Updates on AMS-02 Veronica Bindi Physics and Astronomy Department - - PowerPoint PPT Presentation

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Updates on AMS-02 Veronica Bindi Physics and Astronomy Department - - PowerPoint PPT Presentation

- Workshop SLAC - March 6-8, 2013 Updates on AMS-02 Veronica Bindi Physics and Astronomy Department University of Hawaii at Manoa AMS is a US DOE led International Collaboration Spokesperson: Nobel laureate Prof. Dr. S. Ting from MIT AMS-02


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  • Workshop SLAC - March 6-8, 2013

Veronica Bindi

Physics and Astronomy Department University of Hawaii at Manoa

Updates on AMS-02

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AMS-02 has been installed on the International Space Station

  • n May 19th 2011

AMS is a US DOE led International Collaboration

Spokesperson: Nobel laureate Prof. Dr. S. Ting from MIT

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6

5 m x 4 m x 3 m 7.5 tons

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AMS consists of 5 sub-detectors which provide redundant information for particle identification

TRD TOF

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  • Indirect search of Dark Matter: simultaneous observation in several signal

channels... e+ , antiprotons, Ɣ, antideuterons

  • Measuring CR spectra up to the iron – refining propagation models;
  • Solar modulation on CR spectra over 11 year solar cycle
  • Solar activity
  • Direct search of primordial antimatter: Anti He, Anti C ...
  • New forms of matter: strangelets
  • Identification of local sources of high energy photons: SNR, Pulsars, ...

Scientific goals of AMS on the International Space Station Main analysis currently

  • n going:
  • Positron fraction
  • B/C
  • P, He, electron ... fluxes
  • Monitor of the solar activity

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Time at location [s]

AMS-02 Orbital parameters

Acquisition rate [Hz] DAQ efficiency Particle rates vary from 200 to 2000 Hz per orbit Average DAQ efficiency 85% Average DAQ rate ~800Hz 28 billion events collected in 18 moths 60 TB raw events (Downlink 10 Mbit/s)

19 May 2011 1 Jan 2013

DATA collected

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TRD offline calibration

TRD alignment

Cosmic protons are used for alignment to an accuracy of 0.04 mm for each straw module and used to calibrate the detector response to 3% accuracy.

TRD gain calibration

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Tracker layers thermal stability

Tracker Thermal Control System

Coordinate resolution on each plane is measured with 10 µm in the bending direction. Position of ladders in the external layers are dynamically aligned to an accuracy of 3 µm.

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TRD Distinguish between electrons and protons SILICON TRACKER and MAGNET measure the sign and the rigidity ECAL measures the energy, Identifies 3D characteristic positron shower and rejects hadronic showers

Total rejection of proton 1,000,000 Verified at test beam at CERN Positron identification and Proton rejection

e+ low signal and high P background: P ~ (103 ÷104) e+ P rejection factor: 105 ÷106 to identify e+ with an error at % level

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Proton rejection at 90% e+ efficiency Rigidity (GV)

  • ISS data

Signals from 20 layers are combined in a likelihood estimator which allows an efficient discrimination of proton background

TRD Proton rejection

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A fit of particle trajectory is used to measure the sign of the particle and its rigidity: 1) Used to suppress e- 2) compared to the energy E measured by ECAL to suppress P.

3 m

Tracker e+ and e- identification and P rejection

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Positron E=636 GeV

The Electromagnetic Calorimeter

17 radiation length

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Momentum (GeV/c)

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3

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Proton Rejection

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2

10

3

10

4

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5

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ECAL performance on ISS

A Boosted Decision Tree (BDT) is constructed on the basis of the shower shape in the ECAL to distinguish protons and electrons. BDT and E/p matching combined give a Proton Rejection of 104

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The TRD Likelihood shows clear separation between protons and positrons with a small charge confusion background

E bin = 82 - 100 GeV

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AMS-02 Positron Fraction will be published soon

e+ / (e+ + e−) Energy (GeV)

HEAT: J.Beatty et al., Phys. Rev. Lett. 93 (2004) AMS-1: M.Aguilar et al., Phys. Lett. B 646 (2007) Pamela: O.Adriani et al., Astropart. Phys. 34 (2010) FERMI: M.Ackermann et al., PRL 108 (2012) 15

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Geomagnetic cutoff

Average Incidence angle

East West

ΔΦ (degrees)

Particle Rigidity (GV)

Protons Electrons Average AMS-02 inclination

East - West effect

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AMS Nuclei Measurement on ISS

Entries

H He Li Be B C N O F NeNaMg Al Si Cl Ar K Ca ScTi V Cr P S Fe Ni

0 5 10 15 20 25 0 5 10 15 20 25

108 107 106 105 104 103 102 10 1

T

  • F

C h a r g e Tracker Charge Accurate Study of the composition of the cosmic rays Multiple Independent Measurements of the Charge (|Z|)

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Helium rate

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ZTRK_L1=5.2 ZTRD=5.2 ZTOF_UP=5.5 ZTOF_LOW=5.4 ZTRK_L2-L8=5.0 ZRICH=4.8

Boron

Rigidity=680 GV

Boron and Carbon

ZTRK_L9=5. 1 ZTRK_L1=5.8 ZTRD=6.0 ZTOF_UP=6.1 ZTOF_LOW=6.5 ZTRK_L2-L8=6.0 ZRICH=6.1

Rigidity=666 GV

Carbon

front view side view front view side view

ZTRK_L9=6.1

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ZTOF_LOW=5.2 ZTRK_IN=4.8 ZRICH=5.1 ZTRK_L1=6.1 ZTRD=6.0 Z0=9.9 Z1=5.3

Carbon Fragmentation to Boron in Upper TOF

Rigidity 10.6 GV

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Boron measured by AMS

(~90%)

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Conclusions

  • AMS02 is in on the ISS since May 19th 2011 and all the detectors

are properly functioning

  • Detector calibration (alignment, e/p rejection, charge id, etc.) are well

advanced

  • Data analysis is in progress (positron fraction, P and He fluxes, B/C

ratio, gamma)

  • 10+ years on board the ISS at 109 events/year will provide enormous

sensitivity and statistic: great physics potential We want to thank NASA and DOE for making AMS possible!

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Science coming soon!!! Stay tuned!!!

Thank you

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Back-ups

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Test Beam Results used as reference points

Velocity measured to an accuracy of 1/1000 for 400 GeV protons Bending Plane Residual (cm)

N N

Reconstructed Velocity

TRD: 400 GeV protons Energy N

e± Energy Resolution: 2.5-3%

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The Time of Flight System - Data from ISS

TOF 1 and 2 TOF 3 and 4

Measures Velocity and Charge of particles

Plane 4 3, 4

Z=2 Z=6 σβ=2% σTime=80ps σβ=1.2% σTime=48ps

x103

TOF Charge Events/Bin Events/Bin TOF Charge Z±ΔZ=26.01± 0.38

Z=26 One-Typical-Counter Charge Resolution

Velocity [Rigidity>20GV] Events Velocity [Rigidity>20GV] Events

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Accurate Study of the composition of the cosmic rays

Multiple Independent Measurements of the Charge (|Z|)

TRD T O F Tracker TOF RICH ECAL

1

2

7-8 3-4 9 5-6

  • 1. Tracker Plane 1
  • 6. RICH
  • 4. Tracker Planes 2-8
  • 7. Tracker Plane 9
  • 2. TRD
  • 3. Upper TOF
  • 5. Lower TOF
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There are six types of Quarks found in accelerators (u, d, s, c, b, t). All matter on Earth is made out of only two types (u, d) of quarks. “Strangelets” are new types of matter composed of three types of quarks (u, d, s) which should exist in the cosmos.

Carbon Nucleus Z/A ~ 0.5 Strangelet Z/A ~ 0.1 37

u d s s d d s s u d u d u u d d s u s u u d d d d d d u u u u s u s s s

d d u u u d u u d d d u u u d d d u d d u d d u d d u u u d u u d u u d

p n

Search for New Matter in the Universe

  • E. Witten, Phys. Rev. D,272-285 (1984)

After many years, the question of the existence of strange quark matter still remains without a definitive answer.

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Strangelets

Front view Side view β1 Amplitude => Z, β2 Rigidity = 4.31 ± 0.38 GV Charge Z = 2 β1 = β2 = 0.462 ± 0.005 Mass = 16.45±0.15 GeV/c2 Z/A = 0.114 ± 0.01 Flux (1.5 < EK < 10 GeV) = 5x10-5 (m2 sr sec)-1

Candidate observed with AMS-01 5 June 1998 11:13:16 UTC

Jack Sandweiss (Yale) is leading the AMS search.

Z/A~0.1

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On-orbit thermal control

Over 1,100 temperature sensors and 298 heaters are monitored to assure components stay within thermal limits and avoid permanent damage.

E q u a t

  • r

ISS Orbital Plane

23.4o

Earth’s Orbital Plane

Solar Beta Angle

Solar Vector SUN

β

Orbital Inclination 51.6o

The thermal environment on ISS is constantly changing due to:

  • Solar Beta Angle (beta)
  • Position of the ISS Radiators and Solar Arrays
  • ISS Attitude

STBD Main Radiator moved from -8o to +25o STBD Main Radiator parked at -8o TRD Pump temperature 3 Sep 4 Sep 5 degrees in a few hours

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As estimations: 3 g/cm2 in the TRD 2 g/cm2 in the TOF

Material on AMS-02

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AMS Data/MC Volumes Projected

DATA Per Year Of Operation:

  • 1.6×1010 Events
  • 35 TB Raw Events
  • 130 TB Reconstructed Ev.

MC Per Year Of Operation:

  • ~2 X 1010 Simulated Events
  • ~ 200 TB Simulated Data Volume