Hugh unlocked HAM3 this morning after SUS people finished in there this morning. I've taken dtt tfs and they look ok. Hugh reported purge is high, so tfs look a little ratty, but resonances seem clear.
At approximately 12:33 UTC (4:33 PST), the 35W FE power watchdog tripped, causing the HPO power watchdog to trip ~6 seconds later (see 1st attachment). Looking at the laser power for the 35W FE shows the MOPA and the NPRO lose power at the same time, thereby causing the watchdog trip (2nd attachment; the little bump in H1:PSL-OSC_PD_AMP_DC_OUTPUT is simply residual light from the still operating HPO hitting the PD, it goes away once the HPO power watchdog trips). It is unclear what caused the FE to lose output power in this way. Putting all the signals from the 2nd attachment on one plot and zooming in, it appears the watchdog tripped before the FE lost output power (3rd attachment). Possibly a glitch in the PSL Beckhoff software?
The PSL was restarted without issue.
Nutsinee, Terry, Daniel
We installed all the in-air coax cables for the squeezer that were on hand. Six weeks after the promised delivery date, it still seems ~20% are missing due to being back ordered...
Fil et al. started laying down the long D-sub cables.
We also completed the missing chassis in the racks. All racks are now according to drawings with the exception of a missing quadplexer for WFS AS_B in ISC-R3.
Today, in HAM2/3 we:
While installing the north door on BSC 1 this morning, as we were inspecting the flange, I saw what appeared to be a rust spot on the flange in the sealing area of the inner O-ring at roughly the 5 o clock position (facing the BSC from inside the biergarten). I wiped, rubbed, and wiped again. I repeated this several times. There was no drag felt on the alcohol wipe, or on my clean gloves, no "rust residue" or any other foreign material came off on the wipe or glove. I put a piece of tape on the bolt head located near this position and showed Kyle the picture. Kyle said he would make a comment on this post.
The area of interest bridges the inner O-ring contact patch and might result in an inner O-ring leak. We began pumping the annulus space soon after this door was installed and will be able to get useful information via the pressure data as we will have atmosphere on the VE side of this inner O-ring for the next several days. Though undesirable, an inner O-ring leak wouldn't require immediate attention as would a leak across an outer O-ring. The main issue resulting from an inner O-ring leak is the scenario where relatively large amounts of air get introduced into the annulus volume as part of an annulus ion pump replacement. We have work-arounds for this case and, as a matter of policy, always assume that an inner O-ring leak exists when replacing ion pumps or otherwise have a need to introduce air into an annulus space.
Squashed bug? Who did I leave the stoning tools with?
John, I have the stones
4.4 x 10-6 Torr this morning at the cart backing the locally mounted turbo ("hung" turbo). This is excellent for the vent/pump duration.
WP7230
Sheila, Dave:
I have modified h1asc.mdl to reassign the ADC inputs. This model was compiled and installed, and is waiting for a restart tomorrow morning.
WP7230 also covers fixing a PSL bulls-eye channel issue. We believe this was resolved in hardware. Sheila will check if a software change is still needed. If it is, she will add it to her model changes (WP7227).
J. Kissel I've taken standard transfer functions of the IMs as we begin close-out of the HAM2 chamber. All IMs -- IM1, IM2, IM3, and IM4 -- are free of rubbing, and their dynamics look virtually identical to just-prior-to-vent measurements. We've still got plenty of other things to do, but the IMs are ready for HAM2 door closure. Huzzah! Attached are the results and comparisons. Raw data templates live in /ligo/svncommon/SusSVN/sus/trunk/HAUX/H1/ IM1/SAGM1/Data/2017-12-20_2122_H1SUSIM1_M1_WhiteNoise_L_0p01to50Hz.xml IM1/SAGM1/Data/2017-12-20_2122_H1SUSIM1_M1_WhiteNoise_P_0p01to50Hz.xml IM1/SAGM1/Data/2017-12-20_2122_H1SUSIM1_M1_WhiteNoise_Y_0p01to50Hz.xml IM2/SAGM1/Data/2017-12-20_2124_H1SUSIM2_M1_WhiteNoise_L_0p01to50Hz.xml IM2/SAGM1/Data/2017-12-20_2124_H1SUSIM2_M1_WhiteNoise_P_0p01to50Hz.xml IM2/SAGM1/Data/2017-12-20_2124_H1SUSIM2_M1_WhiteNoise_Y_0p01to50Hz.xml IM3/SAGM1/Data/2017-12-20_2140_H1SUSIM3_M1_WhiteNoise_L_0p01to50Hz.xml IM3/SAGM1/Data/2017-12-20_2140_H1SUSIM3_M1_WhiteNoise_P_0p01to50Hz.xml IM3/SAGM1/Data/2017-12-20_2140_H1SUSIM3_M1_WhiteNoise_Y_0p01to50Hz.xml IM4/SAGM1/Data/2017-12-20_2146_H1SUSIM4_M1_WhiteNoise_L_0p01to50Hz.xml IM4/SAGM1/Data/2017-12-20_2146_H1SUSIM4_M1_WhiteNoise_P_0p01to50Hz.xml IM4/SAGM1/Data/2017-12-20_2146_H1SUSIM4_M1_WhiteNoise_Y_0p01to50Hz.xml
R. Savage, J. Oberling, J. Driggers, S. Dwyer, P. King (via phone), R. McCarthy, F. Clara
This morning we completed the initial in-air alignment of the ISS 2nd loop PD array. Recall from yesterday afternoon, we did not make much progress in the alignment. This was due to the signals out of the PD array dropping for apparently no reason. After some intial investigation it was decided to re-convene this morning, this time with Rick helping out (as he has worked with the ISS PD arrays extensively).
Some notes from this morning's work:
This taken care of, the beam was then centered on the PD array enclosure input aperture using the first steering mirror (located on the -Y side of the table), and then the signals maximized (to the best we could achieve with a flashing IMC) using the second steering mirror (located on the +Y side of the table). This was iterated several times until we had a strong signal on all of the PDs and the array enclosure QPD, and the beam was centered on the entrance aperture of the array enclosure. This is more than sufficient for the in-air alignment; the PD signals will be maximized when the IMC is once again locked (after the corner station is pumped down).
Jason is correct, that the HWP installed on the PSL table is to make the IMC flash on the wrong polarization, which has lower finesse, so the output flashes should be easier to see. This is why the temporary HWP needs to be in the path after IM1, to undo this polarization change, before the beam goes to the input Faraday isolator.
WP7252:
During today's CDS meeting Rolf reported that moving the fast front-end computer's IRIG-B card away from slot-1 resolved timing issues on his test system. To try this out on a production system, this afternoon I moved h1susey's IRIG-B card.
Recall (alog 39361) that on 09nov2017 I had moved h1susey's OneStop from slot-2 to slot-5 as part of this investigation. Today I returned the OneStop back to slot-2, and moved the IRIG-B card from slot-1 to the newly vacated slot-5.
slot id | 7 | 6 | 5 | 4 | 3 | 2 | 1 |
before | empty | empty | OneStop | 5565 | Dolphin | empty | IRIG-B |
after | empty | empty | IRIG-B | 5565 | Dolphin | OneStop | empty |
It was a messy restart of h1susey. After taking it out of the Dolphin fabric and issuing the poweroff command, the OS got stuck trying to umount NFS after apparently disabling its network ports. I had to power down using the front panel button, knowing that this would most probably cause a Dolphin glitch. Sure enough, on restoration of power the EY dolphin fabric glitched, requiring a restart of models on h1seiey and h1iscey. EY is now back in operation.
Tagging DetChar, so it's on their record books that this change was made.
The upcoming front-end OS upgrade (Gentoo with 3.0.8 kernel) has a much cleaner startup/shutdown process that works with the OS instead of fighting with it. This should help those issues.
I also took the opportunity to move the eyws1 iMac workstation to EY. It is located on a cart parked by the computer racks.
Unfortunately there were two h1iopsusey blips this morning at 03:20 and 06:02 PST.
Today, Travis and I worked to closeout BSC 3 to finish out the set of chambers needing doors put on. We:
I attach a screenshot of the pitch transfer function during the Ring Heater cable rubbing. I also include illustrative drawings and pictures of the rubbing site. In words -- the ring heater cables (CBL7 and CBL 8 of D1001517), exiting the QUAD lower structure, should be sandwiched between the two inner face plates (aka "figure eights", D060462). On this ITM, it is not, and for the first time, it escaped far enough out of its designated path that it started to lightly interfere with the bottom of the main chain's UIM base plate (D060376). Attachments: First -- (from D0901346) A side view of the full solidworks assembly of the quad. The face plates are the long vertical blue things that extend the length of the lower structure. The two in the middle are the inner face plates. Second -- (from D1001838)An isolated view of the test-mass-side's inner face plate, with the fully assembled ring heater and cabling system. Third -- (from G1100850) Another view of the test-mass-side's inner face plate, with the fully assembled ring heater and cabling system. Fourth -- (from D0901346) A screenshot of the QUAD's solidworks eDrawing assembly, where I've hidden enough to show the ring heater cables, and made the face plates transparent. Naturally, the eDrawing is buggy, and the ring heater cables are displaced from where they're designed to be, and are actually interfering with the *reaction* chain's UIM base plate, but you get the point. Fifth -- a picture Betsy / Travis took of the offending cable rubbing against the *main* chain UIM base plate. Sixth -- (from D1001517) A screenshot of just the cable assembly to show what "CBL7" and "CBL8" are. Seventh -- A screenshot of the Pitch transfer function. Blue and Black are nominal, normal transfer functions. Red was while this rubbing was happening. As expected from the modes shapes of the middle-frequency pitch modes nominally at 1.33 Hz, 1.59 Hz, and 1.98 Hz, that had so clearly shifted, we knew that something was (wrong / rubbing) (in / around) the middle masses -- the PUM / UIM.