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AMS-02AMS-02Integration & Test Integration & Test

Plans & StatusPlans & Status

Ken Bollweg/NASAJohn Heilig/JS

Robert Becker/MIT

12 January, 2007

AMS TIM @ JSC

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Agenda

• AMS Assembly Area/Clean Room 867 • STA & Flight Integration Hardware Status• Pre-integration of STAs in the Flight USS prior

to STA VC/CMR arrival• Pre-integration of Detectors on the STA VC &

Flight USS prior to Flight Cryomagnet arrival• Integration discussion items & plans for

resolutions• Final Flight Integration• Integration data delivery

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AMS Assembly Area Clean Room 867

Everything in the AMS Assembly Area/Clean Room 867 needed to begin the STA integration will be ready no later than (NLT) February 2, 2007.

• Operation as a Clean Room (air conditioning, filters, sealed & positive pressure) will be ready in May, 2007

• Rotation Assembly Stand (RAS) delivered, assembled, installed, and ready for use

• Scaffolding delivered, assembled, and ready for use

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AMS Assembly Area Clean Room 867

• Information provided in the Resource Requirements checklists has been used to order common use supplies and to estimate facility requirements

• Work area required – with & without crane access & special access• Crate storage area, volume, and environment• Tables & chairs• Storage cabinets & open shelves• Air bearing pallet requirements• Cleaning fluids/supplies & vacuum cleaners• Supply gases (Xe, He, CO2, N2, Compressed air, etc.)• Fans for ventilation/cooling of hardware & personnel• Power requirements• ???

• If you didn’t ask for it on the checklists, do NOT expect it to be provided!

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Remov-able Ceiling Panels

NCeiling Panels

are NOT Removable

Airlock

AMS Assembly Area Clean Room 867

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• STA VC integration with the STA Magnet (Cold Mass Replica - CMR) was completed in December at SM• STA VC Arrived in Terni/INFN for Sine Sweep Tests

on January 10th• Test hardware was previously shipped to Terni and

testing has been completed• Ship STA VC to ESTEC for Acoustic Tests - March

’07 *• Return to CERN for integration in USS – late March

’07 *

* Depends on results of STA VC/CMR sine sweep & acoustic tests

AMS STA Integration Hardware

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•Flight USS is complete and will arrive at CERN with the Primary Support Stand (PSS) and the Primary Lift Fixture (PLF) on January ~22-23, 2007

AMS Flight Integration Hardware

•Flight Vacuum Case is complete and will be shipped to SCL/SM when they have room in their facility to accommodate it (after Flight Cryomagnet tests are completed and the SFHe Tank is delivered and SFHe leak tested)

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Pre-integration of STAs in the Flight USS Prior to STA VC Arrival

STA Hardware Pre-integration in Flight USS

• On-line integration of the STA Crates/Radiators on the USS will begin the week of February 5, 2007– before the STA VC arrives

• This allows work to proceed even if the sine sweep & acoustic tests are delayed

• 10T crane installation will be delayed until after STA Pre-integration is complete at beginning of March• If necessary, the USS/STAs in PSS will be moved

away from crane installation• There are ~3-4 weeks available in March to use the flight

USS & STAs for fit checks, cable & plumbing runs, measurements, etc.

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STA Hardware assembly in Flight USS (cont)

• Integration of all STAs in USS to be completed by mid-April ’07 *

• Even though the STA VC delivery to Terni slipped ~5 weeks and the RAS readiness at CERN slipped ~3 weeks, this is only ~2 weeks later than previously reported at AMS TIM on October 27, 2006

Ship USS with STAs to Munich/IABG in April ’07 *• Static Tests• Modal Tests• Return USS with STAs to CERN in August ’07 *

* Depends on results of STA VC/CMR sine sweep & acoustic tests and USS/STA modal & static tests

Pre-integration of STAs in the Flight USS Prior to STA VC Arrival

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Integration Discussion Items

• Interference between Flight VC/Magnet & Electronics Crates during Final Flight Installation

• Interference with installation access holes on LUSS after LTOF is installed

•ECAL Main Fixation Bolts & Shims•TRD M-Structure Shear Pins & Eccentric bushings•Schedules, Schedules, Schedules

Top Views Bottom

Views

Temporarily remove mid-brackets and lower struts

Move Main Ram & Wake Radiators outward to allow installation of Flight VC & Magnet

Temporarily Reattach Top Brackets to Upper USS

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Interference between Flight VC/Magnet & Electronics Crates during Final Flight Installation

• R. Becker/MIT, J. Kastelic & P. Mott/JS, & R. Stafford-Allen/SM to determine how much room is required to clear the Flight VC/Magnet as well as how much room is available by Jan 29th.

• Provide estimate of additional length required for lower inter-radiator cables to M. Capell & A. Lebedev

• Final cable routing must accommodate additional length• Be sure there’s no interference with hardware mounted outboard of crate jigs

during pre-integration activities• Upper inter-radiator connections will be disconnected because the additional length

will be too much additional weight• C. Lauritzen/JS to determine if there is any problem on the USS if the brackets are

temporarily re-attached at a wider position by Feb 5th• M. Molina/CGS to determine if Radiator brackets are OK by Feb 5th

• Consider using blocks/spacers under the brackets and reattaching the lower struts• K. Bollweg & J. Heilig will arrange trial test using STA Crates/radiators in late February

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Interference with installation access holes on LUSS after LTOF is installed

•J. Kastelic to provide USS Interface info to G. Laurenti & F. Cadoux by Feb 16th so four new handling brackets can be made

•G. Laurenti to produce new handling brackets by Sept 1st

New handling brackets will use existing fasteners and swivel hoists

F. Cadoux to provide extra long hold-down bolts to GSE

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ECAL Main Fixation Bolts & Shims

•NASA will provide the ECAL Main Fixation Bolts•The flight Shims have already been provided

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TRD M-Structure Shear Pins & Eccentric Bushings for STA

SS - Aachen

SS or Al - Aachen

SS Bolts, Nuts, & Washers - NASA

SS – NASA? Aachen?

SS - Aachen

SS – NASA? Aachen?

Al or SS - NASA

USS (Al) - NASA

TRD M Structure (Al) - Aachen

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TRD M-Structure Shear Pins & Eccentric Bushings for Flight

Ti - Aachen

Ti - Aachen

SS Bolts, Nuts, & Washers - NASA

SS – NASA? Aachen?

Ti - Aachen

SS – NASA? Aachen?

Al or SS - NASA

USS (Al) - NASA

TRD M Structure (Al) - Aachen

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• All the detector groups have continued to evaluate the pre-integration proposal and have agreed that it should proceed according to the schedules thoroughly discussed at this TIM• Current estimate of Pre-integration start: August, 2007• Pre-integration finish: December, 2007

• Optical fibers between ACC & VC for TAS will be installed• Constantly monitor the Cryomagnet progress and decide

how much more flight hardware to pre-integrate• Current estimate of magnet delivery to CERN: February, 2008

• Do as little de-integration as possible – just in time to remove the STA VC and install the Flight VC & Cryomagnet in the USS

Pre-integration of Detectors on STA VC & USS prior to Cryomagnet Arrival

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• Consider removing the STA VC, Tracker, and ACC from the USS as an assembly so parallel work can continue during Flight VC/Magnet installation• Use VC rotation fixture and wheels/brackets developed at SM

• This could shorten deintegration by 2-3 weeks; thus allowing combined cosmic ray testing to be extended

Pre-integration of Detectors on STA VC & USS prior to Cryomagnet Arrival

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• All detectors must be integrated and functionally tested with the Flight VC and Cryomagnet at CERN by July, 2008

• Beam tests at CERN (~1 month reserved)• Thermal Vacuum Tests at ESTEC (~3 months reserved)• EMI Tests at ESTEC (~1 month reserved)

• Delivery to KSC in December, 2008

Final integration of Detectors on Flight VC & USS after Cryomagnet Arrival

AMS Integration Data DeliverySTA

Pre-Integration

Flight Integration

STAPre-

IntegrationFlight

Integration

(On-Line)(Off & On-

Line)(On-Line) (Off-Line) (On-Line) (On-Line)

(Off & On-Line)

(On-Line)

DUE DATE: 29-Sep-06 29-Sep-06 29-Sep-06 29-Sep-06 29-Sep-06 22-Sep-06 9-Oct-06 12-Jan-07 12-Jan-07HDWR to

CERN - 30 days

Tracker Stefano Lucidi N/A 3-Nov-06 3-Nov-06 2-Oct-06 2-Oct-06 3-Oct-06 N/A

TRD Klaus Luebelsmeyer 12-Sep-06 12-Sep-06 15-Nov-06 12-Sep-06 12-Sep-06 15-Nov-06 15-Nov-06

TRD Gas Sys Thorsten Siedenburg 5 N/A 3-Nov-06 12-Sep-06 28-Sep-06 28-Sep-06 15-Dec-06 N/A

LTOF F. Palmonari & G. Laurenti 6, 7 N/A N/A 20-Nov-06 27-Oct-06 27-Oct-06 15-Dec-06 N/A

UTOF Federico Palmonari 6 N/A 3-Nov-06 20-Nov-06 27-Oct-06 27-Oct-06 w/TRD N/A

RICH Carlos Diaz Ginzo 6 N/A N/A 27-Oct-06 27-Oct-06 27-Oct-06 In work by FC N/A

ECAL Franck Cadoux 1 20-Oct-06 N/A 20-Oct-06 20-Oct-06 20-Oct-06 Early 25-Nov-06

Cryomagnet Stephen Harrison 2 19-Sep-06 19-Sep-06 19-Sep-06 19-Sep-06 In work 9-Oct-06 N/A

Cryo GSE Alexander Grechko N/A N/A 12-Oct-06 19-Sep-06 19-Sep-06 N/A N/A N/A N/A N/A?

CAB 4 Mike Capell 4, 7 N/A N/A ? ? ? ? N/A N/A

TAS Wolfgang Wallraff N/A 29-Sep-06 29-Sep-06 20-Oct-06 20-Oct-06 15-Dec-06 N/A 12-Sep-06 12-Sep-06

ACC Thomas Kirn 3 N/A 29-Sep-06 29-Sep-06 29-Sep-06 29-Sep-06 15-Dec-06 N/A

Elect Crates Giovanni Ambrosi 9/27 w/ TCS 27-Oct-06 27-Oct-06 ? 9/27 w/ TCS

UPS & CDD 4 Tim Urban 4 N/A N/A 15-Nov-06 15-Nov-06 15-Nov-06 N/A N/A

EGSE 4 Alexandre Elin 4 N/A N/A N/A 15-Nov-06 N/A N/A N/A N/A N/A N/A

Cabling Alexei Lebedev N/A 28-Sep-06 28-Sep-06 ? N/A

TCS Marco Molina 27-Sep-06 27-Sep-06 27-Sep-06 27-Sep-06 27-Sep-06 12-Oct-06 27-Sep-06 N/A? 27-Sep-06

TTCS J. van Es & He Zhenhui 7 N/A N/A 29-Oct-06 27-Oct-06 27-Oct-06 29-Oct-06 N/A N/A?

USS Joe Kastelic 7 19-Sep-06 19-Sep-06 19-Sep-06 19-Sep-06 19-Sep-06 22-Sep-06 28-Apr-06

VC Phil Mott 19-Sep-06 19-Sep-06 19-Sep-06 19-Sep-06 19-Sep-06 22-Sep-06 28-Apr-06

Star Tracker Paolo Trampus N/A 31-Aug-06 31-Aug-06 31-Aug-06 31-Aug-06 N/A N/A

GPS Claude Zurbach N/A N/A Del 1/15/07 20-Oct-06 26-Oct-06 N/A N/A

Building 867 S.Ting N/A N/A N/A N/A N/A N/A N/A

1 Original POCs were Franco Cervelli & Jean-Pierre Vialle; changed to Franck Cadoux on August 25, 20062 Original POC was Robin Stafford Allen; changed to Stephen Harrison on September 14, 2006. 3 Original POC was Wolfgang Wallraff; changed to Thomas Kirn on October 2, 2006.4 New System and Gert Viertel as POC added on Oct. 20; approved on Oct. 26, 2006.5 Original POC was Feng Zhou; changed to Thorsten Siedenburg on October 26, 2006.6 Original POC was Giuliano Laurenti; changed to Carlos Diaz Ginzo & Federico Palmonari on October 27, 2006.7 POCs added for Safety inputs or revised because of availability at JSC TIM on January 10, 2007.

Input received/sched late, incomplete, or there are questions

Input received on time & should be adequate for now

Input was expected, but none was received

Not Applicable - no input required

DETECTOR / SYSTEM

Point of Contact (POC) Below

Draft Integration ProceduresIntegration SchedulesResource Checklists

CAD models for fluid lines or cable

routing

Follows detectors/crates

Follows detectors/TCS

With Project 867 weekly minutes

Accept-ance Data Packages

What we have… sort of.

Where we must be by December 2008 at KSC...