The ISI was strongly excited on march 1 at its first rigid body mode (1.24Hz). Since L4Cs and GS13s have their resonance at 1Hz and T240 are fragile instruments, they may have been damaged during the intense shaking. The attached calibrated spectra shows that all geophones seem to be working properly. Spectra were measured with the ISI locked and unloaded (lower stages of the QUAD removed). Then motions measured by stage 1 (L4C, T240) and stage 2 (GS13) geophones are very close. CPSs seem to work too.
Today, we pulled 2 of the FirstContact(FC) sheets we sprayed on yesterday. Specifically, we pulled and inspected ITMy-HR and ITMY-AR. While it appears that some of the particulate generated from the fiber breakage and subsequent chamber removal activities were removed from our cleaning, we still saw particulate on the surface. It is on the order of what was observed when we left the ITMy and closed the chamber in Feb. We reapplied the FC to these 2 surfaces and proceeded to remove it from the lower structure. Using the ergo arm, Gerardo, Calum and I parked the ITMy in a v-block on a small optics table in the LVEA fiber welding cleanroom. We will continue to prep the optic and suspension for a wire hang. Pictures of the FC spray-on application are at: https://ligoimages.mit.edu/?c=1019 Note, this was a first article spray application - more secure and fool=proof fixturing will replace all of the foiling shown in the pictures if we proceed with the spray-on technique.
Attached are plots of dust counts > .5 microns. I have also included plots of the modes of the dust monitors that were disconnected to set the audible alarms. These show the approximate times when this took place.
Jim, Eric, Corey, Hugo
We recently received 5 production-GS13s from LLO: 3 verticals (Pods #: 30, 14, 88) and 2 Horizontals (Pods #: 93, 24). They are intended for HAM-ISI Unit #4.
We huddl-tested them before installation. One of them (Horizontal, pod #24) features the behaviour we have observed on GS13s with whether a broken flexure or a stuck mass. We tried tilting the instrument back and forth to unlock the mass. We could feel the mass moving. The ASD measured after tilting the instrument is the same as before.
Greg, Hugo,
Pod #24 was opened. The flexures were checked. Nothing abnormal was noticed. The instrument's leveling was quickly perfected and the pod was closed.
Attached power spectra shows that the instrument is still not working. It also shows that the rough leveling of the test bench is not the cause of this malfuctionning.
The audible alarms have been set on the following dust monitors: LVEA location 4 (clean room over test stand area): 20 raw counts @ .3 micron, 20 raw counts @ .5 micron LVEA location 15 (clean room over BSC 8): 20 raw counts @ .3 micron, 20 raw counts @ .5 micron LAB location 1 (OSB optics lab): 2000 raw counts @ .3 micron, 800 raw counts @ .5 micron LAB location 3 (OSB bake oven room): 2000 raw counts @ .3 micron, 800 raw counts @ .5 micron At the current sampling period of 1 minute, these raw counts should be multiplied by 10 to get particles per cubic foot. These alarm settings correspond to the current major alarm values for the alarm handler in the control room.
Dave B., Jeff G. The H2 FMX Simulink model was modified today to clean up some compiling errors and have a working FMX model running on "h2susb78". The model from FMY was used for FMX, which had not been updated with the latest BIO parts. There were several ADC and DAC channels out of order for the existing FMX model, but they have all been reconciled with the latest SUS control wiring diagram (D1001725-v9). The changes have been committed to the SVN under: '/opt/rtcds/lho/h2/userapps/trunk/sus/h2/models/h2susfmx.mdl' The new model was compiled and installed on the Front End this afternoon.
J. Garcia, J. Kissel, B. Shapiro After unlocking both the QUAD and the ISI, here are the latest results from H2 SUS ETMY. In summary, the chains look good and match other equivalent chains reasonably well, save the details below. My only concern is - There seems to be cross-coupling, most notably in the M0 Transverse direction (but present in other degrees of freedom *and in both chains*), between T/R at 1.25 Hz, and T/R/P 1.6 Hz. Other things that are not worthy: - The upper two Vertical mode frequencies are consistently higher than ITMY by ~2% (for main chain, same SUS but with metal erm for reaction chain). BUT, this would mean an equivalent increase in lower blade stiffness of sqrt(2%) = 0.04% -- by which I'm not alarmed, merely interested, since almost all other instances of SUS project wide have had *remarkably* consistent vertical modes. - Again focusing on the vertical TF -- Brett identified that we had accidentally left the UIM horizontal center of mass parameter, h1, at 0.005 m instead of the nominal production value of 0.000 m for the main chain, monolithic, 'fiber', parameter set. This offset, when present, (among other things, most notably) creates a cross-coupling of Pitch to the Vertical TF @ 2.76Hz. I've corrected this in the production model parameter set. Further, as you'll see in the attached, ITMY has some of this offset, where ETMY does not (good!). ------------ For persepective, one should probably start with allquads_120315_H2SUSETMY_ALL_TFs.pdf Here, I compare 2 chains, 4 measurements of monolithic main-chains, and 3 measurements of equivalent reaction chains. Main Chain H2 SUS ITMY 2011-12-02 -- Pre-cartridge install, Floating ISI, After IAS Adjustments, Stiffening Elements + Vibration Absorbers in Place, L1&L2 Aligned H2 SUS ITMY 2012-02-16 -- Post-cartridge install, Pre-ISI-Shakedown-Fiber-Failure, Floating ISI H2 SUS ETMY 2012-02-14 -- Pre-cartridge install, after major intra-chain rubbing was relieved H2 SUS ETMY 2012-03-14 -- Pre-cartridge install, after further UIM flag rubbing relieved, stiffening elements installed, etc (only thing missing is VA, which shouldn't effect anything). A quick scan through these TFs show that, for the most part, the most recent ETMY measurement matches the best ITMY measurement. In fact, comparing CYAN with MAGENTA, shows that the most recent round of UIM flag adjustment has greatly cleaned up all DOFs measurements. The only flaws visible are those mentioned above: - Cross-coupling, most notably in the M0 Transverse direction between T/R at 1.25 Hz, and T/R/P 1.6 Hz. - Slightly higher Vertical stiffness. Reaction Chain QUAD04 2011-11-22 -- Phase 1 approved measurement of H2 SUS ETMY, with metal ERM (on a solid stack) QUAD03 2012-01-24 -- Phase 1 approved measurment, with metal ERM (on solid stack) H2 SUS ETMY 2012-02-14 -- Pre-cartridge install, after major intra-chain rubbing was relieved H2 SUS ETMY 2012-03-15 -- Pre-cartridge install, after further UIM flag rubbing relieved, stiffening elements installed, etc (only thing missing is VA, which shouldn't effect anything). Here, in the most recent ETMY measurement, the reaction chain looks OK at first glance, but upon closer investigation shows the same 1.25Hz and 1.6Hz modes as the main chain, and the mid-frequency band just looks kinda noisier (though not as bad as 2012-02-14). -------------- The ALL_ZOOMED_TFs.pdf plot just shows a tighter X-axis for a better look at the details, and the first two attachments show a lot more information (cross-coupling, plus OSEM basis) on the CYAN measurements. Though it's difficult to blame a particular thing (*sigh* isn't that always the case?), my gut tells me there's still something rubbing between the chains. I know we've been having trouble with UIM flags... Also it's difficult to imagine a scenario where Transverse couples to Pitch... We'll keep thinking.
2012-03-14 and 2012-03-15 data shown in the above plots were taken by the following Schroeder Phased Matlab script: M0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGM0/Scripts/collectTF_20120208_H2SUSETMY_allDoFs_0p01to50Hz.m R0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGR0/Scripts/collectTF_20120207_H2SUSETMY_R0_0p01to50Hz_AllDOFs.m which save the data to the following .mat files: M0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGM0/Data/2012-03-14_H2SUSETMY_M0_0p01to50Hz_allDOFs_tf.mat R0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGR0/Data/2012-03-15_H2SUSETMY_R0_0p01to50Hz_allDOFs_tf.mat These were individually processed and plotted with ${SusSVN}/sus/trunk/QUAD/Common/MatlabTools/plotquad_matlabtfs.m (i.e. the script that makes the YYYY-MM-DD_[IFO]SUS[OPTIC]_[M0/R0]_ALL_TFs.pdfs) which saved the processed/analyzed data and plots in a standardized format to M0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGM0/Results/2012-03-14_H2SUSETMY_M0_MATTF.mat R0: ${SusSVN}/sus/trunk/QUAD/H2/ETMY/SAGR0/Results/2012-03-15_H2SUSETMY_R0_MATTF.mat which where then added to the list off all Matlab/DTT measurements, and compared by ${SusSVN}/sus/trunk/QUAD/Common/MatlabTools/plotallquad_dtttfs.m (i.e. the script that makes the allquads_YYYY-MM-DD_[IFO]SUS[OPTIC]_ALL_TFs.pdfs)
Diagonalization measurements were run on the H2 ETMY M0 & R0 top masses yesterday. Results are attached. The results show ideal isolation for the two DoFs on both masses. Each DoF on both masses is at least 20dB isolated from the other OSEMs, which is well above tolerance. M0 Yaw: 25ct amplitude at 1.3Hz 21dB isolation M0 Vert: 1000ct amp. at 2.2Hz 25dB isolation R0 Yaw: 25ct amplitude at 1.3Hz 24dB isolation R0 Vert: 1000ct amp. at 2.2Hz 23dB isolation
Yesterday, Mark L. and Chris spent some serious time in chamber doing the final clean-up inside BSC8 so that the door could go back on ASAP. The interior of the ACB was wiped down with a dry wipe to collect the glass dust at the lips so that it could be easily vacuumed up. During this process, one additional free range washer was found on the lower shelf. The two central planks of the BSC flooring were removed from the chamber and set aside in the staging cleanroom. The remaining planks on the east side of the chamber were stacked on top of the west side flooring so that the chamber floor could be inspected, vacuumed, and wiped down. There was very little visible debris on the east side of the chamber floor or rim. Next, the east side flooring was wiped down and re-installed so that the planks from the west side could be stacked up. The west side of the chamber floor was inspected, vacuumed, and wiped down. As expected, the west side of the chamber floor and the rim had numerous glass shards as well as dust (likely from glass). After wipe down, the west side flooring was returned to its starting position. Flooring hardware was installed around the perimeter. The central planks were wiped down and returned to position along with the accompanying hardware. The GV1 nozzle, the nozzle to GV3 and the Y-beam manifold as far as the first joint were vacuumed and wiped down.C-3 covers were removed from both structures (Quad Upper Structure and FM)so that they could be inspected. Thomas came in to swing the ACB back into its usual position. Some particulate, most likely glass, was found on the metal masses of the FM and carefully vacuumed off. Today, Mark and Chris completed the work in BSC8. A clean step-stool was placed into the chamber so that the upper parts of both structures could be given a close inspection: nothing distressing was found there. However, inspection of the support tube bellows revealed glass shards in the C-4 bellows.The shards were vacuumed up. Five witness plates were placed: 1. Bottom of GV1 nozzle close to septum; 2. Bottom of bellows convolutions in GV3 nozzle; 3. Bottom of bellows convolutions in Y-beam manifold; 4. BSC flooring/ACB face as landmark (approximately parallel with quad optic face);and 5. Center of BSC flooring (approximately center of space between the quad and FM, which seems to be a "dirty" spot). O-ring protection was removed. Then, o-rings were partially removed (lower half)and closely inspected for any glass debris. The o-rings looked good so they were wiped down and re-installed. The chamber door was vacuumed, wiped down, and then, re-installed. This concludes the physical clean-up of the fiber break at BSC8.
Thomas, Mark (Apollo), Caleb (Apollo), Chris (Apollo) The Arm Cavity Baffle in BSC8 is returned to its suspended position, the balance seemed good. I had double checked the crevices and the hardware to make sure that we didn't leave extraneous hardware laying on the baffle. During the course of repositioning the assembly, we could only find 3/4 of the 1/4-20 SHCS on a tray outside of the chamber but we had a spare bolt of the same size that came from removing some of the swingback tooling (class A).
Conlog is running again after being stopped yesterday afternoon for code changes. It was restarted a number of times since then. The channel list has changed. Currently 20,208 channels are monitored, 4,113 channels are unmonitored.
Some remaining bugs now necessitate further work.
Attached are plots of dust counts > .5 microns.
Praxair delivery
https://ligoimages.mit.edu/?r=18431 See entry 2426
B. Bland, J. Garcia, J. Kissel, T. Sadecki After the ISI shakedown, and lamenting the loss of H2 SUS ITMY, we found that H2 SUS FMY seemed to have survived according to first visual inspections, but OSEM signals / alignment looked pretty bad on the digital side. The last time FMY's TOP to TOP TFs had been measured (see aLOG 2237), it was identified that there was some rubbing, but the source was unclear. After the initial inspection, (and a couple of measurement tries by both Jeff and I), we identified severe badness in these TFs. Travis, yesterday, then worked some magic -- but now, as is evident from an "after" measurement -- we're back to the rubbing that was seen before the ISI badness. Attached are plots showing the story. 2012-01-09 -- Approved post-cartridge, in-air data [[but was taken before EQ stops were adjusted to 0.75 nominal distance]] 2012-02-15 -- At vacuum, first sign of rubbing [[two differences -- in-air vs. in-vacuum, and EQ stop placement]]. 2012-03-13 -- post ISI badness, in-air TF, crazy bad rubbing (later identified to be TOP/M1 vertical blade spring / mass stops that may have rattled down during the Shakedown.) 2012-03-14 -- Post-Travis fix of TOP EQ stops: back to black. The data shows: - Indeed FMY has survived the Shakedown. *phew*! - Because Cyan lines up identically with Black, I surmise that there's no change to whatever mechanic rubbing that was caused by bringing all the EQ stops in to the nominal 0.75 +/- 0.25 mm We've elected (i.e. Landry made the call) to go for close up of doors given this data. So, when we go back in the chamber to restore the repaired, wire suspended, ITMY, we'll attack FMY with more rigor.
2012-03-13 and 2012-03-14 data shown in the plots were taken with the following DTT .xmls: ${SusSVN}/sus/trunk/BSFM/H2/FMY/SAGM1/Data/ 2012-03-13_1342_H2SUSFMY_M1_L_WhiteNoise.xml 2012-03-13_1342_H2SUSFMY_M1_P_WhiteNoise.xml 2012-03-13_1342_H2SUSFMY_M1_R_WhiteNoise.xml 2012-03-13_1342_H2SUSFMY_M1_T_WhiteNoise.xml 2012-03-13_1342_H2SUSFMY_M1_V_WhiteNoise.xml 2012-03-13_1342_H2SUSFMY_M1_Y_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_L_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_P_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_R_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_T_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_V_WhiteNoise.xml 2012-03-14_1416_H2SUSFMY_M1_Y_WhiteNoise.xml Exported as 2012-03-13_1342_H2SUSFMY_M1_L_WhiteNoise_tf.txt 2012-03-13_1342_H2SUSFMY_M1_P_WhiteNoise_tf.txt 2012-03-13_1342_H2SUSFMY_M1_R_WhiteNoise_tf.txt 2012-03-13_1342_H2SUSFMY_M1_T_WhiteNoise_tf.txt 2012-03-13_1342_H2SUSFMY_M1_V_WhiteNoise_tf.txt 2012-03-13_1342_H2SUSFMY_M1_Y_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_L_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_P_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_R_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_T_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_V_WhiteNoise_tf.txt 2012-03-14_1416_H2SUSFMY_M1_Y_WhiteNoise_tf.txt Initially processed by ${SusSVN}/sus/trunk/BSFM/Common/MatlabTools/plotBSFM_dtttfs.m Which saved the data into the standard .mat file format, ${SusSVN}/sus/trunk/BSFM/H2/FMY/SAGM1/Results/ 2012-03-13_1342_H2SUSFMY_M1.mat 2012-03-14_1416_H2SUSFMY_M1.mat Which were then used to produce the above entry's attachment, using ${SusSVN}/sus/trunk/BSFM/Common/MatlabTools/plotallbsfm_tfs.m
Jim and I installed vented hardware into the holes we tapped for the ACB work. So no more dropping chips during strong HEPI motion. We did not bore-scope the holes.
At Mike's request, Bubba and I scopped the holes. Here is the url: https://ligoimages.mit.edu/?r=18431 to the 5 minute 32 mByte video file for your review. We saw some things in the threads of some of the holes and some bits up above the threads so it is conceivable that there may have been other chips that were shaken out on March 2. It did not appear that any of the remaining bits were loose as we did not dislodge any with the probe although we did not really try to do that. Certainly any bits now remaining will be trapped by the installation of the vented bolts.