ams tracker hardware status (mechanics and cabling) divic rapin, unige ams splinter tracker, septidi...
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AMS tracker hardware status(mechanics and cabling)
Divic RAPIN, UniGe AMS splinter tracker , Septidi 7 Brumaire 217 (october 28, 2008)
• off-line operations• preparation for integration
Franck CadouxEric Perrin*Divic Rapin
Florian MasciocchiPhilippe BouvierJavier MesaMaarten WeberManfred Willenbrock*
With the help of S.Lucidi (Perugia) for paper work (QA)* Retirement approaching
Université de Genève
University of Geneva staff involved:
NIKHEF and NLR staff involved:Bart Verlaat, Erno …, Johannes Van Es, Aswin Pauw
Ladder repair (test with mobile station)
• Non working ladders were:– L15AP098 (read-out:600 oct:8 pwg:1 TDR:1B) Layer:8, slot:7M (---)
bad K cable recoverable repairing of cable failed Spare S-type cable was used – L12AJ019 (read-out:309 oct:3 pwg:1 TDR:3B) Layer:4, slot:6P (+-+) K
cable disconnected recoverable with front shell opening
K flight cable connector of L15AP098 DR. july 18, 2008
Pin 2 Guard ring
Line 5 (H1)
6 ohm 1.5 ohm
1.5 ohm
Pin 7 (H1)
• Test of K flight cable showed interruption on pin 7 of connector of TDR side.
• Surgery to access connections on patch panel for better diagnostic.
• Contact was re-established (by chance). Poor contact through the Airborne connector.
• Airborne connector faulty ?? Or cold soldering ???
• This problem occurred already with another cable.
Apparent repairing by resoldering pin 7, but failure showed again after reinstalling sleeve
Change cable (s-type)
Ladder L12AJ019 Layer:4 Col:6P (+X –Y +Z) octant:3 pwgrp:1 TDR:3B Read-out: 309 ?
Pictures taken may 8, 2007. After tests. Just before closing last shell
DSCN0356.JPG
DSCN0353.JPGConnection hidden during most of the time by supporting bars.Tests were OK
Fixation of connectors with Kapton tape
OK
U
Access by
outer side
only !
Front shells were opened
Special tools were designed to hold the scotch tape (with vacuum)
Example of new fixation on –X side
Operations on evaporators (cooling loops)
• Change (weld) new connectors
• Modify the pigtails to solve the interferences with LTOF
• High pressure and leak tests ( 200? bars)
• Mounting on external planes + checks
• Cleaning (this week)
• Mounting on inner tracker (to be done)
AMS TRACKER ADP Annex 1
Modification of the top evaporator to provide more clearances with the tracker cables
Fig. 1 below is showing the interference between one of the copper blocks of the top evaporator with the tracker cables in the vicinity of the Star Tracker support
Copper block before and afterthe modification on ladderPositions 10 M and 10P.
Work done by PhB/ EP 16/7
Incompatibilities between locations of LTOF patch panel and pigtails of the tracker lower cooling pipes and collision.
Need to modify the lower cooling loops by replacing the last pigtails by a simple S.
AMS TRACKER ADP Annexe 2
Modification of one evaporator loop to solve interference with Lower ToF (LToF)
6mm down
Twisting in this area
New connectors welding, pigtails suppression, tests
Bart Verlaat
Erno
Cleaning (this week) • Flush with CO2
• Rinse with IPA
• Flush with CO2Aswin Pauw NLR
Cleaning (this week)
Mount outer evaporators on planes + check support geometry
modificationsTwo types of fixation:• Plane only: on thermal bars + plane• Shared: brackets on conical flange + plane
Fixation on thermal bar (upper part on plane not shown)
Spring coupling
Thermal bridge
Screw securing: helicoils + glue
ChoTherm
Six damaged helicoils or threads were repaired
Riveting and gluing of the upper parts of fixations
Two pins to secure cable connectors
Five different sizes ! (clearance from 0 to 1 mm)
Trial assembly of the whole bracketery supporting the
evaporators. Design & fabrication of new
and missing brackets
• New brackets• Jigs to simulate the fixation of the lower part of brackets to conical flange • Check if it fits
Maarten Weber
… in order to avoid bad
surprises at final
integration..
Supporting brackets for evaporator connectors
• New loop connectors need a better fixation (magnetic force twice ~ 5 N )
Tracker crate balconies
Lower parts installed with controlled torques
ATS exists
Remaining off-line operations
(in clean room)
• Evaporators (cooling loops)- Cleaning (in progress)
- Outer planes- Terminate test and installation of bracketry (in progress)- Install connectors securing pins (plane 1 done)
- Inner Tracker- Install upper inner cooling loop- Glue and prolongate DS thermal sensor chain- Install evaporators supporting brackets on conical flange- Install thermocouples for TVT tests (locations to be defined)
Missing procurements
- Mylar patches on M10 nuts (ship to US)- Structural screws (NASA)- Shims for tracker feet. (clarify situation)
Cold Vacuum Case Installation
• No solutions are seen if we want no stress on feet during mission. (impossible to mount the feet under stress)
• If one accept stress on the feet during mission, mounting the feet with pumped VC can be considered.
Opinion :
Preparation of final integration
• Update of integration procedures (ATS, S. Lucidi, FC, EP, DR) taking into account what we have learned in pre-integration and the limitations imposed by the real vacuum case:
- Limitation of RAS rotation
- Field mapping / Need for special protection
- Cryogenic services to VC
- Final cabling