roberta sparvoli for the pamela collaboration

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Roberta Sparvoli Roberta Sparvoli for the PAMELA Collaboration University of Rome Tor Vergata and INFN Roma II, Italy Uuuuuu Uuuu uuuuuuu

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Uuuuuu Uuuu uuuuuuu. Roberta Sparvoli for the PAMELA Collaboration University of Rome Tor Vergata and INFN Roma II, Italy. PAMELA scientific program. - PowerPoint PPT Presentation

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Page 1: Roberta Sparvoli for the PAMELA Collaboration

Roberta SparvoliRoberta Sparvoli for the PAMELA Collaboration

University of Rome Tor Vergata and INFN Roma II, Italy

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Page 2: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 22

PAMELA PAMELA scientific programscientific program

energy range particles/3 years

Antiproton flux 80 MeV - 190 GeV >3 104

Positron flux 50 MeV – 270 GeV >3 105

Electron flux up to 400 GeV 6 106

Proton flux up to 700 GeV 3 108

Electron/positron flux up to 2 TeV

Light Nuclei (up to Z=6) up to 200 GeV/n He/Be/C: 4 107/4/5

AntiNuclei search (sensitivity of 3 10-8 in He/He)

Unprecedented Statistics and new Energy Range in

Cosmic Rays

Actual limits: antip&positrons 40 GeV

PAMELA is a magnetic spectrometer which will fly on a Russian satellite by Fall 2005. Its scientific scope is the measurement of the antiproton and positron spectra up to few hundred GeV, of the proton and electron spectra up to 700 GeV and that of light nuclei.

Page 3: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 44

What is PAMELA now?What is PAMELA now?

Flight Model – Munich, Jan 2005

Page 4: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 55

Mass&Thermal Model in TsSKB Pressurized Container

Mass & Thermal Model Mass & Thermal Model PAMELA Mass & Thermal Model was assembled in the clean room of Rome Tor Vergata (2001-2002) and then integrated into the Pressurized Container at TsSKB-Progress (Samara/Russia), between March 2002 and April 2003, for all mechanical compatibility tests. It passed thermal and dynamical qualification tests.

Integration in the Container

Page 5: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 66

PAMELA Technological Model was assembled and tested (preliminary Acceptance Tests with EGSE: power ON/OFF, telecommands, data transmission through adapter) in the clean room of Rome Tor Vergata in 2003-2004.

Technological Model Technological Model

It was then shipped to Samara inside a special transport container in April 2004. Magnetic compatibility tests and Incoming Tests (stand-alone) already performed. Integration with satellite and transmission to mass memory still in progress (Jan 2005).

Page 6: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 77

Flight Model Integration Flight Model Integration The final Flight Model integration is in progress in Rome clean room since almost 12 months. All flight components have been mounted. From 16/02/2005 a Russian delegation is in Rome for official Acceptance tests of PAMELA FM before delivery to Samara.

PAMELA-FM inside Transport Container

Design: > 5000 km flight & 1000 km rail, +40/-50°C outside

Page 7: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 88

Beam testsBeam tests

SPS, July 2000

SPS, July 2002

Magnet/Tracker,Calorimeter

SPS, September 2003

From July 2000 until September 2003 PAMELA Flight Model was extensively exposed to beam tests to study physical performance.Detectors operated at CERN PS/SPS test beams as prototypes and in FM configuration. Final test in Sept. 2003.

Page 8: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 99

Dynamic testsDynamic tests

Risposta ricerca di risonanza asse Z per accelerometro MP 14 (montante)

PAMELA FM Model passed a cycle of vibration tests at IABG/Munich (January 2005) to verify the final structure. Minimal loads have been imposed to the instrument. 100 channels were mounted.

All resonance searches confirm the integrity of the detector after the test.

Page 9: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 1010

Cosmic ray tracks (Dec. 2004)Cosmic ray tracks (Dec. 2004)

Since November 2004 PAMELA is set in cosmic-ray acquisition during night shifts.

Page 10: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 1111

First “physics” resultsFirst “physics” results

From the statistics acquired by cosmic-ray acquisitions we are analyzing PAMELA performance and comparing with literature.

Page 11: Roberta Sparvoli for the PAMELA Collaboration

R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 R. Sparvoli - INFN-SPAZIO/2 - LNF, 16 Febbraio 2005 1212

ConclusionsConclusions – already done – already done

(0) Detectors and Systems are designed & ready

(1) MASS & THERMAL MODEL done All tests passed space qualification!

(2) TECHNOLOGICAL MODEL ~ done Assembly finished in Rome (~ 1 yr) Integration with satellite in Samara almost complete

(started 05/2004)

(3) FLIGHT MODEL SPS BeamTest of almost complete setup done in Sept. 2003

for final calibration & alignment done Vibration Test (minimal loads) of complete setup for final check of structure – Munich (Jan. 2004) done

Page 12: Roberta Sparvoli for the PAMELA Collaboration

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Conclusions – to be doneConclusions – to be done

The PAMELA launch is in Fall 2005

FLIGHT MODEL Acceptance tests to be performed (end by 23 Feb.

2005) Cosmic-ray acquisition (long run) (end by 10 March 2005) Transport to Samara – Russia (March 2005) Full integration of PAMELA, ARINA & EOS into satellite

(April 2005) Tests in Samara – Russia (up to 3 months) All final tests in-situ - Baikonur/Kazahstan (2 – 3 months)