P A M E L A Payload for Antimatter / Matter Exploration and Light-nuclei Astrophysics

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P A M E L A Payload for Antimatter / Matter Exploration and Light-nuclei Astrophysics Mark Pearce KTH, Department of Physics, Stockholm, Sweden SLAC Summer Institute / 2007-08-07

Overview Indirect searches for dark matter with antiparticles (briefly - already covered by Lars Bergström) Description of PAMELA instrument and performance Launch into orbit (15th June 2006) Flight data (i.e. does it work?)

Signal (SUSY) background p p p p p p ISM CR e e X p p e X p p ISM CR e ISM CR γ γ γ π π ν ν μ ν μ π π μ μ ; ; ; ; 0 0

AMS-01: space shuttle, 1998 Antiprotons CAPRICE balloon experiment, 1998 Secondary production (upper and lower limits) Simon et al. ApJ 499 (1998) 250. PAMELA Secondary production C94 model primary χχ distortion Primary production from χχ annhilation (m(χ) = 964 GeV) Ullio : astro-ph/9904086 Secondary production (CAPRICE94-based) Bergström et al. ApJ 526 (1999) 215

Secondary production Moskalenko Strong model without reacceleration. ApJ 493 (1998) 694. Positrons Secondary production Leaky box model R. Protheroe, ApJ 254 (1982) 391. PAMELA Secondary production MS model primary χχ distortion Primary production from χχ annhilation (m(χ) = 336 GeV) Baltz Edsjö, Phys Rev D59 (1999) 023511.

UED models: Kaluza-Klein Klein dark matter e Insert other chi mass plot Mention KK p - KK Cheng, Feng, Matchev, hep-ph/0207125v2 Bringmann, astro-ph/0506219v2

~450 kg e - p - e p (He...) ~1.2 m Trigger, ToF, de/dx Anticoincidence system reduces background. - Sign of charge, rigidity, de/dx NB: e /p: 10 3 (1 GeV) 5.10 3 (10 GeV) p /e - : 5.10 3 (1 GeV) <10 2 (10 GeV) Electron energy, de/dx, lepton-hadron separation

The magnet Characteristics: 5 modules of permanent magnet (Nd-B-Fe alloy) in aluminum mechanics Cavity dimensions (162 x 132 x 445) cm 3 GF ~ 21.5 cm 2 sr Magnetic shields 5mm-step field-map on ground: B=0.43 T (average along axis), B=0.48 T (@center)

The tracking system Main tasks: Rigidity measurement Sign of electric charge de/dx (ionisation loss) Characteristics: 6 planes double-sided (x&y view) microstrip Si sensors 36864 channels Dynamic range: 10 MIP Performance: Spatial resolution: ~3 μm (bending view) MDR ~1 TV/c (from test beam data)

The electromagnetic calorimeter Main tasks: lepton/hadron discrimination e /- energy measurement Characteristics: 44 Si layers (X/Y) 22 W planes 16.3 X o / 0.6 λ L 4224 channels Dynamic range: 1400 mip Self-trigger mode (> 300 GeV; GF~600 cm 2 sr) Performance: p/e selection efficiency ~ 90% p rejection factor ~10 6 e rejection factor > 10 4 Energy resolution ~5% @ 200 GeV

Combined tracker calorimeter performance Non-interacting p 100 GeV/c Interacting p 100 GeV/c Interacting e - 100 GeV/c (CERN SpS testbeam 2003)

The time-of-flight system Main tasks: First-level trigger Albedo rejection de/dx (ionisation losses) Time of flight particle identification (<1GeV/c) Characteristics: 3 double-layer scintillator paddles X/Y segmentation Total: 48 channels Performance: σ(paddle) ~ 110ps σ(tof) ~ 330ps (for MIPs)

The anticounter shields Main tasks: Rejection of events with particles interacting with the apparatus (off-line and second-level trigger) Characteristics: Plastic scintillator paddles, 8mm thick 4 upper (CARD), 1 top (CAT), 4 side (CAS) Performance: MIP efficiency > 99.9%

Neutron detector Main tasks: e/h discrimination at high-energy Characteristics: Main tasks: Neutron Detector trigger Characteristics: Plastic scintillator paddle, 1 cm thick Shower-tail catcher 36 3He counters: 3He(n,p)T Æ Ep=780 kev 1cm thick polyethylene Cd moderators n collected within 200 μs time-window

Design performance Energy range Particles/3 years Antiproton flux 80 MeV - 190 GeV >3x10 4 Positron flux 50 MeV 270 GeV >3x10 5 Electron flux up to 400 GeV 6x10 6 Proton flux up to 700 GeV 3x10 8 Electron/positron flux up to 2 TeV (from calorimeter) Light nuclei (up to Z=6) up to 200 GeV/n He/Be/C: 4 10 7/4/5 Antinuclei search Magnetic curvature (trigger) Spillover Sensitivity of 3x10-8 in He-bar/He EM shower containment Maximum Detectable Rigidity (MDR) Unprecedented statistics and new energy range for cosmic ray physics e.g. contemporary antiproton & positron energy, E max 40 GeV Simultaneous measurements of many species constrains secondary production models 1 HEAT-PBAR flight ~ 22.4 days PAMELA data 1 CAPRICE98 flight ~ 3.9 days PAMELA data

Resurs-DK1 Satellite Main task: multi-spectral remote sensing of earth s surface Built by TsSKB Progress in Samara (Russia) Lifetime >3 years (assisted) Data transmitted to ground via radio downlink PAMELA mounted inside a pressurized container Mass: 6.7 tonnes Height: 7.4 m Solar array area: 36 m 2

Gagarin - 12th April 1961

T 1 day

Launch: 15 th June 2006, 0800 UTC

PAMELA milestones Launch from Baikonur: June 15 th 2006, 0800 UTC. First light : June 21 st 2006, 0300 UTC. Detectors operated as expected after launch Different trigger and hardware configurations evaluated PAMELA in continuous data-taking mode since commissioning phase ended on July 11 th 2006 As of ~now: > 300 days of data taking (70% live-time) ~5.5 TByte of raw data downlinked ~610 million triggers recorded and under analysis

Orbit characteristics 350 km SAA 70.0 ο 610 km Quasi-polar (70.0 ) Elliptical (350 km - 600 km) PAMELA traverses the South Atlantic Anomaly At the South Pole PAMELA crosses the outer (electron) Van Allen belt Data downlinked to Moscow. ~15 GByte per day (2-3 sessions)

www.heavens-above.com above.com Next visible pass: Friday August 10th / ~0530

Hz

6.5 GV interacting proton

Preliminary!!! Polar regions p spectra @ different cut-off rigidities Equatorial regions

Preliminary!!! de/dx ~ Z 2 Galactic p and He spectra Z=1 Z=2 γ~2.76 γ~2.71

Antiparticle selection Preliminary!!! e - e p p, d [Momentum (GeV) / charge (e)]

Positron selection with calorimeter -ve -ve ~R m => 50% e - e - p-bar (non int.) p e - e - e - e - Preliminary!!! ve ve p (int.) e (e ) p (non int.) Fraction of charge released along the calorimeter track (left, hit, right) p e Fraction of charge released along the calorimeter track (left, hit, right) Example calorimeter selection criteria: Total energy release Longitudinal and lateral shower development Shower topology e p e e Fraction of charge released along the calorimeter track (left, hit, right)

18 GV non-interacting anti-proton

~41 GV interacting antiproton

1.09 GV positron

~70 GV positron

Summary PAMELA is conducting an indirect search for dark matter using antiparticles (e, p-bar) in the cosmic radiation. Launched on June 15th 2006. PAMELA has been in continuous data taking mode since 11th July 2006. ~5.5 TB of data downlinked, to date. Data analysis is on-going. First science results (probably antiparticle flux ratios) should appear before the end of this year. [http://wizard.roma2.infn.it/pamela]

The PAMELA Collaboration Italy: Bari Florence Frascati Naples Rome Trieste CNR, Florence Russia: Moscow St. Petersburg Germany: Siegen Sweden: KTH, Stockholm [http://wizard.roma2.infn.it/pamela]