTC Jeff B. back. Dust monitor 4 restarted. 16:22 UTC LN2 delivery truck through gate 16:26 UTC Hugh to HAM3 to balance ISI 16:52 UTC Cintos through gate 16:56 UTC Betsy to LVEA to talk to Hugh 17:00 UTC Betsy back 17:06 UTC Jim to LVEA to help Hugh 17:11 UTC Betsy and Keita taking camera crew to bier garten. Betsy also unlocking PR3. 17:12 UTC Ed to LVEA to prep for HAM2 work 17:18 UTC Ed and Cheryl installing alignment hardware in HAM2 17:23 UTC Travis to LVEA to investigate problems with walkie-talkies 17:39 UTC Jason to LVEA to talk to Cheryl 17:43 UTC Jason back and starting adjustment of PSL diode currents 17:52 UTC Travis back 17:55 UTC Chris to LVEA for FAMIS tasks 18:03 UTC Jeff K. to LVEA to help Cheryl and Ed transition to laser hazard 18:10 UTC Chris done 18:13 UTC Jim back 18:23 UTC Jason to HAM2 18:26 UTC Marc to mid Y to pickup and drop off parts 18:33 UTC Betsy, Keita and camera crew back 18:34 UTC Jason back and reports LVEA transitioned to laser hazard 18:42 UTC Keita to HAM2. Vern taking camera crew to HAM2. 18:52 UTC Camera crew getting a different camera 19:06 UTC Karen leaving end Y 19:18 UTC Gerardo to optics lab. LN2 delivery truck through gate. Sheila and Terry to squeezer bay. Kyle and Rakesh to LVEA to leak check CP1. 19:36 UTC AHU-3 back on 20:35 UTC Betsy to LVEA to talk to HAM2 group 20:37 UTC Terry back HAM2 group out for lunch 20:58 UTC Betsy back and starting transfer functions of PR2 and PR3 21:25 UTC Terry back to squeezer bay. Turning squeezer laser on. 21:50 UTC Ed, Keita and Jason to HAM2 21:56 UTC Kyle to end Y 21:58 UTC Betsy to LVEA 22:29 UTC Kyle back 22:41 UTC Chandra to LVEA. Chandra and Kyle leak checking around CP1. 22:52 UTC Koji to optics lab 23:21 UTC Vern and camera crew back 23:44 UTC Marc to mid Y 23:49 UTC Toggled PSL FSS autolock to relock FSS
[Gerardo, Koji]
As reported before [LHO ALOG 39359], we confirmed the disqualification of the installed OFI in terms of the optical isolation. The OFI was pulled out and place in the optics lab. [LHO ALOG 39366].
Yesterday, the optical performance of the OFI was tested without any adjustment and then after the performance optimization. The reasonable performance was recovered. It's hard to believe that we can keep this 43dB isolation forever under environmental fluctuations.
Next steps: Today, some of the measurement will be repeated for confirmation of the stability. In addition, a dry run of the in-situ isolation measurement will be done in the optics lab to pin down the reference numbers and accuracy/precision.
Here the detailed testing procedure can be found in E1700350.
LHO OFI 2017/11/13 Before the adjustment |
LHO OFI 2017/11/13 After the adjustment |
|
Transmission From the input port to the output port |
0.973 +/- 0.002 (2.7% loss) |
0.967 +/- 0.002 (3.3% loss) |
Back-scatter isolation S-pol From the input port to the squeezer port |
1960 +/- 20 ppm | 1300 +/- 10 ppm |
TFP AR reflection From the input port to the squeezer port |
N/A | 890 +/- 10 ppm |
Isolation From the output port to the input port |
1800 +/- 200 ppm ( = 27.4 +/- 0.5 dB isolation) |
52 +/- 13 ppm ( = 43 +/- 1 dB isolation) |
Back-scattering From the input port to the input port |
2.3 +/- 0.4 ppm | 3.0 +/- 0.5 ppm |
Squeezer transmission From the squeezer port to the input port |
0.974 +/- 0.002 (2.6% loss) |
0.978 +/- 0.002 (2.2% loss) |
The transmission was checked with a Thorlabs power meter with an integrated sphere. The numbers were 0.972+/-0.004 and 0.971+/-0.006. But the systematics is large (+/-1%) everytime the number is measured.
Other OFI Performance to compare:
LLO OFI Performance summary [LLO ALOG 25788]
Previous LHO OFI measurement in the opt lab [LHO ALOG 39276]
What has been done:
- A noticeable thing was that the half-wave plate (HWP) was not tightly fastened in the holder. It is a notorious holder (Attached Pic) that the HWP can still jiggle in the holder even the screw is fastened with a normal torque. This was the issue the initial OFI of the LLO (actually... this unit). This time, the screw was fastened much tighter with an Allen key.
- Other alignment was basically fine. The angle of the thin film polarizer (TFP) was a bit tweaked to minimize the backscatter iso, but it seems that this is the minimum. This may mean that the isolation was optimized by sacrificing the polarization purity of the transmitted beam through the faraday rotator and half wave plate.
Can you please note the temperature in the optics lab? Temperature changes of a few degrees will limit us to <40dB of isolation.
I don't have a thermometer right now. We will measure it.
Degradation of the isolation due to the temperature dependence of Verdet effect for TGG
When the isolation was optimized (< -40 dB), the backscatter isolation (S-pol of the transmission from FR+HWP) was 1300 ppm. Assume this was caused by the deviation of the rotation angle at the faraday rotator from the nominal 45deg.
Backward beam
Faraday: phi_0 = 45 + delta [deg]
HWP: phi_H = 45 - delta [deg]
Total: phi_0 + phi_H = 90 [deg]
Forward beam
Total: phi_0 - phi_H = 2 delta
==> S-pol power: sin[2 delta/180*pi]^2 == 1300ppm
==> delta ~ 1deg
Temp dependence of the faraday rotation
FR had the rotation of 45deg + delta at T=298. According to JOSA B 9 (1992) 1912, the Verdet effect of TGG crystal has the temperature dependence of the follwoing form: phi = a (6751/T - 6.968) [deg]. a is a constant. T is the temperature in K. In our case, phi = phi_0 at T=298. This gives us a=2.935. ==> dphi/dT @T=298 = -0.223 [deg/K]
This will cause additional dphi = dphi/dT x dT rotation on the backward beam
Temp dependence of the isolation
So, the isolation is given by the following expression:
sin[dphi/180*pi]^2 = sin[-0.223 dT/180*pi]^2
This will hit 40dB (1e-4) at dT = 2.6 K and 30dB (1e-3) at dT= 8.1 K.
Temp dependence of the backscatter-isolation (and transmission)
This 2.6K deviation cause the backscatter isolation changing {+830ppm,-630ppm}.
For the 8.1K deviation, it changes {+3300ppm, -1300ppm}. The sign depends on the sign of delta.
To be checked:
- Temp dependence of the retardation of the half wave plate
- Temp dependence of the other optical parameters
Attached are the temperature trends from inside the optics lab (lab1 channel) and the vacuum prep lab (lab2 channel), data taken from the dust monitors.
This morning I relieved the PR3 of the mechanical rubbing Kissel pointed out in 39384. The Front HR Upper Right stop was grounded on the face of the optic. I also freed up the locked down PR2. We'll run some TFs at lunch when IO is finished with the MC bypass install, but before alignment through the PR chain.
At lunch I took the needed TFs. Both suspensions look healthy now according to the 6 DOF TFs (each) which can be found in the usual spot at:
/ligo/svncommon/SusSVN/sus/trunk/HSTS/H1/PR2/SAGM1/Data/2017-11-14*.xml
and
/ligo/svncommon/SusSVN/sus/trunk/HLTS/H1/PR3/SAGM1/Data/2017-11-14*.xml
J. Kissel Since HAM4's construction / installation stuff for this vent is complete as of yesterday's HWS Scraper Baffle install (LHO aLOG 39266), and the debugging of SR2's M2 OSEM today (LHO aLOG 39277), I took the afternoon to start B&K hammering all of the new / old baffle equipment and HWS mirror / lens mounts. Note, I deliberately skipped the SR2 cage, since nothing has changed on it since it was originally measured in LHO aLOG 12089, and I trust that Betsy and Travis successfully re-dogged and torqued bolts when they finished the relocation a few days ago LHO aLOG 39240. Will post pictures and results next week.
I'm attaching some plots of Jeff's data. Would be nice if the B&K data were easier to get into a publishable form, I can't guarantee I haven't screwed something up in here, a lot of places where it would be easy to make a mistake. Some of the TFs have almost no coherence, Jeff said it was hard to get the accelerometer close in couple cases.
One extended point about getting data from the B&K machine. It's possible to export one data set at a time (i.e. get the tf & coherence for one channel). Then to get them in a manageable format for matlab, I used sed to remove the last seven lines and the first 84 lines from the exported data txt file. This was some thing of the form:
sed -i '6486,6492d' *100-1100*.txt
to remove the last seven lines of all of Jeff's data files that had 100-1100 in the name (for the frequency band) and:
sed -i '1,84d' *.txt
to remove the first 84 lines from all of the files in the directory. Best to backup your data before doing this, cause sed won't ask if you're sure. I had to try several times to get it right. The '1,84d' tells sed to delete lines 1-84. There's probably some clever way to tell sed to remove the last seven lines, I couldn't find it, so I just looked in the file to see how many lines there were.
Attached are pictures of each setup for the above B&K hammering, in case they need to be reproduced. Jim has volunteered to process the data.
J. Kissel I've taken new, more comprehensive B&K hammer response measurements of the H1SUSPRM and H1SUSPR3 cages, now that they have newly installed (what I'm calling) Venetian Baffles (see attached HAM2_NewBaffling_WithLabels.pdf for names of baffles) whose installation was finished last week LHO aLOG 39170. These baffles have pretty high-Q, low-frequency drum-head / longitudinal resonances (roughly aligned with ISI / IFO Y axis). PRM Upper: 42.38 & 46.75, 91.00 PRM Lower: 42.38 & 46.75, 75.62 PR3 Upper: 36.75, 75.6 PR3 Lower: 36.75, 83.12 My guess is that the lower frequency of the modes are the baffles bending in longitudinal in concert on the Venetian bracket, and the upper frequencies are their individual longitudinal modes. This mode-shape guess is based only on intuition, and that the lower frequency modes are seen in both upper and lower excitations. The cage's transverse modes appear to be relatively unaffected by the new baffles. I'm little surprised it hasn't stiffened up any of the transverse modes; oh well. These resonances have been identified by comparing against the history or cage resonance measurements for each of the SUS -- see the three pdfs: 2017-10-30_H1SUSPR3_CageResponse.pdf 2017-10-30_H1SUSPRM_CageResponse.pdf 2017-10-30_H1SUSPRMvsPR3_CageResonance_Comparison.pdf Note, also new with these measurements -- data out to 1.1 kHz. The former data is from LHO aLOG 6014 -- VA ON vs OFF data for H1SUSPRM and H1SUSPR3 LHO aLOG 8654 -- Former Cage Baffles on H1SUSPR3 Photos attached (and remaining HitLocations.pdf) are for historical reference for future repetition.
From Stephen and Norna
We (Stephen, Norna, Calum, Cormac) have done further experiments in the lab at Caltech to better understand the effect of the addition of the "Venetian blind" baffles ( D1700256 HSTS BAFFLE ASSY.PRM), on an HSTS and to help with the interpretation of the results seen at LHO.
A few caveats which should be noted:
a) We only have a bare structure - no vibration absorbers, hanging suspension, cables etc. attached. Also not as well dogged down as on site due to potential interference with baffle (our HSTS is not on a spacer). We have included baseline results displaying excitation of this structure without baffles mounted for comparison, see figures 2a and b described below.
b) We only used one baffle panel - so it was either attached at lower or upper position. See figure 1 for set-ups.
Basic findings
1) We show with and without damped baffle in upper position, exciting at top of structure in longitudinal (beam) direction and transverse. Basic conclusion, we do not see noticeable new resonances when exciting structure itself. See figures 2a and 2b
2) We only see extra low frequency ( ~ 40 Hz in our case) resonance introduced by baffle when directly hitting on the baffle. It is not seen when excitation is done to the structure itself. It is also only seen when hitting the baffle in its upper position, not in the lower position. See figure 3 for upper position results.
*We strongly suggest that if time permits, a test where the structure itself is hit in the longitudinal (beam) direction is done at LHO to see if this finding also holds for the PRM suspension now in situ.* From our experience we expect those low frequency peak(s) not to appear or least to be less prominent when the structure itself is excited.
3) The viton O-rings in the attachment units make a significant beneficial difference to the behaviour. Adding a baffle without viton introduces extra features which are suppressed or damped with the introduction of the viton.
See figures 4 (upper) and 5 (lower) baffle results.
4) The viton also adds some damping to the original structure resonances, apart from the first two flagpole resonances at 65 Hz (longitudinal) and 75 Hz (transverse) for our set-up. The dominantly torsional mode at ~160 Hz in our set-up shows some damping, as does the ~350 Hz feature. This can be seen particularly in the transverse results.
See figures 6 (upper) and 7 (lower).
5)We also did some investigations of different tightening levels corresponding to different levels of compression of viton O-rings within the two different flavors of attachment unit, D1700232 and D1700236. Basic result: the system is quite tolerant to different levels of tightening,with similar results over a range from hand tightened plus 1/4 turn to hand + full turn.
We will write this up more fully on the DCC at T1700473, including posting all data sets.
I have added one further set of comparison traces. In figure 8 we show the effect of including the damping O-rings in the baffle attachment units, where we are now comparing the results when hitting directly on the baffle in its upper position, rather than hitting the structure as shown in figure 4. We see again that the damping makes a significant beneficial difference.
S. Dwyer, J. Kissel While inspecting HAM6 regarding the broken OMC REFL Beam Diverter Dump, we took the opportunity to check out the fast shutter. We saw several things of concern: (1) The cabling that emanates from the shutter itself looks (and has been previously confirmed to be) very close to the main IFO beam path. Koji indicated in his LHO aLOG 28969 that "the clearance does not look great in the [above linked] photo but in reality the beam is clearly away from the wire." (2) One of these wires (the wire closer to the IFO beam) has a kink in it, but no visible burn marks, so we suspect this is from mechanical manipulation during install. (3) OM3's readout cables are kinked in a stressed position to make room for the fast shutter, which is a little forward (-Y, away from the beam splitter) of the position indicated in the drawing likely because of this interference. (4) Some small fleck of particulate on the inside of the "toaster" face, on the HR (back towards OM1) side of the shutter. I attach picture collections of these things (admittedly the particulate pictures are not great -- we tried lots of times to get a good picture but failed). Hopes: Re (1): Can we find a way to route these cables below the beam line, instead of surrounding it? Re (2): Same as (1) Re (3): Can we replace OM3's OSEM cables with a 90 deg backshell, so as to clear room for the fast shutter and relieve stress on the cable? Re (4): hopefully this is not from the HR surface of the fast shutter optic
We were motivated to look at the fast shutter wires by the incident on July 17th where the wire from the fast shutter must have been clipping the to OM1 from HAM5. My original alog about this might not have spelled things out well enough, so here are some plots.
The first plot is from July 17 2017 5:51:00 UTC, this was after Jim, Cheryl and I figured out that the fast shutter was malfunctioning. We locked DRMI, and opened and closed the fast shutter several times. The top panel shows the state of the shutter, 0 is open 1 is closed. The second panel shows AS_A_SUM, which is downstream of the shutter, and goes to zero when the shutter is blocking the beam as it should. The third panel shows AS_C, which is upstream of the shutter but downstream of the place where the wire is close to the beam (check Jeff's annotated photo). You can see that moving the shutter causes dips in the amount of light on AS_C, and that the wire must land in a slightly different place in the HAM5 to OM1 beam causing a different level of light to be seen on AS_C
The second attachment shows that the shutter did seem to block the beam going to the AS WFS in the July 16th lockloss before we had this malfunction. Chandra also checked vacuum pressures for a spike in HAM6 pressures similar to what happened when we burned the OMC in August 2016, and saw nothing. I had been wondering if the fast shutter might have failed to durring a lockloss where the OMC was unlocked, which could result in a lot of power being on the beam dump. It seems like this didn't happen on July 16th.
Note, we played with this shutter cable last in Aug 2016. We struggled with getting this wire away from the beam at that time. The pictures in the log from Aug 2016 28969 show that we left the wire in a larger arc than the pictures show now. I suppose it's not so surprising that the wire has maybe migrated into the beam path over the numerous cycles over the last year.