Title: Folie 1
1AMS02 ACCstatus(background info flight safety )
- October 21, 2004
- Houston
- W. Wallraff
2ACC flight hardware
3ACC general dimensions
RWTH-Dwg 1865 see RB/MW for a copy
4ACC mounting details
RWTH-Dwg 1770b see RB/MW for a copy
5ACC AMS-01 ETH Zürich July 1997
6ACC panel overall dimensions
8mm
7light transport (shifter part) hermeticity
by interlocked panels
2 x 37 fibres
8ACC panel in preparation for glueing the fibres
9ACC light detection system on VC
10PMT, VC and tracker-flange (Z,Y-)
Underneath the MLI, exit for cables to S crate,
cable stress relief
11ACC AMS-01 cabling supports
123
03. Dec. 03
2
5
1
4
ACC Connector Materials
132x40gx, 2x10gy, 2x10gz Displacement Vector Length
0.967 mm
14light cable fixation results of FE calculations
- Summary
- Max. Length of Displacement Vector
- 0.967 mm (2x40g)
- Max. Stress in VC Web
- lt13 MPa (2x40gx), lt48 MPa (2x40gy), lt21 MPa
(2x40gz) - Margin of Safety
- Minimal MS (spring)270/147 1 0.8
- Minimal MS (connector support) 462/140-12.3
15Finished panel, fine mesh PMT, properties of
wrapping
16ACC (ToF) PMT housing
17PMT housings (Bologna INFN) before potting
- Polycarbonate (injection molded)
- voltage divider completely sealed
- vented
- glass tight
18ACC PMT Support
19PMT housing with ACC plastic fibre connector (2
panels)
03. Dec. 03
20Fibre routing in front of ACC PMT
03. Dec. 03
21PMT front view including light cable (148 fibres,
2 panels)
03. Dec. 03
Radius R3
Radius R10.125
Entry cross-section area equals that of a hose
with a diameter of 14mm (individual lightcable)
22PMT vibration test (RWTH, Prof. Lübelsmeyer)
23PMT (in box) response to vibrations
24PMT gain before and after space qualification
tests
25ACC Connector and Support Design
26Connector View From Outside The VC
03. Dec. 03
3,1mm
Distance from lower edge of hose to upper edge of
the VC-Rib
27Connector View From Inside The VC
03. Dec. 03
1,9mm
Distance lower edge hose to upper edge VC-Rib
(blue lines)
28Connector View From Outside The VC
03. Dec. 03
2.8mm
Height of the Connector above the radial ribs
29Center VC Cross-Section (Z) with ACC lightcables
30ACC status 20-Oct-04
- ACC detection hardware
- Design finished
- Fabrication of engineering modules
- Cosmics beam tests are done
- Components for the production of flight modules
are being purchased - ACC electronics
- Design at INFN Bologna (SFEA, SHV, ..)
- Meeting at CERN 27th October
- Fabrication of engineering modules spring 2005
- Fabrication of flight modules winter 2005
- Tests of CAEN produced SFET, SHV (for ToF) this
winter - ACC installation
- Magnet up right
- Test with cosmics magnet horizontal/inclined
- Details see RB, KL, GL study
31Cabel Fixation
32(No Transcript)
33ACC Connector PMT Arrangement
34PMT box (common for both ToF and ACC)
35ACC mounting on VC