Ibrahim and I went to End Y with the PS4 Working Standard to do a PCAL End Station measurement. We followed T1500062-V21 to complete the measurment suite with out any issues.
Here are the obligitory Before Beam spot pics.
Martel plots for ADC conversion.
Working standard at TX module with only One beam.
Working standard at the RX module with only One beam.
Working standard at RX module with Both beams.
Post measurement beam spots!
anthony.sanchez@cdsws25: python generate_measurement_data.py --WS PS4 --date 2026-07-16
Reading in config file from python file in scripts
../../../Common/O4PSparams.yaml
PS4 rho, kappa, u_rel on 2026-07-16 corrected to ES temperature 299.6 K :
-4.698647654693516 -0.0002694340454223 0.000750622815531554
Copying the scripts into tD directory...
Connected to h1daqnds1
martel run
reading data at start_time: 1469911700
reading data at start_time: 1469912270
reading data at start_time: 1469912670
reading data at start_time: 1469913100
reading data at start_time: 1469913500
reading data at start_time: 1469913900
reading data at start_time: 1469914560
reading data at start_time: 1469915320
reading data at start_time: 1469915650
Ratios: -0.5339859682199335 -0.543765733929218
writing nds2 data to files
finishing writing
Background Values:
bg1 = 18.671164; Background of TX when WS is at TX
bg2 = 5.156755; Background of WS when WS is at TX
bg3 = 18.605483; Background of TX when WS is at RX
bg4 = 5.281252; Background of WS when WS is at RX
bg5 = 18.674174; Background of TX
bg6 = -1.117857; Background of RX
The uncertainty reported below are Relative Standard Deviation in percent
Intermediate Ratios
RatioWS_TX_it = -0.533986;
RatioWS_TX_ot = -0.543766;
RatioWS_TX_ir = -0.526609;
RatioWS_TX_or = -0.535095;
RatioWS_TX_it_unc = 0.059001;
RatioWS_TX_ot_unc = 0.057064;
RatioWS_TX_ir_unc = 0.061781;
RatioWS_TX_or_unc = 0.063032;
Optical Efficiency
OE_Inner_beam = 0.985936;
OE_Outer_beam = 0.983757;
Weighted_Optical_Efficiency = 0.984846;
OE_Inner_beam_unc = 0.046465;
OE_Outer_beam_unc = 0.047412;
Weighted_Optical_Efficiency_unc = 0.066385;
Martel Voltage fit:
Gradient = 1637.889101;
Intercept = 0.085727;
Power Imbalance = 0.982015;
Endstation Power sensors to WS ratios::
Ratio_WS_TX = -0.927858;
Ratio_WS_RX = -1.383422;
Ratio_WS_TX_unc = 0.047658;
Ratio_WS_RX_unc = 0.041564;
=============================================================
============= Values for Force Coefficients =================
=============================================================
Key Pcal Values :
GS = -5.135100; Gold Standard Value in (V/W)
WS = -4.698648; Working Standard Value
costheta = 0.988362; Angle of incidence
c = 299792458.000000; Speed of Light
End Station Values :
TXWS = -0.927858; Tx to WS Rel responsivity (V/V)
sigma_TXWS = 0.000442; Uncertainity of Tx to WS Rel responsivity (V/V)
RXWS = -1.383422; Rx to WS Rel responsivity (V/V)
sigma_RXWS = 0.000575; Uncertainity of Rx to WS Rel responsivity (V/V)
e = 0.984846; Optical Efficiency
sigma_e = 0.000654; Uncertainity in Optical Efficiency
Martel Voltage fit :
Martel_gradient = 1637.889101; Martel to output channel (C/V)
Martel_intercept = 0.085727; Intercept of fit of Martel to output (C/V)
Power Loss Apportion :
beta = 0.998844; Ratio between input and output (Beta)
E_T = 0.991820; TX Optical efficiency
sigma_E_T = 0.000329; Uncertainity in TX Optical efficiency
E_R = 0.992968; RX Optical Efficiency
sigma_E_R = 0.000330; Uncertainity in RX Optical efficiency
Force Coefficients :
FC_TxPD = 9.158396e-13; TxPD Force Coefficient
FC_RxPD = 6.237025e-13; RxPD Force Coefficient
sigma_FC_TxPD = 4.417816e-24; TxPD Force Coefficient
sigma_FC_RxPD = 2.847865e-24; RxPD Force Coefficient
data written to ../../measurements/LHO_EndY/tD20260804/
WP13482
Jim, Erik, Dave:
h1seiey was powered down: computer, IO Chassis and AI chassis.
The IO Chassis A2 Adnaco backplane was replaced with a spare. The original backplane's slot3 failed during O4 (Oct 2025) and back then we shifted the cards left by one slot to avoid it.
| old backplane with broken slot3 (removed) | C8610513 |
| spare backplane (installed) | C8610832 |
I was then able to put the cards back into their original slots, making h1seiey identical to h1seiex. This meant A3 now had no cards installed, so I disconnected the A3 fibers from the rear of h1seiey.
For backplane testing we stopped the models from running to verify all the cards are seen. Auto start was turned back on, the system was powered up, the models started and lastly I powered the AI chassis back on.
Masayuki Nakano, Khanh Vu We successfully closed all of the JAC ASC loops. Attached below are the outputs from the two wavefront sensors. All of the signals converge to zero within approximately 30 seconds, indicating that the loops are working beautifully. More details will be reported tomorrow.
TITLE: 08/04 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: Ryan S
SHIFT SUMMARY:
Slow day due to ongoing FAC water and outdoor air quality issues but the following was done:
LOG:
| Start Time | System | Name | Location | Lazer_Haz | Task | Time End |
|---|---|---|---|---|---|---|
| 14:45 | FAC | Kim | LVEA | Local | Technical Cleaning | 15:18 |
| 15:21 | SQZ | Camilla | LVEA | Local | Taking Viewport covers off HAM5 | 16:13 |
| 15:31 | FAC | Kim | LVEA | Local | Technical Cleaning | 16:15 |
| 16:11 | ISC | Jennie | Optics Lab | Local | Looking for parts | 16:13 |
| 16:17 | JAC | Jennie, Masayuki | LVEA | YES | IOT1 beam profiling, then IOT2L beam pwr meas. | 19:17 |
| 16:21 | FAC | Chris | LVEA | YES | FAMIS Tasks | 17:21 |
| 16:31 | JAC | Khanh | LVEA | YES | Joining JAC Team | 20:02 |
| 16:37 | SEI | Jim | LVEA HAM2 | yes | Chcking signal paths | 17:58 |
| 17:16 | VAC | Jordan | LVEA GV6 | y | Getting parts. | 17:25 |
| 18:30 | CDS | Dave | EY | N | SEI Chassis work | 20:02 |
| 18:40 | SQZ | Camilla | LVEA | YES | HAM7 power measurements | 19:34 |
| 18:42 | SQZ | Ryan S | LVEA | YES | HAM7 Power measurements | 19:34 |
| 19:33 | PCAL | Tony | PCAL Lab | Local | Staging parts | 19:53 |
| 19:39 | FAC | Randy | LVEA | Y | Scissor Lift Work | 20:39 |
| 19:54 | CAL | Tony, Ibrahim | EY & Lab\\ | Y | PCal measurement | 22:18 |
| 20:50 | SQZ | Camilla | LVEA | - | Covering HAM5/7 viewport | 21:16 |
| 21:44 | SQZ | Camilla | LVEA | Y | HAM7 power budget | 00:44 |
| 22:01 | SQZ | Ryan S | LVEA | Y | HAM7 power budget | 23:13 |
| 23:31 | SQZ | Sheila | LVEA | Y | HAM7 power budget | 01:31 |
| 23:31 | CDS | Dave | EY | N | Chassis work | 23:32 |
It is also worth nothing that as of 16:30 PT, there are no active fires in Benton or Franklin county per Watch Duty.
Jennie Wright, Masayuki Nakano, Khanh Vu This morning we worked on several tasks on the IOT1 table, including installing the camera and shutter, profiling the beam, and calibrating the DC power. We identified a new location for the camera using the beam transmitted through JACR_M5. During this process, Masayuki noticed that the beam was being clipped by the shutter. We suspect that the beam may have been clipped for some time. We then installed the camera in its new location, and Masayuki aligned the shutter on the table. Next, we profiled the beam for the wavefront sensors. We found that the Gouy phase separation between the two WFSs is approximately 70 degrees. We decided to leave the current configuration as it is since the separation is good enough. Masayuki will make a plot and perform a more detailed calculation later. We also maximized the laser power in the REFL path by optimizing the waveplate angle. When JAC is unlocked, the measured power on the RFPD is 5.1 mW, and the trigger PD voltage is 0.28 V. When JAC is locked, the measured power decreases to 0.4 mW, and the trigger PD voltage is 0.02 V. Since the beam is split evenly, each WFS receives approximately 2.55 mW of optical power. Finally, we calibrated the DC readout of RFPD by converting counts to mW. Before performing the calibration, Masayuki checked the alignment and recentered the RFPD. He then recorded two sets of measurements, each averaged over 10 seconds: Measurement #1 * JAC_REFL_A_LF_INMON: 1072.3966186523437 counts * DC power: 4.4 mW Measurement #2 * JAC_REFL_A_LF_INMON: 1073.5228637 counts * DC power: 4.5 mW After the calibration, we updated filter number 10 with the new coefficients.
The beam profile between the beamsplitter and the JAC WFS was measured. Here I fit a Gaussian beam to those measured beam sizes and convert the WFS locations into Gouy phase.
The measured beam diameters were fit independently in x and y with the standard Gaussian beam model, w(z) = w0 * sqrt(1 + ((z - z0)/zR)^2) with zR = pi * w0^2 / lambda and lambda = 1064 nm:
| w0 [um] | z0 [m from JACR_BS4] | zR [cm] | |
|---|---|---|---|
| x | 141.2 | 0.377 | 5.89 |
| y | 151.9 | 0.370 | 6.81 |
The beam is slightly astigmatic, so x and y are treated separately throughout.
The positions of WFS A and WFS B were measured with a ruler from the same reference as the profile scan: WFS A at z = 0.325 m, WFS B at z = 0.410 m. The corresponding Gouy phases, psi(z) = arctan((z - z0)/zR), are:
| WFS A [deg] | WFS B [deg] | Separation [deg] | |
|---|---|---|---|
| x | -41.3 | +29.5 | 70.8 |
| y | -33.5 | +30.4 | 63.9 |
The separation is 71 deg in x and 64 deg in y, not the optimal 90 deg. This is not optimal, but it is not terrible either: the two WFS remain well separated in Gouy phase and the sensing matrix would not be close to degenerate. Given the time available we did not optimize the layout.
If we want to optimize it later, the fix is straightforward: moving WFS A upstream (toward the BS) by about 5 cm in x / 7 cm in y, i.e. from z = 0.325 m to roughly z = 0.27 m, brings the separation to 90 deg. WFS B does not need to move.
TITLE: 08/04 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
SEI_ENV state: CALM
Wind: 4mph Gusts, 1mph 3min avg
Primary useism: 0.01 μm/s
Secondary useism: 0.08 μm/s
QUICK SUMMARY:
IFO is in IDLE for MAINTENANCE
Today, we anticipate some Ion Pump work from Vacuum and some comissioning work after Tues Maintenance
Workstattions were updaed and rebooted. This was an OS packages update. Conda packages were not updated.
FAMIS 63910
Last Tuesday's interlock work and brief time in the enclosure are clearly seen on many trends, and essentially everything came back as expected. One item of note is the PMC, which relocked at a slightly higher temperature, which seems to have caused the transmitted power to be a bit lower while the reflected power is a bit higher.
[Keita, Elenna]
Sheila and I struggled to lock SRY last Friday, 91360. Keita and I revisited today.
To start, I ran the usual SR2 alignment, which centers the beam on AS_C, and the AS centering which centers OM1,2 on AS A and B.
Then, we could see a large beam at the center of the AS AIR camera, and a strange fringing beam at the top edge of the camera. We swept SRM in both pitch and yaw to both edges and saw the beam disappear. This convinced us that we were seeing the two beams we needed to overlap in SRY, however, there was not an SRM alignment that could overlap the two beams.
Keita first moved ITMY 10 urad in pitch, and was able to overlap the two beams. He then undid that alignment and moved the beamsplitter instead. We were able to achieve the SRY fringing and then lock SRY with the guardian. The resulting beam ended up on the top edge of th AS AIR camera view.
Using that beamsplitter alignment, we then relocked MICH dark, which required a large movement of ITMX, since we had decided to maintain the beamsplitter and ITMY alignment. ITMX is now at P: -135 and Y: 113.1 on the sliders. This means it has been moved relative to where it should be according to a previous arm alignment we achieved.
We can still see the MICH fringes on the ISCT1 refl camera with this alignment.
We can also lock PRX, with a movement of PRM. We still see no beam on POP A or B, so Keita is scanning the input alignment.
The attached screenshot shows the alignment sliders after we locked SRY, MICH, and PRX.
I'm not sure if we are happy with this alignment overall, since we're not sure if this is where we want the ITMs.
Attached is a not-to-scale, super-simplified cartoon so people understand what happened. As of now, ITMY is unchanged (because I reverted the changes temporarily made to ITMY), BS is angled in PIT, ITMX was angled mostly in PIT to follow the BS motion.
Initial state is in the top cartoon. The symptom that the two beams (single bounce and reflection of SRM reflected back by ITMY) didn't interfere well only meant that the beam was not retro-reflecting on ITMY.
This could be remedied by many different ways. At first I moved ITMY just to confirm that something like this was going on, and we did confirm that (because we were able to make the SRY fringe deeper).
Once we confirmed this was actually the case, I reverted the ITMY back, moved BS, and refined SRM using SRY fringe. The bottom cartoon represents this final state.
Though it's not captured in the cartoon, this of course made the MICH fringe wrong, so we moved ITMX, too.
Using BS or ITMY (or a combination of them) is not the only way though, you can change the angle of the beam from PR3 hitting the BS and refine SRM alignment to recover a good SRY fringe depth. As long as the beam is still on ITMs it will work. I haven't done that bacause it was late and I wanted to see the beam on POP_A or B, but we should.
Note that, ultimately, the good alignment of the ITMs, BS and PR3 won't be known until we open the arms. There's no magic in the current alignment we have (or even after using PR3 instead of BS to regain SRY fringes).
The main purpose of this excercise is just to confirm that nothing terrible is going on in the SRC chain. Because of the things described in Elenna's alog above, we already know that nothing terrible is going on. The rest is just an effort to gradually, maybe, approach the good alignment (on a belief that we already know the good angles for ITMs).
After discussion this morning, I put the ITMX sliders back to the O4 alignment position: pitch = -113 and yaw = 104.6
Per WP 13472 updated h1daqfw0 to use the new auto-reconfiguring frame writer. This is the same code has been running on h1daqfw2 for months in a test mode.
I also did an inplace upgrade of h1daqfw0 to Debian 12, which is what h1daqfw2 is running and what we have tested as.
Erik helped with package wrangling for Debian 12. I had been running h1daqfw2 from the experimental repository (which is a snapshot of the continous integration system). We were able to move this from using the experimental repository to the unstable repository. We will move it up to production later. We don't have a full Debian 12 release of advligorts as we are not planning on supporting the rcg and real time code on Debian 12.
Dave and I will be watching the timings and checksums to make sure everything looks good. The IO setup is a bit different between h1daqfw2 and h1daqfw0 (fw2 writes to local disk, fw0 to a NAS).
As the new framewriter is a different piece of software, we track different metrics. So we will need an updated edc capture list and a daqd restart.
A note about what this system brings in.
* It automatically changes its configuration when there is a channel list. It is a step towards not having daqd restarts (those don't go away while we have the daqd in other places).
* When we restart the daqd we usually have a gap of several frames. We hide this from the outside world by having two frame writers and only restarting one at a time. This reconfigures the channel list and does not have gaps unless you actually restart the program.
* It is also being used in the ngdd work to write derived frame data, so that we have a common frame writer (we just change the input type).
TITLE: 08/03 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
SEI_ENV state: CALM
Wind: 11mph Gusts, 7mph 3min avg
Primary useism: 0.01 μm/s
Secondary useism: 0.07 μm/s
QUICK SUMMARY:
The well pump was not working today due to some electrical issue. Last I heard FAC had a contractor on site to check on the well. So there is limited amounts of water here. Many folks were asked to work from home if they can.
GRB-Short E644098 @ 17:29 UTC
Jonathan started working on the FrameWrite0 today, installing Deb12 OS.
End stations were misaligned today to some tests that Camilla was doing.
ITMX ISI Stage 1 & 2 WD tripped twice today. Jim went out to the CER today to fix this.
Vac Team did some work on the GV6 Gate Valve today and GV6 is currently Open on the Y arm, But GV5 is still closed so the corner volume is still not open to the Arms yet.
| Start Time | System | Name | Location | Lazer_Haz | Task | Time End |
|---|---|---|---|---|---|---|
| 15:10 | FAC | Kim | LVEA | y | Technical cleaning & resupply | 17:00 |
| 15:41 | CDS | EJ | Remote | N | Test on OAF | 15:42 |
| 15:43 | FAC | Tyler, Eric, & contractors | EY | N | Working on the well | 20:39 |
| 15:48 | SQZ | Camilla | LVEA HAM5 | YES | Opening ViewPort on HAM5 | 15:55 |
| 16:10 | FAC | Kim | Mid X | N | Tecnical Clkeaning & resupply | 17:01 |
| 16:11 | SEI | Jim | LVEA | n | working on SEI near BSC2 | 18:08 |
| 16:41 | VAC | Jordan & Travis | LVEA GV6 | N | Working on the Gate Valve | 18:39 |
| 17:20 | SEI | Jim | remote CER | N | Tests on HAM2 & looking at Wiring | 18:22 |
| 17:25 | VAC | Gerardo | LVEA | N | Checking on GV6 work | 19:25 |
| 17:45 | CDS | Partick | MSR | N | CDS work? | 18:06 |
| 18:39 | FAC | Kim | HAM Shaq | N | technical Cleaning & Resupply | 19:07 |
| 19:05 | CDS | Jonathon | Remote | N | Re-imaging FW0 | 22:04 |
| 19:59 | SEI | Jim | Remote | N | Tests on HAM3 | 21:25 |
| 20:03 | VAC | Jordan | LVEA | N | Getting pics of GV6 | 20:07 |
| 20:51 | VAC | Travis & Gerardo | End Y | N | Using the pump cart for Anulus work. | 21:28 |
| 21:10 | SQZ | Camilla & Ryan S | LVEA HAM7 | YES | Beam Profiling with M2**2 profiler. Ryan Out early | 23:10 |
| 21:12 | SEI | Jim | CER | N | troubleshooting ITMX ISI WD trips. | 21:24 |
| 21:43 | VAC | Jordan | LVEA GV6 | N | Checking on GV6 status | 22:28 |
| 22:41 | VAC | Jordan & Gerardo | LVEA GV6 | N | Opening GV6 | 00:11 |
| 22:46 | SQZ | Sheila | LVEA HAM7 | YES | Working on the Power budget | 00:16 |
Keita and I took an opportunity while JAC was offline to run all the dark offsets. I ran the usual dark_offsets_exe.py from userapps isc/h1/scripts/dark_offsets
I did not visually check all of them but the ones I compared before and after in SDF looked reasonable.
Some of the whitening gain settings have been set strangely for the vent, so this should help fix that now that we have reset the proper settings.
SDFed, see screenshots.
After we ran, Keita and I realized the whitening settings for POP B were still wrong, so I corrected them and reran the offset for the POP B segments. Added screenshot.
Sheila, Ryan S, Camilla
We spent the morning repeating 90783, now that ZM4 preloading has been adjusted (90951) and ZM5 has been swapped and now has a different preloading than our O4 ZM5 (91292):
Sheila then used her script to run OMC scans at a grid (below) of PSAMS locations. These initially look great, showing sqz to omc mode mismatch is as good as 1%. with some alignment fluctuations. Ndscope of data taking attached.
Ryan then took M^2 measurements on SQZT7 of a slightly different grid:
Below I calculate the astigmatism based Ryan's grid of M^2 measurements.
I compute the 1D overlap between the x and y directions using the q values from the M^2 measurements
eta_1D = 4*zRx*zRy / ( (z0x - z0y)^2 + (zRx + zRy)^2 ) where z0 is the waist position and zR is the rayliegh length = pi * w /(M^2*lambda)
The astigmatism, which i express as 1 - eta_1D is tabulated below in %
| ZM5 \ ZM4 | -3.2 | -1 | 1.2 | 3.4 |
|---|---|---|---|---|
| -8 | 0.52 | 0.52 | 0.55 | 0.59 |
| -6.75 | 0.51 | 0.48 | 0.60 | 0.64 |
| -5.5 | 0.56 | 0.55 | 0.62 | 0.50 |
| -4.5 | 0.57 | 0.56 | 0.55 | 0.36 |
| -3.3 | 0.52 | 0.50 | 0.40 | 0.29 |
| -2 | 0.42 | 0.50 | ||
| -1 | 0.56 | 0.78 | 0.62 | 0.15 |
The dependance is pretty weak over much of the grid, but things get a bit squirly in the lower right corner near the positive end of the range for both PSAMS. We're not as sensitive to the strain gauge setting as ZM2 (91185), but there's clearly a noticible dependence.
Travis, Gerardo, Jordan
During the closing of GV6 back in May, we noticed that there was some blow-by in the pneumatic system when trying to hard close the valve, see alog 90093.
We were able to hard close the valve eventually but as preventative maintenance we wanted to replace the air cylinder seals, similar to GV7.
Prior to disassembly we measured the locations of the reed switches from the top surface of the bottom plate to the bottom surface of the reed switches:
Bottom Switch: 1 1/8"
Top Switch: 49 1/4"
We then disassembled the air cylinder and replaced the seals following procedure/notes collected during the GV7 repair. During cleaning of the old grease on the piston head, we noticed there were two burrs on the top of the piston, we did not notice any damage to the inside of the cylinder, but as a precaution we used a small flat file to remove the burrs. We also chased the threads on the four threaded rods with a die to aid with reinstallation. After cleaning and inspection of the cylinder tube, we found no issues or damage so we decided to continue to use that cylinder and keep the new one as a spare.
No other issues encountered, we removed the old seals, cleaned the grooves, added copious amounts of the supplied grease to the o-rings, seals and the inside of the air cylinder, and then re-assembled the cylinder tube. Pictures posted below and a final procedure is in progress and will be posted to the DCC.
We did not get a chance to cycle the valve after the seal replacement, so we will continue tomorrow with cycling the valve.
We were unable to fully open GV6 today after the cylinder repair. We heard the clunk of the gate camming over at 45 psi, but it did not start to raise until 55 psi, at which point we could hear air blow-by at the solenoid manifold, and up at the cylinder itself.
So we stopped trying to open the valve any further and slowly reduced the regulator output in order to bleed out the accumulated pressure on the bottom side of the piston. This lowered the gate back down and we heard the gate touch down indicating it is soft closed.
We will have to disassemble to air cylinder again and see what may be the issue. We still have 4 sets of replacement seals and one brand new air cylinder on hand if needed.
The valve remains soft closed until we are able to troubleshoot and repair the cylinder.
8/3/2026
Travis, Gerardo, Jordan
Today we again disassembled the GV6 air cylinder with the valve soft closed to try and see what may have been causing the air blow-by which prevented us from fully opening the valve last week.
We did not find anything immediately obvious such as a seal that had jumped out of the groove, so we measured the ID of the original air cylinder, which was re-used, and found that it was ~0.01" larger than the ID of the spare cylinder (original ID ~8.015", spare ID ~8.005"). We then elected to use the spare cylinder instead to make sure there is good sealing contact with the cylinder wall, so we re-distributed the grease on the new cylinder and attempted to install over the piston, but the tube seemed to be slightly out of round and would not fit over the piston. So we flipped the tube 180 degrees and measured that side of the tube and found it was better. We again added grease to that side of the cylinder and installed it over the piston, ensuring the seals and wear band stayed in place, Then we re-installed the threaded rods, torqued the nuts, installed the reed switches and installed the air lines.
To verify all the new joints/connections were ok, we put ~10 psi to the top of the cylinder and then to the bottom to see if there were any leaks. There were none so we started to open the valve by increasing air pressure at the regulator, once we got to ~25 psi we could hear and feel air coming out of the bottom plate/adapter flange below the cylinder assembly, see picture below the area where air is coming out of is circled in red, at which point we stopped trying to open the valve and closed the quarter turn isolation valve to the air line.
We spoke with a GNB rep who advised we try to to open at a higher pressure and see if the bottom seals, so we then tried to open the valve again. This time we started at 20 psi and followed our normal opening procedure with the exception of increasing by 5 psi instead of 10 and waiting 3 minutes between increases. At ~35 psi, air stopped leaking out of the bottom flange, there was no air blow-by in the cylinder and we could hear the carriage starting to move. The gate fully opened at ~48 psi and Gerardo was able to take a video where you can hear the piston incrementally move up the cylinder. We increased the holding pressure to 58 psi and verified the MEDM screen showed the valve status as green.
I used the earthquake down time from the weekend to look at the health of the BSC2-ISI sensors.
Sensors look OK (including the newly replaced H1 L4C - see alog 90840) except for CPS ST2 H1 (see red curve on the last plot) with large noise below 1Hz. This will need an investigation (I would start by swapping cables at the field box to see if it's an in-chamber issue).
Dtt Template lives under /ligo/svncommon/SeiSVN/seismic/BSC-ISI/H1/BS/Data/Spectra/Undamped/bs_all_sensors.xml
I had already done this test several years ago trying to diagnose the issue with BSC2, which, contrary to my comment in the alog Arnaud linked to, still has alot of flat looking excess noise in the 1-10hz. Arnaud's spectra here doesn't make me think this noise is due to a broken cps, the high frequency noise floor is unchanged, there's no evidence of glitching, unless it is some new failure mode.
Knowing that I would have few chances to try swapping in the near future, I did this over lunch when I went out to also unlock HAM1&2 hepi. I put BSC2 in damped, collected St2 CPS spectra, swapped the St2 H1 cps with a spare sensor, and got a comparison spectra. No change, see first attached spectra, refs are with the old H1 cps, live spectra are with the new sensor. I have left the spare sensor in for now, I will try to swap it back to the old sensor so we can preserve our ISI alignment (the new sensor reads a slightly different location that the old), but physically there should be no difference, the BSCs just use the free hanging position for the cps reference, unlike the HAMs.
Performance is no better with the new cps, as well, see second plot, refs are with the new cps, live is before the swap.
As dicussed with Jim on the phone it would be interesting to see the result of swapping H1 and V1 at the lemo input of the field cables - V1 noise is low enough between 10mHz-100mHz when the ISI is damped that the H1 noise would be obvious if it followed the cable.
Finally had a chance to repeat the test swapping st2 h1 v1 cps. Still no change, as I have seen when I did this test before. The excess low freq noise follows the in-air to feedthru and in-vac cables, so the problem is not from the satellite chassis or the CER rack. I can try to swap the cable from the feedthru to the satellite rack, but the work platform, crossbeam and feedthru protection make access to that difficult from pretty much any direction.
Attached spectra compare the nominal H1 V1 asds and the asds with the white in-air cables at satellite rack for st2 H1&V1 swapped. Dashed is nominal, solid is the swapped configuration. Red is the H1 channel, blue is the V1 channel.