Satellite and balloon
borne experiments
F.S. Cafagna, INFN Bari
F.S. Cafagna, VI IFAE Napoli
1
Outline
F.S. Cafagna, VI IFAE Napoli
PAMELA
science overview
2
Outline
F.S. Cafagna, VI IFAE Napoli
PAMELA
science overview
3
Outline
F.S. Cafagna, VI IFAE Napoli
PAMELA
science overview
4
Outline
F.S. Cafagna, VI IFAE Napoli
PAMELA
science overview
5
Outline
F.S. Cafagna, VI IFAE Napoli
PAMELA
science overview
6
Outline
Balloon
experiments
Primary cosmic ray spectrum (inclusive)
Direct measurements of the energy spectra of
light nuclei in VHE cosmic rays (1012-1015 eV)
require a large collection-power.
BESS
ATIC
CREAM
VHCR
AMS-02
• Large calorimeters are too heavy.
• TRD’s cannot measure the energy
of protons and He nuclei.
We need a light-weight energy meter
Space-based
Composition
Ground
experiments
experiments
PAMELA
Courtesy of P. S. Marrocchesi - Univ. of Siena and INFN
F.S. Cafagna, VI IFAE Napoli
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The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
F.S. Cafagna, VI IFAE Napoli
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PAMELA prehistory
• Astromag/WiZard project (PAMELA precursor) on board of
the Space Station Freedom ÆCANCELED
• Balloon-borne experiments: MASS-89,91 TS-93 CAPRICE94,97,98
• Space experiments*: NINA-1,2 SILEYE-1,2,3 ALTEA
(*study of low energy nuclei and space radiation environment)
M 89
M 91
TS 93 C 94
C 97 C 98 NINA-1
NINA-2
1989 1990 1991 1992 1993 1994 1995 1996 1997 1998 1999 2000 2001 2002 2003 2004 2005 2006 2007
-ASTROMAG
---X
SILEYE-1
SILEYE-2
F.S. Cafagna, VI IFAE Napoli
SILEYE-3
ALTEA
9
The Resurs DK-1 spacecraft
•
Mass: 6.7 tons
Height: 7.4 m
Solar array area: 36 m2
Multi-spectral remote sensing of
earth’s surface
Æ near-real-time high-quality
images
• Built by the Space factory TsSKB
Progress in Samara (Russia)
• Operational orbit parameters:
• inclination ~70o
• altitude ~ 360-600 km
(elliptical)
• Active life >3 years
• Data transmitted via Very high•PAMELA mounted inside speed Radio Link (VRL)
a pressurized container
•moved from parking to
data-taking position few
times/year
F.S. Cafagna, VI IFAE Napoli
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PAMELA apparatus
GF: 21.5 cm2 sr
Mass: 470 kg
Size: 130x70x70 cm3
Power Budget: 360W
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PAMELA
The magnet
Characteristics:
•
•
•
•
•
5 modules of permanent magnet (NdB-Fe alloy) in aluminum mechanics
Cavity dimensions 162x132x445 cm3
Æ GF 21.5 cm2sr
Magnetic shields
5mm-step field-map
B=0.43 T (average along axis),
B=0.48 T (@center)
SPECTROMETER
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PAMELA
The tracking system
Main tasks:
•
•
•
Rigidity measurement
Sign of electric charge
dE/dx
Characteristics:
•
•
•
6 planes double-side (x&y view)
microstrip Si sensors
36864 channels
Dynamic range 10 MIP
•
•
Spatial resolution: 3-4μm
MDR ~1T (from test beam data)
Performances:
SPECTROMETER
F.S. Cafagna, VI IFAE Napoli
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PAMELA
The electromagnetic calorimeter
Main tasks:
•
•
e/h discrimination
e+/- energy measurement
•
•
•
•
•
44 Si layers (X/Y) +22 W planes
16.3 Xo / 0.6 l0
4224 channels
Dynamic range 1400 mip
Self-trigger mode (> 300 GeV GF~600 cm2 sr)
Characteristics:
Performances:
•
•
•
•
p-bar and e+ selection efficienecy ~ 90%
p rejection factor >105
e- rejection factor > 104
Energy resolution ~5% @200GeV
SPECTROMETER
CALORIMETER
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PAMELA
S1
S2
S3
SPECTROMETER
CALORIMETER
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PAMELA
The time-of-flight system
S1
S2
Main tasks:
•
•
•
•
First-level trigger
Albedo rejection
dE/dx
Particle identification (<1GeV/c)
•
•
•
3 double-layer scintillator
paddles
X/Y segmentation
Total: 48 Channels
•
•
σpaddle ~ 110ps
σTOF ~ 330ps (for MIPs)
Characteristics:
Performances:
S3
SPECTROMETER
CALORIMETER
F.S. Cafagna, VI IFAE Napoli
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PAMELA
The anticounter shields
CARD
Main tasks:
•
S1
Rejection of events with particles
interacting with the apparatus
(off-line and second-level
trigger)
Characteristics:
CAT
S2
CAS
•
•
scintillator paddles 10mm thick
4 up (CARD), 1 top (CAT), 4 side
(CAS)
Performances:
•
Efficiency > 99.9%
S3
SPECTROMETER
CALORIMETER
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PAMELA
Shower-tail catcher (S4)
CARD
Main tasks:
• ND trigger
Characteristics:
• 1 scintillator paddle
10mm thick
S1
CAT
S2
Neutron detector
Main tasks:
CAS
•
e/h discrimination @high-energy
•
36 3He counters:
Characteristics:
•
•
S3
3He(n,p)T
Æ Ep=780 keV
1cm thick polyetilene moderators
n collected within 200 μs timewindow
S4
NEUTRON DETECTOR
SPECTROMETER
CALORIMETER
F.S. Cafagna, VI IFAE Napoli
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PAMELA: the integration
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PAMELA in the satellite
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The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESSPOLAR
F.S. Cafagna, VI IFAE Napoli
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Progress of BESS Experiment
1993~ 2000, BESS, North Canada
2002, BESS-TeV
1999, 2001, BESS-Ground, Japan
2001, BESS-TeV, Fort Sumner
2004, BESS-Polar I, Antarctica
10 scientific balloon flights during1993-2004
See. Yamamoto @ crheu07
F.S. Cafagna, VI IFAE Napoli
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BESS Detector
–Rigidity
–
measurement
SC Solenoid (L=1m, B=1T)
JET/IDC
Rigidity
– Min. material (4.7g/cm2)
–
–
Uniform field
Large acceptance
–Central
–
–
tracker
(Drift chamber
δ ~200μm
TOF
β, dE/dx
–
Z, m measurement
–
R,β --> m = ZeR
√ 1/β2-1
–
dE/dx --> Z
See. Yamamoto @ crheu07
F.S. Cafagna, VI IFAE Napoli
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BESS-TeV Upgrade
2001~2002
–Central Tracker
– (JET/IDC)
improvement
BESS-TeV
BESS-98
–δ = 200 -->150 μm
– N = 28 --> 52
–New detector
– (ODC) installed
– L = 0.8 --> 1.6
–MDR:
–200 GV
m
ODC
JET/IDC
ODC
See. Yamamoto @ crheu07
--> 1400 GV
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BESS-TeV Deflection Resolution
MDR 1.4 TV
BESS-98
MDR 200 GV
See. Yamamoto @ crheu07
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BESS-TeV Spectrometer
TOF
ODC
MAGNET
JET/IDC
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Feature of BESS-Polar Spectrometer
BESS-2000
BESS-Polar
TOF Upper
Coil
18g/cm2
5g/cm2
10g/cm2
JET/IDC
MTOF
ACC
TOF Lower
Incident Particles
Minimize material in spectrometer
New detector (Middle TOF)
Energy range extended down to
0.1 GeV
Low power electronics
Solar Power System, LongerF.S.
lifeCafagna,
of cryogen,
VI IFAELHe
Napoli
See. Yamamoto @ crheu07
Long duration flight
27
BESS-Polar 2004
●
●
●
8.5 day flight successful
35-37 km in altitude
900 million events recorded
Altitude~38000m
Residual air~4g/cm2
Floating
F.S. Cafagna, VI IFAE Napoli
See. Yamamoto @ crheu07
28
The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESSPOLAR
• AMS
• AMS1 (AMS98), AMS2
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AMS1
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AMS: General
• ISS : 108 x 80m, 420 t ,
400km
• Inclination = 51.57 o
• 15.62 revolutions/day
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AMS: General
• TRD (e/p)
• Scintillator system (TOF)
(β, dE/dx, trigger)
• Superconducting magnet
(BL2= 0.85 Tm2)
• Silicon Tracker (rigidity,
charge)
• RICH (β, charge)
• Em. Calorimeter(energy, e/p
Rigidity meas.
Particle ident.
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AMS: General
≈3m
ƒ Large geometrical
acceptance: 0.45 m2 sr
ƒ Long exposure: 3 years
ƒ Redundant measurements
≈3m • High vacuum
• High radiation levels
• Strong gradients of
temperature : -60°C ÷
+40°C
• Weight < 7 Tons
• Power consumption < 3kW
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Superconducting Magnet
racetrack coils
dipole coils
B
B
Superfluid He Vessel
Chan Hoon Chung, RWTH-Aachen, Germany
Diameter = 1.2 m, Height = 0.8 m, Weight = 2.3 t
Bdipol = 0.860 [T], Estored = 1.15 MJ, I = 459.5[A]
Cold Heat Exchanger : Superfluid Helium
(-271.35o, 2500 l)
Long Duration Operation without refill
34/23
AMS: Tracker
ƒ
ƒ
ƒ
ƒ
ƒ
ƒ
ƒ
2264 Double sided Silicon
wafers
640 readout strips on
implantation or p-side
(bending coordinate)
384 readout strips on
junction or n-side
(non-bending coordinate)
Combined into 192 Ladders
of 7-15 sensors
1024 readout channels for
each ladder, total of ~ 200k
channels
Ladders arranged on 8
layers piled up in 5 planes
~ 6.4m2 total
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ToF & ACC
Chan Hoon Chung, RWTH-Aachen, Germany
Anti-Coincidence Counter
Upper ToF
Lower ToF
Fast Triggerprim
σt ≤ 130 [ps]
Layers = 4 (2 + 2)
Area = 8 m2
ToF : 34 Paddles
ACC
: 16Napoli
Cylindrical Shell Paddles 36
F.S. Cafagna,
VI IFAE
36/23
AMS: Em. Calo.
ƒ 9 Superlayers (Pb + Fiber
Sandwich)
ƒ 16.4 Xo and ~ 0.5 λnucl.
ƒ Standalone Gamma Trigger
ƒ 65×65 cm2, m= 640 kg, 324 PMTs
e±
ΔE/E ~3% @ 100GeV e-
p
Lead foil (t:1mm)
Fibers (φ:1mm)
Superlayers
F.S. Cafagna, 3/9
VI IFAE
Napoli
Hamamatsu
fine mesh37PMT
AMS: TRD
ƒ 2.2x 2.2x0.8 m3 , 350 kg, 20
layers of straw tubes. Radiator: 2
cm polyethylene/ polypropylene 10
mm fibre fleece. Gas mixture is
Xe:CO2 80:20% (1 bar), 8100l
ƒ Conical octagon structure made of
aluminum honeycomb with carbonfibre skins and bulkheads
ƒ Mechanical precision: 100 mm to
assure gas gain homogeneity
below 2%
ƒ 4 lower and upper oriented parallel
to the magnetic field, middle 12
perpendicular to it, for 3D tracking
Cafagna, VI IFAE Napoli
One of 328 StrawF.S.
Modules
38
AMS: Rich
Radiator (Aerogel and NaF) Cerenkov
Cone
Mirror
θc
cosθc = 1/(βn)
PMTs Array
ƒ Rad. NaF(n=1.336) in central region
and Aerogel (n=1.035) elsewhere
ƒ 680 PMT's Array, Spatial Pixel
8.5×8.5 mm2
ƒ Velocity Res.: Δβ/β ≃ 0.07 % (Z=1)
ƒ Charge Measurement: Z ≤ 26 (w/
Tracker + ToF)
ƒ Charge Nγ ∝ Z2 ∆L (1 - (βn)-2 )
ƒ Mass: m(β,Z,R) = RZe sqrt(1- β2)/ βc
F.S. Cafagna, VI IFAE Napoli
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The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESSPOLAR
• AMS
• AMS1 (AMS98), AMS2
• CREAM
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CREAM
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See. Seo @ crheu07
CREAM
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CREAM
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See. Seo @ crheu07
CREAM
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See. Seo @ crheu07
The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESSPOLAR
• AMS
• AMS1 (AMS98), AMS2
• CREAM
• ATIC
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ATIC
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See. Wefel @ crheu07
ATIC
F.S. Cafagna, VI IFAE Napoli
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See. Wefel @ crheu07
ATIC
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See. Wefel @ crheu07
The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESS-POLAR
• AMS
• AMS1 (AMS98), AMS2
• CREAM
• ATIC
• TRACER
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TRACER
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TRACER
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TRACER
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52
The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESS-POLAR
• AMS
•
•
•
•
•
• AMS1 (AMS98), AMS2
CREAM
ATIC
TRACER
JACEE
RUNJOB
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Primaries
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Primaries
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Primaries
Error: < +/-5 %
@ 100 GeV
Sanuki et al. ApJ. 545 (2000) 1135
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Primaries
Error: < +/-15 %
@ 500 GeV
Haino et al. PLB 594 (2004) 35
See. Yamamoto @ crheu07
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Primaries
See. Yamamoyo @ crheu07
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ATIC
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ATIC
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ATIC - TRACER
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PAMELA DATA
PAMELA
PRELIMINARY !!!!
Z=1
Z=2
γ~2.76
γ~2.71
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PAMELA DATA
PAMELA
PRELIMINARY !!!!
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PAMELA DATA
PAMELA
PRELIMINARY !!!!
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Why Anti(particle)matter matters?
Earth
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Spectra modification
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Here is the status: flux
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Here is the status: ratio
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The positron charge ratio
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Where is the focus ?
Larger statistic
is needed at E>10 GeV
Absolute fluxes
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Here is the status: ratio
Very good
F.S. Cafagna, VI IFAE Napoli
particle identification
71
PAMELA
PAMELA
PRELIMINARY !!!!
4He
B,C
3He
d
Be
p
Li
e+
Tracker dE/dx
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72
PAMELA
Calorimeter dE/dx (first Si-layer)
O
N
C
B
Be
Li
PAMELA
PRELIMINARY !!!!
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PAMELA
PAMELA
PRELIMINARY !!!!
Fraction of charge released along the track
p-bar
(non int.)
e-
e-
p
p
(int.)
(non int.)
(e+)
e+
Many selection criteria provided by the calorimeter:
• total energy release
• longitudinal and later shower development
• shower topology
•…
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18 GV
non-interacting anti-proton
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11.6 GV
interacting anti-proton
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32.3 GV positron
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The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESS-POLAR
• AMS
• AMS1 (AMS98), AMS2
• CREAM
• ATIC
• GLAST
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GLAST
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GLAST
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GLAST
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GLAST
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GLAST
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GLAST
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GLAST
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The Experiments
• WIZARD
• MASS89, MASS91, TS93, CAPRICE 94, CAPRICE 98
• NINA1, NINA2, Si-EYE, PAMELA
• BESS
• BESS93 ÷ BESS00, BESS-GROUND,BESS-TeV, BESS-POLAR
• AMS
• AMS1 (AMS98), AMS2
•
•
•
•
CREAM
ATIC
GLAST
AGILE
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AGILE
• The AGILE satellite in the Shriharikota
clean room (April 1, 2007)
• Launch scheduled 23 April 2007
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AGILE
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AGILE
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AGILE
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Future experiments
•
•
•
•
Nucleon
CALET
JEM-EUSO
EUSO ?
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NUCLEON : direct measurements of the elemental energy spectra of
1012-1015 eV cosmic rays aboard a Russian satellite.
The NUCLEON device includes :
• charge measuring system
• tracker and energy measuring system
(KLEM device),
• trigger system
• control electronics
The charge measuring system consists of 4 silicon detectors layers.
The tracker and energy measuring system consists of a carbon target 50×50×9
сm3, 6 identical layers of micro-strip silicon detectors, 2 tungsten layers
50×50×0.7 сm3 as gamma-converter.
The trigger system (SC1-SC6) consists of three double layer 16-strip scintillator
3) with 1 mm WLS fibers.
detectors (size ~ 500×30×0.5 mm
F.S. Cafagna,
VI IFAE Napoli
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Expected exposure in 5 years :
NUCLEON :
~ 170 m2 sr days for protons
- Weight < 165 kg
- Power consumption < 120 W
~ 460 m2 sr days for Fe nuclei
- nominal telemetry : 270 MB per day
- time in orbit ≥ 5 years
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CALET: CALorimetric Electron Telescope
CALET Mission Concept
zInstrument:
High Energy Electron and Gamma-Ray
Telescope Consisted of
- Imaging Calorimeter (IMC)
- Total Absorption Calorimeter (TASC)
zLaunch:
HTV: H-IIA Transfer Vehicle
zAttach Point on the ISS:
Exposed Facility of Japanese Experiment
Module (JEM-EF)
zNominal Orbit:
407 km, 51.6o inclination
zLife Time:
3 years (minimum)
zMission Status
Mission Concept Study
Launch around 2013 in Plan
See. Torii @ crheu07
CALET Payload:
・ 1GeV ~ 10 TeV for electrons
・ 20 MeV ~ TeV for gamma-rays
+ Gamma-ray bursts in 7 keV~20 MeV
・ several 10 GeV ~ 1000 TeV for nuclei
・ Weight: 2000 kg
・ Geometrical Factor: ~0.75 m2sr
・ Power Consumption: 640 W
・ Data Rate: 300 kbps
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Conceptual Structure of CALET
Requirements:
¾ Large Acceptance: ~1
sr
¾ Imaging Capability: < 1mm
¾ Hadron Rejection Power: >105
¾ Energy Measurement:
20 MeV~10 TeV for e, γ
several 10 GeV ~ 1000 TeV for hadrons
m2
Schematic Side View of CALET
・Anti-Coincidence Detector for Low E. γ
・Silicon Array for High Z and Particle ID
Detector Weight: 1450 kg
Total Absorber Thickness: 32 r.l, ~1.7m.f.p
SciFi/W Imaging Calorimeter (IMC):
¾ Area: ~ 0.8 m2
¾ SciFi Belt: 1mm square x ~1 m length
17 layers (x &y)
¾Tungsten Thickness: 4 r.l , 0.15 m.f.p
Total Absorption Calorimeter (TASC):
¾ Area: ~0.36 m2
¾ BGO Log: 25 x 25 x 300 mm
6 layers (x & y)
¾ Thickness: 28 r.l , 1. 5 m.f.p
See. Torii @ crheu07
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Schematic Structure of CALET
GBM
アンチコインシデ
ンスディテクタ
(ACD))
ACD
VSC
MDP
シリコンアレイ
(SIA)
SIA
イメージング
カロリーメータ
(IMC)
IMC
トータルアブソープ
ションカロリーメータ
(TASC)
TASC
See. Torii @ crheu07
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Scarica

pamela - Indico