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AMS the AntiMatter Spectrometer

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The future: 2001-2003 and beyond... STS-91 mission (June ... Aerogel Threshold Cherenkov - 2 planes. 168 10x10cm2 7cm thick solid cells. D. VITE' - AMS Gen ve ... – PowerPoint PPT presentation

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Title: AMS the AntiMatter Spectrometer


1
AMSthe Anti-Matter Spectrometer
  • The past ? 1999
  • The present 2000
  • The future 2001-2003 and beyond
  • STS-91 mission (June 1998)
  • ISS 3 year mission (May 2003?)

2
AMS in space
  • the first large magnetic spectrometer
  • i.e.
  • the first particle physics experiment
  • and
  • the biggest silicon system to date

3
AMS Physics Goals (1)
  • Measurement of H, He, C isotopes
  • better understanding of cosmic ray origin and
    propagation in the galaxy
  • Antiprotons and positrons
  • search for exotic sources
  • High energy photons (gt 1 GeV)
  • complementary to satellite and ground telescopes

4
AMS Physics Goals (2)
Search for antimatter primary goal of AMS, up to
Z 6
  • Antimatter discoveryantistars, primordial
    antimatterExplanation for antimatter domain
    formation?
  • No antimatter foundexplanation for antimatter
    disappearance?Strong CP-violation?

Antihelium could originate from primordial
nucleosynthesis OR from antistars anticarbon
could ONLY come from antistars
5
The AMS apparatus for the precursor flight (1)
  • Construction and test of detector elements
  • assembly, integration, system tests
  • space qualification  outgassing, vibrations
  • Permanent magnet
  • 1.2m diameter, 80cm height, 1.9 tons
  • 0.15 Tesla
  • blocks of Nd-Fe-B of high field strength

6
The AMS apparatus for the precursor flight (2)
  • Tracker
  • 4 inner planes and 2 outer planespartially
    equipped (40)
  • 57 modules of 11 to 15 double-sided DC silicon
    microstrip detectors (CSEM, Neuch.)
  • front-end Viking/High Dynamic Range4ms peaking
    time, 0.7 mW/ch
  • 365W allocated (out of 1 kW), 0.5 Mbit/s (out of
    1), 5MHz ADC on ext. TDR

7
The AMS apparatus for the precursor flight (3)
  • Time-of-flight - 4 planes
  • trigger
  • particle velocity and absolute charge
  • Anticoincidence - 16 counters
  • background rejection (albedo)
  • Aerogel Threshold Cherenkov - 2 planes
  • 168 10x10cm2 7cm thick solid cells

8
The STS-91 Discovery missionJune 2-12, 1998 (1)
  • Transport
  • from ETH-Zurich to Kennedy Space Center
  • Final tests and integration
  • Installation on the Shuttle Discovery
  • More tests and software uploads.
  • Launch
  • Switch on and first data downloads!

9
The STS-91 Discovery missionJune 2-12, 1998 (2)
  • Data Taking
  • Control from Johnson Space Center
  • Slow Rate
  • temperatures, currents
  • counter rates, voltages
  • High Rate
  • calibrations
  • full events (ehm)

10
The STS-91 Discovery missionJune 2-12, 1998 (3)
  • Landing at KSC
  • Transport
  • back to ETH-Zurich
  • Beam tests ( cosmic muons)
  • GSI-Darmstadt
  • Helium, Carbon
  • Cern-Geneva
  • charge-1 particles

11
Physics from STS-91
  • Search for antihelium
  • 2,86 million helium nuclei observed
  • rigidity 1 to 140 GV
  • Search for antimatter
  • Cosmic ray proton spectra
  • from 0.1 to 200 GeV
  • Gamma ray search

12
Que fait Genève? (1)
  • Mechanical design
  • support, cooling
  • Construction of tracker modules (ladders)
  • Tests, metrology and integration of modules
  • Electronic design
  • Analysis and simulations
  • Silicon development
  • Environmental studies
  • Problem analysis from STS-91

13
Que fait Genève? (2)
  • full responsibility of tracker readout system
  • FE electronic hybrids production test
  • development of module test system
  • PC card, power supply (temp)
  • one of the three production lines of tracker
    modules
  • module integration center

14
AMS on the International Space Station (1)
  • Precursor Flight final data analysis
  • near completion (2000)
  • RD for Phase II (1999-2001)
  • design finalisation and optimisation
  • superconducting magnet
  • new detectors
  • space qualification of single elements

15
AMS on the International Space Station (2)
  • 2nd construction phase
  • Assembly (2000-2002)
  • Full space qualification
  • long-term operation tests
  • Installation on the Space Station (2003)
  • 3 to 5 years of data taking
  • (if we get He refill)
  • Lots of work and physics (and fun) ahead!
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