Displaying reports 75621-75640 of 76923.Go to page Start 3778 3779 3780 3781 3782 3783 3784 3785 3786 End
Reports until 14:19, Wednesday 07 September 2011
H2 DAQ
aidan.brooks@LIGO.ORG - posted 14:19, Wednesday 07 September 2011 (1355)
H2-TCS ITMY Ring Heater driver calibration of voltages and current
Steve O'Connor, Chris G. and I calibrated the ring heater temperature, voltages and current channels in the front-end code.

H2:TCS-ITMY_RING_HTR_SEG1_I_MON
H2:TCS-ITMY_RING_HTR_SEG2_I_MON
Ring Heater Current = 1.221E-2 mA/count (1V into ADC = 40mA = 3276.8 counts)
 & "deWhiten" filter = dewhitening by pole at 0.4Hz and zeros at 10Hz and 1kHz (+ gain = -1)
Filter file: /opt/rtcds/lho/h2/chans/H2TCSITMY.txt
 

H2:TCS-ITMY_RING_HTR_SEG1_V_MON
H2:TCS-ITMY_RING_HTR_SEG2_V_MON
Voltage over ring heater = 6.1035E-4 V/count (1V into ADC = 2V across Ring heater = 3276.8 counts)
  & "deWhiten" filter = dewhitening by pole at 0.4Hz and zeros at 10Hz and 1kHz  (+ gain = -1)


H2:TCS-ITMY_RING_HTR_SEG1_V_MON
H2:TCS-ITMY_RING_HTR_SEG2_V_MON
Local voltage across output from driver = 6.1035E-4 V/count (1V into ADC = 2V across Ring heater = 3276.8 counts)



H2 DAQ
david.barker@LIGO.ORG - posted 08:32, Wednesday 07 September 2011 (1354)
new H2 TCS ITMY model installed
Rolf installed a new h2tcsitmy model yesterday on h2tcsl0. He also installed a new MEDM screen, which I have linked to the sitemap.

To complete this installation, we need filter-module settings to perform the adc-counts to engineering units conversion, and the list of channels which should be written to frame.
H2 General
cheryl.vorvick@LIGO.ORG - posted 21:16, Tuesday 06 September 2011 (1353)
TCS Ring Heater SN001 was weighed and resistance was measured today.
The TCS ring heater shield / heating element assembly, SN001, was weighed and it's resistance measured today.  Results are as follows:

D100680-v4, SN001
224g
35.8 ohms

D100679-v4, SN001
228g
35.8 ohms

Cables and brackets will still need to be weighed.

- Cheryl, Chris Mueller
H2 General
jodi.fauver@LIGO.ORG - posted 18:20, Tuesday 06 September 2011 (1352)
BSC-6 ICC
The crew was split today.

Half of the crew worked on the dome. After the dome was lifted and the C-3 cover was removed, the crew started on the first checklist items: 1.)The conflat was removed 2.) The interior condition was documented and 3.) A particular area was investigated for contamination. 

The other half of the crew worked in and around the chamber. Viewports, camera, and illuminator were removed and preserved in a clean condition. The chamber interior was documented, pre-work wipe samples/FTIRs were taken, and the flooring was installed. Pre-work inspections, including the support tube surfaces, were conducted. Fibers were found on the support tubes. (No surprise there. That's 3 BSCs and 3 sets of support tubes with large fibers attached!)The fibers were photographed and then vacuumed off. The support tubes were wrapped in foil and C-3. Bellows protection was installed. Dust barriers were installed in both door nozzles to help protect the door/chamber flange area since both doors are still in place. That means brushing can get started tomorrow. GO TEAM!
X1 SUS
jeffrey.bartlett@LIGO.ORG - posted 17:24, Tuesday 06 September 2011 (1351)
Quad-4
Andres R. and Jeff B. installed Quad-4 on the mechanical test stand in the staging building. Final assemble and alignment will begin in the morning.       
X1 SUS
jeffrey.bartlett@LIGO.ORG - posted 17:18, Tuesday 06 September 2011 (1350)
Mate FMY to BSC/ISI
Today we mated FMY to the BSC/ISI. The fit between the test stand, inside the BSC/ISI, the Genie lift, and the Quad is very tight. Several times, we had to rest the Fold Mirror on the LSAT remove and reposition the Genie in order to complete the operation. We also encountered a fit issue between the unloaded Genie and the gusset plates on the test stand cross member. Once the Fold Mirror was positioned properly under the BSC/ISI, it installed with no problems.     
H2 SUS
jeffrey.garcia@LIGO.ORG - posted 16:44, Tuesday 06 September 2011 - last comment - 10:43, Thursday 08 September 2011(1345)
H2 ITMY Quad Vibration Absorber ON/OFF hammer tests
On Friday, Impulse response measurements were conducted using a Bruel and Kjaer (B&K) impact hammer and tri-axial accelerometer (also B&K) on the Quad  structure. The purpose of these investigations is to assess the effectiveness of the newly-installed Vibration Absorbers on the Sleeve of the QUAD structure. The Vibration Absorbers are arranged in a "spiral" arrangement around the frame of the sleeve structure of the Quad.  One VA is on each corner of the sleeve with the position heights incremented upwards around each corner - giving a "spiral" arrangement around the sleeve.

The accelerometer was positioned on the M0 chain side of the Quad on the cross brace of the Lower structure just above the Test Mass. It's X-axis was oriented along the beam path, the Y-axis crossing the beam path in the same horizontal plane, and the Z-axis vertically up through the Quad. The accelerometer's position did not change throughout each test.

Tap tests were conducted for three sub-structures of the Quad, with multiple spots selected within each sub-structure.  The three sub-structures are the Upper Structure (cage around M0/R0), the Lower Structure (cage surrounding everything below M0/R0), and the stiffening Sleeve Structure (structure surrounding the whole build) installed on August 19th. The Upper Structure had three tap test locations, the Lower Structure had four, and the Sleeve had five.  

The configuration for the BSC-ISI/QUAD system was:
BSC8 ISI - locked
H2 ITMY QUAD - unlocked, suspended with damping loops closed for both M0 and R0 chains.
Watchdogs did not trip during any of the tap tests.

Data was processed in real-time using the PULSE software provided with the B&K instruments. The PULSE software monitored for "double-hits" and for impact Force range. Data was then extracted after each measurement into .txt files that were imported and processed in Matlab. 

The VA OFF tests were conducted first. Three spots on the Upper Structure, four on the Lower, and five on the Sleeve were selected.  The VAs were then replaced to their previous locations, and the tap tests were repeated at the same locations for the VA ON tests.

The attached plots are Frequency response comparison plots of the Accelerometers in each degree of freedom (DoF) at each tap test location. The magnitude ((m/s^2)/N) of the accelerometer response is plotted against the frequency range (0.5-800Hz).

Each plot has a trace in dashed-red displaying the data from the tests with the VAs OFF and a trace in solid blue of the data from the tests with the VAs ON. Each plot is of the same tap test location for ON and OFF.

The pdf files are grouped by sub-structure (upper, lower, sleeve) and display the responses for all locations (in separate plots) on that sub-structure for a specific DoF. I have only attached the X and Y DoFs, but the Z DoF plots will be in the SVN.

Data collection parameters were:  0-800Hz response with a 0.5Hz resolution.  

----------------------
Tap Test Locations
*for location reference, when facing the Quad from the M0 chain, the "Beam Tube side" is on the right and the "Clean Room side" is on the left.*

Upper Structure:
location 1 - M0 side tapping from the Beam Tube Side across to the Clean Room side.
location 2 - R0 side tapping from Clean Room side across to the Beam Tube side.
location 3 - Beam Tube side - diagonal cross-brace in a downward direction.

Lower Structure:
location 1 - M0 bottom - from Beam Tube side across to the Clean Room side.
location 2 - R0 bottom - from Clean Room side across to the Beam Tube side.
location 3 - R0 side tapping on cross-brace just above the PUM from Clean Room to Beam Tube side
location 4 - M0 side tapping on cross-brace just above the PUM from Beam Tube to the Clean room side

Sleeve Structure:
location 1 - M0 bottom right corner of sleeve on the Beam Tube side
location 2 - R0 bottom right corner of sleeve on the Clean Room side
location 3 - M0 top left corner of sleeve on Clean room side
location 4 - R0 top right corner of sleeve on Clean room side
location 5 - diagonal cross brace on the Beam Tube side

Images attached to this report
Non-image files attached to this report
Comments related to this report
jeffrey.garcia@LIGO.ORG - 20:01, Wednesday 07 September 2011 (1362)
2 Supplemental Items:
--------

1.) Attached is a picture of the location of the accelerometer used for the tests.  The aLog automatically rotated the photo 90 deg counter-clockwise, but one can see the accelerometer on the cross-brace just above the test mass and slightly off center.

2.) The SUS SVN has been updated with the data and plots of these measurements as follows:

Data Location:
'~/sus/trunk/QUAD/H2/ITMY/Common/Vibration_Absorber_tap_tests/Data/'

where the file names denote the Vibration Absorber ON/OFF configuration, which sub-structure on the Quad, and the location of the measurement.

"VA_tap_test_data_VA_*OFF/ON*_*sub-struct*_*location*_110902.txt"

Plots are located in:
'~/sus/trunk/QUAD/H2/ITMY/Common/Vibration_Absorber_tap_tests/Plots/'
jeffrey.kissel@LIGO.ORG - 10:43, Thursday 08 September 2011 (1364)
Also, it should be noted that these tests were performed with the H2 ISI ITMY (BSC-ISI) *locked* for these measurements. The suspicion is that the resonant modes seen between ~10 and 50 Hz are modes of the support structure coupling through the locked BSC-ISI. We'll need further B&K transfer function + ST2 ISI transfer function measurements with the BSC-ISI unlocked in order to confirm; the hope is to obtain these after H2 SUS ITMY (QUAD)'s lower half is returned.
LHO FMCS
kyle.ryan@LIGO.ORG - posted 16:26, Tuesday 06 September 2011 (1348)
Prepping VE configuration for squeezer
Burped GV14 and GV15 gate annulus volumes into aux. pump cart*Opened GV14 and GV15*Switched YBM pumping from MTP to IP5*Burped GV1 and GV5 gate annulus volumes into aux. pump cart*Soft-closed GV6*Opened GV1 and GV5*Pumping BSC1 annulus with aux. pump cart

Will continue tomorrow
H2 General
jeffrey.garcia@LIGO.ORG - posted 16:05, Tuesday 06 September 2011 (1347)
Ops Day Summary
Deliveries/Visitors:

9:10 - Unifirst delivery

9:45 - Patrick changing dust monitors in the Diode Room

10:00 - Patrick and Michael R. to diode room

10:45 - Platt electric for Richard M.

10:55 - APS visitor for Richard M.

11:15 - Paradise water delivery

12:30 - Platt electric for Richard M.

At around 4:00, the Squeezers are ready to transition the LVEA to "Laser Hazard", pending the completion of the IAS crew.
------------

Other Activities throughout the day:

Mating of FMY onto the BSC-ISI in the LVEA
Ken working on the PSL
IAS crew making measurements on the H2 ITMY Quad build
SEI crew prepping ISI for re-balancing
Sno-Valley on-site
Portable Toilets serviced
H2 SUS
jeffrey.kissel@LIGO.ORG - posted 14:55, Tuesday 06 September 2011 (1346)
H2 SUS ITMY -- Post-Mate TF Comparison
J. Garcia, J. Kissel

As a supplement to Garcia's analysis of the H2 SUS ITMY (QUAD) main chain and reaction chain transfer functions taken on 110825, after that QUAD had been suspended post-mate I attach a "pre-mate and post-mate" comparison for both chains. The Reaction Chain (R0 -- see 110825r0alltfs.pdf) shows a significant increase in stiffness in pitch (with the first mode at 0.58 Hz simply disappearing), along with other degrees of freedom less effected but still not passable. Although several things changed between the measurements (listed below), my suspicion is that the new cable routing -- the "as designed" cable routing -- is what's causing the badness. The hope is to get this diagnosed *before* we must remove the lower half for fibering, but is not a "fix before detaching lower half or die" as we still have to lace up the ESD cables, and do (at least one more) iteration(s) of cable arranging to find an ideal cable route that has minimal effect on the suspension dynamics. We can do preliminary lacing while the reaction chain is split from the main chain (so as to not do so with a delicate fibered main chain in the way), and route the remainder up the top mass after the re-mate.

The differences between the two measurements are
- 2011-08-12 (ORANGE)

- QUAD mounted to Solid Stack on Mechanical Test Stand (MTS) 1
- No stiffening elements are in place
- Satellite amplifiers still under "old" design (as per D0901284-v1)
- Cable Routing as shown in entry 1230, where the R0 L1/UIM and R0 L2/PUM cables, in their jump between the R0 TOP mass to CAGE, are clamped well at R0 TOP mass, but temporarily shoved in cubby holes at the corner of the cage

- 2011-08-25 (BLACK)

- QUAD mounted to BSC-ISI on MTS 2
- All stiffening elements are in place, including stiffening sleeve, lower structure side panels, and upper structure cross-braces.
- Satellite amplifiers have been modded, as per aLOG entry 1257, and described in G1100856
- Cable routing as shown .pdf attachement "cablerouting110825.pdf", where the R0 L1/UIM and R0 L2/PUM cables, are now routed "as designed," using the c-clamp cable bracket on the now-installed cross-brace.


Things to keep in mind while looking at the three traces in the R0 comparison:
- The model is a main chain model, it's merely to guide the eye
- The ORANGE curve represents an "already approved" cabled up reaction chain, a la entry 1217, and is therefore the nominal reference

The reason why I suspect cabling:
(1) Adding stiffening to the structure/cage should not affect the dynamics of the suspended portion of the QUAD. The only way I could envision this having an effect is if any protruding elements of the suspended portion (read CABLES) are [interfering with/rubbing against] the newly installed structure pieces. This would be most likely at the L2 PUM stage, where the tentacles of the quadrapuss OSEM cables have to loop around the back of the PUM, where there is now a cross-brace of the stiffening sleeve.
(2) The modified satellite amplifiers should have an overall, DC, (160k - 121k)/ 160k = 20% decrease in sensor gain, but otherwise no change in functionality. Given that the calibration on these measurements is at best 50%, we should see minimal change if at all. Further, and change seen would be on all degrees of freedom. They change definitely would not affect the dynamics of the suspension as seen.
(3) As with the stiffening elements, whether the QUAD is mounted to the Solid Stack or the BSC-ISI should make no difference to the suspended dynamics.
(4) The cable routing from the R0 TOP to the CAGE is significantly different. The new routing is more "aligned" to pitch -- the most different degree of freedom.

Remember, the cable philosophy:
When jumping between suspended isolation stages, 
	(1) the clamping on either side of the connection should be as close to the jump as possible
	(2) the jump should be made with as few cables as possible
	(3) the length of cable between the jump should be a loose S shape, and without touching anything around it (which is why (1) is important)
        (4) the distance of the jump (from clamp point to clamp point) should be minimized
These points are only necessary between stage jumps. Cable routing on/within a mechanically connect (but not suspended) stage doesn't matter, and in fact should be tightly contained against the stage, such as to not interfere with other stages.

So, we should try the following:
- "Splitting up" the L1/UIM and L2/PUM cables, i.e. clamp them in separate locations (Bundles of cables are stiffer than single cables)
- Re-orienting the R0 TOP launching point such that the cables come out of the clamp parallel to the Transverse axis, as they were on the Solid Stack (I think this may relieve some of the "pitch pressure" if you will)
- Finding some way to clamp the cables on the *inside* of the cross brace, rather than on the outside. This would require some ingenuity, use of a different clamp, or a re-design of the current clamp. ()

Unfortunately, I think we got lucky with Betsy's awesome first attempt at this when the QUAD was mounted to the Solid Stack. I'm sure we'll need to iterate on some combination of all three of the above ideas, and add some new ones before the dynamics are restored. Not to mention we have to add a whole 'nother lacing cable -- the ESD extension cable (see blue trace in T1100327-v2).


Non-image files attached to this report
X1 SEI
corey.gray@LIGO.ORG - posted 08:49, Tuesday 06 September 2011 (1330)
BSC-ISI Assembly Status

(Corey, Jim)

This entry covers ISI assembly work from last week.

BSCISI#2 (BSC6)

L4C Replaced

H1 L4C s/n 34 (non-vacuum-ready) was replaced with s/n 76 (leak-checked & vacuum ready).  This was a horizontal at Corner1.  This L4C will need to be tested to confirm it is good for end use.

BSCISI#3

Both Types of Springs Installed & Loaded

Installed all Springs and loaded them.  Here are the Flexure S/N's:

Corner1

Corner2

Corner3

A note on the Spring Pre-Loading Tool (namely with the Stage0-1 portion of it).  A short & long Pusher Bolt is used to push the Spring to it's loaded position.  As these Bolts are screwed down, the head of these Pusher Bolts get close to the heads of some 1/4-20 bolts used to keep these Pushers in place.  So one has to be careful not to jam a wrench into these 1/4-20's.  Although one would hope it would be hard and obvious, it's conceivable one could break the heads of these 1/4-20 bolts with their wrench when they are Pushing down on the spring.  Jim mentioned the use of hex head 1/4-20's could be used here (offering a lower profile/less interference with these bolts).  Photos of this issue are attached.

Vertical GS13's Installed

Once the Springs were installed, Vert GS13's  were put on assembly via the forklift.  (These ones have bad Pods [wrong screws used for base flange] and need to eventually be replaced before installed in BSC---SO THEY ARE TEMPORARY!)

Locker Shims Used

The Lockers were installed last week.  Here are the current thicknesses of the shims used to make the Lockers operational:

Corner1

Corner2

Corner3

For BSCISI#3, now at a point where we are waiting for remaining parts (namely Capacitive Position Sensors, Trillium seismometers, cabling, etc.).

Images attached to this report
H2 DAQ
david.barker@LIGO.ORG - posted 11:11, Monday 05 September 2011 (1344)
testing new mx_stream on H2 DAQ
Alex has installed a new multi-threaded version of mx_stream on the H2 DAQ in the h2dc0 target directory. This is a  multi-threaded version which will hopefully fix the problem of all front end DAQ data streams being marked invalid (and consequently zeroed by the frame writer) when one front end stops streaming its data.

Please tell me of any future occurrences of all front end data being marked 0xbad when a front end model is restarted, thanks.
Logbook Admin General
david.barker@LIGO.ORG - posted 11:00, Monday 05 September 2011 (1343)
test of unclosed HTML tags

	test that small font html tag with no closure tag makes all preceding entries small
LHO FMCS
kyle.ryan@LIGO.ORG - posted 20:16, Friday 02 September 2011 (1342)
Pumping XBM
Begin pumping XBM, BSC7 and BSC8 annulus volumes
LHO FMCS
kyle.ryan@LIGO.ORG - posted 20:14, Friday 02 September 2011 (1341)
Connected cables to PT170 and PT180 gauge pairs
PT180B not working -> fuse in rack is OK -> will fix later
LHO FMCS
kyle.ryan@LIGO.ORG - posted 20:11, Friday 02 September 2011 (1340)
Hot QDP80 at X-mid

QDP80 at X-mid started running hot as of last week sometime? -> Coincides in time with switching over to auxilary chilled water circulating pump.  Particulate strainer in TMS valve is probably clogged with rust/scale introduced from valving-in long-idle non-circulating water circuit. -> Switched X-mid pumping to IP10 and shut down MTP and QDP80. Will inspect TMS strainer etc. after it has cooled down.   Also, connected iLIGO cables to PT310 gauge pair as an interim means of monitoring pressure until cables can be shortend/routed permanately etc..
H2 General
michael.rodruck@LIGO.ORG - posted 16:25, Friday 02 September 2011 (1339)
Ops Day Summary
H2 INS
greg.grabeel@LIGO.ORG - posted 16:12, Friday 02 September 2011 (1338)
HEPI LVEA

The HEPI system has been in a flushing loop for several days and will continue to do so over the weekend. No visible leaks were seen anywhere along the piping and valves. The system has been holding steady at 72 psi while the temperature of the HEPI fluid has been 23.8 c with an ambient air temperature of 21.6 c.

Images attached to this report
H2 SEI
brian.lantz@LIGO.ORG - posted 09:29, Friday 02 September 2011 (1337)
changes to the 2 stage isi master and h2isiitmy diagrams
Brian Lantz made a set of changes to the watchdog for the bsc-isi system, in concert with Vincent.
following are the notes on the updates.
----
changes to the master model

for ST1
 - added input 25 'Payload_watchdog'
 - put 'Payload_watchdog as input 6 to ISIWATCHDOG inline c (replaced a ground)
 
 - changed the inline c code to be ISIWATCHDOG function in the c-code ISIWD.c
  (was BSCISIWATCHDOG in BSCISI.c) 
  
 for ST2
  
  reorder the inputs to the ST2 watchdog
     _now_     _was_
  1   CPS      CPS
  2   GS13     GS13
  3  ST1_WD    ACT
  4   BIO      BIO
  5   ACT      ST1 WD
  6   payload  PAYLOADWD_IN  cdsEpicsIn
  7   reset    reset
  
  
  in the BIO
  changed the bits watched by the coil driver, per the Ben Abbott 
  BSV-ISIv5, 
  D0901301-V5 and DCN E1100821
  
  changed the ADD to a 6 input NAND,
  added 2 new epics vars, BIO_IN_ST1_CD_TRIP and BIO_IN_ST2_CD_TRIP.
  these should be 0 if the coil drives are OK, and 1 if the coil drives are tripped.
  
  %% 
  change the h2isiitmy model
  1) back up old model:
  
  userapps/release/isi/h2/models$ cp h2isiitmy.mdl h2isiitmy_preSept1_2011.mdl

In The ITMY model
- new master model appears correctly
- route the Digital Outs via a goto/from tag pair to clean up screen where the payload block will go
- send the 1's to the ISC inputs, and the 65535s to the compter test points.

- added new block for the payload, copy from S1:ISI-ITMX model
- the SUS WD vars are:
FMY-
 H2:SUS-FMY_M1_WDMON_STATE

ITMY-
 H2:SUS-ITMY_M0R0_WDMON_STATE


From: Jeff Kissel 
Date: August 30, 2011 10:29:51 AM PDT
To: Brian Lantz 
Cc: Vincent Lhuillier , Fabrice Matichard , Jeff Garcia 
Subject: Re: BSC watchdog update

Hey Brian,
Sounds good to me. Jeff Garcia can be around if you need anything from the suspensions side. The FM does not have a dedicated watchdog epics variable for you, but for now you can use
H2:SUS-FMY_M1_WDMON_STATE
which is 0 if OK, non-zero if BAD (exactly like what's in the seismic WDMON block).

If we find that the "only watch the top stage" functionality is good in general for any suspension (besides the QUAD, which has the afore mentioned H2:SUS-ITMY_M0R0_WDMON_STATE), then we won't need to add in any specially dedicated channels for you, as there will be a similar variable for every other suspension.

I'll be in my office if you need me!

Cheers,
Jeff Kissel


update the MEDM screen for the Payload mon

userapps/release/isi/h2/medm/h2isiitmy$ cp ../../../s1/medm/s1isiitmx/S1ISI_CUST_ITMX_PAYLOADMON.adl H2ISI_CUST_ITMY_PAYLOADMON.adl

$ svn add H2ISI_CUST_ITMY_PAYLOADMON.adl 

	name="/opt/rtcds/lho/h2/userapps/release/isi/h2/medm/h2isiitmy/H2ISI_CUST_ITMY_PAYLOADMON.adl"


$ perl -pi -w -e 's/S1:ISI-ITMX/H2:ISI-ITMY/g;' *PAYLOADMON.adl


-- update the watchdog screen
userapps/release/isi/h2/medm/h2isiitmy$ cp ../../../s1/medm/s1isiitmx/S1ISI_CUST_ITMX_WATCHDOG.adl H2ISI_CUST_ITMY_WATCHDOG.adl

change the file name at the top of the file to:
	name="/opt/rtcds/lho/h2/userapps/release/isi/h2/medm/h2isiitmy/H2ISI_CUST_ITMY_WATCHDOG.adl"
	
change the epics vars - 	
userapps/release/isi/h2/medm/h2isiitmy$ perl -pi -w -e 's/S1:ISI-ITMX/H2:ISI-ITMY/g;' *WATCHDOG.adl

change the 2 related displays to:
		name="/opt/rtcds/lho/h2/userapps/release/isi/h2/medm/h2isiitmy/H2ISI_CUST_ITMY_PAYLOADMON.adl"
		
$ perl -pi -w -e 's/S1:ISI-ITMX/H2:ISI-ITMY/g;' *WATCHDOG.adl

fix the calls from the BSCISItool
$ perl -pi -w -e 's/s1isiitmx/h2isiitmy/g;' *WATCHDOG.adl

fix the paths and names of related displays
$ perl -pi -w -e 's/stn/s1/lho/h2/g;' *WATCHDOG.adl
$ perl -pi -w -e 's/isi/s1/isi/h2/g;' *WATCHDOG.adl
$ perl -pi -w -e 's/S1ISI_CUST_ITMX/H2ISI_CUST_ITMY/g;' *WATCHDOG.adl
		
X1 SUS
jeffrey.bartlett@LIGO.ORG - posted 17:45, Thursday 01 September 2011 (1335)
Move Fold Mirror Y to LVEA
Team SUS - Betsy B. Travis S., Andres R., and Jeff B.

Today team SUS removed the Fold Mirror (FMY) from the mechanical test stand in the staging building and transported it to the LVEA. It was craned over the beam tube it is now sitting just outside the BSC/ISI cleanroom. Tomorrow we plan to weigh it and mate it to the BSC/ISI.  
Images attached to this report
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