Title: cl99061_8_2007'ppt
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22007
Size 109 m x 80 m
Mass 420 t.
cl99061_8_2007.ppt
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5Ninety Years of Super Conductivity
Normal conduction Wire
Nobel Prizes in
H. Kammerlingh-Onnes Discovery of
Superconductivity
1913
J. Barden, L.Cooper, J.Schrieffer Theory of
Superconductivity (BCS theory)
1972
current
1987
G.Bednorz, A.Müller Discovery of High
temperature Superconductivity
Metal atoms oscillate ? cause friction ? HEAT
Super-Conduction at -270C (Kammerlingh-Onnes
1911)
2003
A.A. Abrikosov, V.L. Ginzburg, A.J.
Leggett Theory of superconductors and
superfluids
current
Applications of Superconductivity Avoid Quench
Quench loss of superconductivity due to relative
motion of wire ? friction ? temperature increase
Metals Pb, Nb, Ti ? Atoms rest, Cooper pairs
of electrons move frictionless (Quantum Mech.)
Superconducting Super Collider (SSC)
1990
y01K530e.ppt
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7Testing Coil to full current
It is not possible to quench the coils except by
outside heating
y03K286bbMagMeetSCL.ppt
8Quench protection
To ensure not to loose all He in case of quench
- All coil cooling is by conduction
- Coils designed for heat removal
- from a small number of discrete points.
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14Configuration of magnet supports
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15Magnet support Straps
300K
The cold mass of 1.8 K has to be supported to
the vacuum case, which is approximately 300
K. This is achieved by 16 straps, which hold the
2-ton cold mass in position during launch
(acceleration 3g) and landing (de-acceleration
10g). In space, the straps are designed to be
nearly disconnected so as not to transfer heat
from the vacuum case to the cold mass.
Tension-only straps with a passive
orbital disconnect.
y03K214dHarrisonStrap.ppt
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18Ground Support Equipment for cool down and
filling AMS with SFHe
(SJTU, ETH-MIT, NASA, SCL)
A B
B only
AMS to Shuttle
AMS arrival
3
1
1
AMS testing
2
A B
B
A
80K-1.8K
300-80K
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29Ring Imaging Cerenkov Counter (RICH)
DV/V 0.1 to determine the mass
P mV
Q?? V
Q?? V
11040 (4mm x 4mm) photomultipliers
Major contribution from Spain M. Aguilar-Benitez
Coordinator G. Laurenti
y03K193_05ca_y1K234RichLscap.ppt
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31AMS-02 Calorimeter
3D Sampling
LAPP Annecy
INFN Pisa
IHEP Beijing
J.P. Vialle
F. Cervelli
H.S. Chen
Shower ? e energy
y01K525_5_03EcalLscap.ppt
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37AMS-02 Electronics
Production, Testing, QA Qualification
Bulk of flight electronics produced at CSIST,
Taiwan, established Mil-Spec technologies,
infrastructure QA 25 engineers 45
technicians. Quality assured by NASA, LMSO AMS
team reviews every 3 months. Testing (Vibration,
Thermal, EMC) at CSIST with established
facilities, teams. Testing (Thermal Vacuum) at
NSPO, Taiwan with space qualified facilities.
y03K324aCapell.ppt
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41AMS-02
After integration, the complete electronics and
detectors will undergo
Calibration Test Beam at CERN
Thermal-Vacuum Test at ESA (Noordwijk)
y03K088a_1.ppt
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45AMS on ISS (search for antimatter
109
108
107
106
105
Yield on GV/c intervals, for 3 years on ISS
104
103
102
10
1
10-1
0
400
800
1200
-400
-800
-1200
GV
Search He sensitivity of 1/billion
?
If no antimatter is found ? there is no
antimatter to the edge (1000 Mpc) of Universe
y2K021c_03.ppt
46Search He sensitivity of 1 / billion
Alpha Magnetic Spectrometer on the International
Space Station (AMS-02) Antimatter Investigation
System (AIS) at Southeast University,
Nanjing June 2003
S.E.U.
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50Unidentified Sources with AMS
g ? e e
g ? e.m.shower
y01K062_2a
y01K062_03.ppt
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58CONCLUSION
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63TVT tests
Make stands
1-
Preparation group
2-
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64Weight reduction
4 x JMDC
1-
Remove most USCM
2-
y03K348.ppt
65WEIGHT meeting
November 28, 2003 S.C.C. Tingoffice 32/4B-03
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66Electronics meeting
December 8 - 12, 2003 CSIST, Taiwan
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67CSIST meeting, Dec. 8 - 12, 2003
December 8, 9 J, JT, JPD systems December 10,
11 T, U systems December 12 UPS systems
y03K344.ppt
68CSIST meeting, Dec. 8 - 12, 2003
- Uni. of Geneva E. Cortina
- Karlsruhe F. Hauler
- Perugia M. Menichelli
- Perugia G. Ambrosi
- MIT S.C.C. Ting
y03K343.ppt
69TIM meeting
January 19 - 23, 2004 at K.S.C.- NASA or at CERN
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70The Thermal CDR is scheduled To be in Milano
(ITALY) At Carlo Gavazzi Space 29-30 January
2004
y03K352
71Thermal CDR - Attendees
- Magnet SCL (S. Harrison)
- ACC LMSO (C. Clark)
- PDS CGS
- Cryocoolers GSFC (S. Breon)
- TTCS NLR, NIKHEF, GVA
- RICH-ECAL-TOF CGS
- TRD OHB-system / RWTH Aachen
- TRD GAS BOX LMSO (C. Clark)
- CAB Crisa
- UPS LMSO (C. Clark, P. Nemeth)
- Electronics MIT (M. Capell)
- Star Tracker INFN RM
- Bricks CNR-FI (G. Castellini)
- CVB ETH (J. Ulbricht)
- J. Burger, H. Hofer
- 3 from OHB
- R. Becker, Y. Wang
- 8 from CGS
- NSPO J.R. Tsai
- LMSO C. Clark, R. Harold,
- B. Sommer, T. Martin
- 2 PHASE expert GSFC
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72Inputs Needed
- Coupled Loads Analysis from LMSO
- by end Nov.
- Confirmation of agreed configuration
- by Nov. 28 mass saving meeting
- Data from subdetectors by 19 Jan. 04
-
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73Safety and rehearsal meetings combined with TIM
March 8 - 12, 2004 at CERN Council Chamber
y03K346.ppt