(Space WEATher Ena Radiation Sensor) · 2019. 7. 3. · Longitudinal range vs Pressure •Low...
Transcript of (Space WEATher Ena Radiation Sensor) · 2019. 7. 3. · Longitudinal range vs Pressure •Low...
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SWEATERS Activity Proposal(Space WEATher Ena Radiation Sensor)
An innovative Micro Pattern Gas Detector (MPGD) for Energetic Neutral Atoms (ENA) detection in the 1-100 KeV energy range
INFN Sezione di Pisa – CSN5
F.Pilo
103/07/2019
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Why ENA investigation
• Energetic Neutral Atom (ENA) imaging is a powerful techniquefor planetary environment studies
• ENA which arise from the charge-exchange process between cold geocoronal neutral hydrogen and the local energetic ion populations provide info about the magnetospheric plasma global dynamics
• Possible progresses in Space Weather predictions
(E. De Angelis/S. Orsini seminar @INFN Pisa - 18/06/2019)
• We propose an INNOVATIVE instrument for ENA detection, using well established HEP technologies in an innovative configuration
203/07/2019NASA Mission - Interstellar Boundary Explorer (IBEX)
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• Standard ENA instruments are classified according to the investigated Energy range: a unique detection technique for the entire ENA energy range does NOT exist
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ENA detectors – State of the art
03/07/2019
LENA(Low Energetic
Neutral Atom)
few eV – 1 keV
MENA1 keV – 30 keV
HENA30 keV – hundreds of keV
• It is possible to get a good compromise in mass, energy and angular resolution by using well-known techiniques, like CarbonFoil and 2-D detectors (MCP and SSD) installed in a TOF device
• Mass → Time of Flight (ToF) =L/v; E=1/2mv2
• Energy → ElectrostaBc Analyser or SSD
• Direction → Collimator-Position detection
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• Nice to have to match the physics goal
• New detector design should aim to an high "Technology Readiness Level" (TRL) (e.g. ≥ 4 – “Component and/or breadboard functional verification in laboratory environment”)
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Central FoV Pointing zenith
Field-of-view (FOV) 90° polar x 90° azimuth
FoV res. 5° x 5°
Energy range 1-100 keV
Energy resolution 20%
Particle flux 102 – 105 ENAs/(cm2 s sr)
Mass channels H, He, N, O discrimination
ENA detectors – Performances
03/07/2019
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• Neutral atoms are ionized at the detector entrance window equipped with a carbon foil
• The ion is detected and stopped within a detection gas volume
• Electrons from ionization are drifted toward a 2D-readout plane
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Electrons from gas
ionization
Drifted Electrons
Impinging ENA
Edrift
Read-out plane
Entrance Window
wiht CARBON FOIL
A new micro-pattern gas detector (MPGD) for ENA detection
Basically a Homogeneous 3D-Imaging Gas Calorimeter for
neutral particles
03/07/2019
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Neutral atom ion conversion
• Carbon foils are a robust and proven technology for ion and neutral atom detection in space
• Typical thickness: 0.5–3.5 μg·cm−2 or ∼2–17 nm
• Conversion efficiency: H 30%, O 20% ... energy dependent
• Scattering and Energy straggling reducedin ultrathin foils
• HERITAGE: great experience from INAF/IAPS detector construction
• Graphene? Is a promising solution to minimize scatteringand straggling https://techport.nasa.gov/view/94407
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pic
03/07/2019
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Longitudinal range vs Pressure
• Low pressure is required to stretch the particle tracks
7
0,01
0,1
1
10
100
0 20 40 60 80 100 120
Ra
ng
e [
mm
]
Ekin [keV]
Longitudinal range - H+ in Pure argon gas
O, 1013 mbar
O, 350 mbar
O, 13 mbar
H, 1013 mbar
H, 350 mbar
H, 13 mbar
03/07/2019
SRIM – Proton of 5keV in pure Argon 10mmHg
• a 100 mm-depth chamber can contain all tracks at O(10) mbar pressure
• Some advantages in design: drastically reduces the constraints in the design of the space-qualified detector; helps in case of entrance window defects (pinholes and tears)
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3D track reconstruction
• Position (X,Y) of the impact point at the read-out plane of each drifted electron is measured with high precision using micro-strip or pixel-shaped electrodes (sub-mm pitches)
• Z coordinate is reconstructed from the arrival time measurement using the electron drift velocity (µTPC)
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The electron drift velocity as extracted from Garfield SIM
SIMULATION
03/07/2019MAMMA collaboration, M. Iodice, Performance studies of Micromegas for
the ATLAS experiment, 2014 JINST 9C01017
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Energy measurement
• ENA tracks must be completely contained in the detector volume
• Good energy resolution at requested energy has been already proven e.g. by MIMAC Collaboration (Santos et al. 2011) with MicroMegasdetectors
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Mean energy resolution: ~ 15%
03/07/2019
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Particle identification
• Good level of H vs O discrimination is obtained measuring track length as a function of kinetic energy
10
0,01
0,1
1
10
100
0 20 40 60 80 100 120
Ra
ng
e [
mm
]
Ekin [keV]
Longitudinal range vs Kinetic Energy
O, 13 mbar
H, 13 mbar
03/07/2019
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Experimental tests
• Dedicated MC simulation has been developed using standard HEP software (Geant4, Garfield)
• At relatively low energies, simulation parameters MUST be validated with a dedicated MEASUREMENT CAMPAIGN
1103/07/2019
• Main components for test-beam setup already available• Ion Beam gun / vacuum chamber INAF/IAPS Rome
• Micromegas detector (MPGD) INFN
• Readout electronics 1 channel
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Micromegas with 192 um gap: first characterization @ CERN
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Test Bench @INFN Pisa
DAQ System
Preamplifier (CAEN A1422 – Charge sensitive)
Oscilloscope used as MCA
PicoAmmeter – Keithley ....
CAEN 2-Ch HV Supply
03/07/2019 13
55Fe X-rays source
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Test Bench @INFN Pisa
Support Gas System
03/07/2019 14
40l Volume
MPGD
MFC
MFC
P
Ar
C
O2
Rotameter
Vacuometer
Vacuometer
Ultra low-cost vacuometer!
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Test Bench @ INFN Pisa
Detector gain vs Amplification field & gas Pressure
03/07/2019
1,00E+02
1,00E+03
1,00E+04
200 250 300 350 400 450 500 550 600
Ga
in
Resistive strip Supply Voltage [V]
MM GAIN vs Voltage (192 um gap)
stdP
100mbarP
40mbarP
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Test activity already started @ INAF/IAPS
03/07/2019 16
Ion-ENA beam Lab @INFN/IAPS-Rome
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Project workplan• Main goal: 2 years R&D to build a full detector prototype
with performances compliant with specs.
• Permanent test setup @ INAF/IAPS with low energy neutral/charged atoms beam
1703/07/2019
Task name Duration
(month)
Responsible
Micromegas full characterization with charged ions 3 INFN
Micromegas performances evaluation with TB data
and MC (full DAQ required)
3 INFN
New gas cell and readout system design 5 INFN
Detector window design and test 6 INFN/INAF
Readout system production and test 6 INFN
Detector full test and characterization with ENA 6 INFN
2019/2020
2020/2021
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Involved INFN personnel
1803/07/2019
Name Role Workload
Percentage [%]
R. Carosi Researcher 20
R. Dell’Orso Researcher 0
F. Frasconi Researcher 20
M. Massa Technologist T.B.D.
A. Moggi Technologist 20
F. Morsani Technologist 40
F. Pilo Researcher 60
A. Terreni Technologist 40
TOTAL 200
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Budget requests
• Equipment – 20k
• Full CERN SRS system for Micromegas DAQ – 7k
• Very high precision HV Power Supply - 7k
• New MPGD procurement (from CERN?) - 4k
• Read-out system prototypes - 2k
• Consumables – 5k
• Mechanical/gas system for TB activities
• Travel
ITALY – 80 days
CERN/other countries – 10 days
1903/07/2019
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Requests to INFN Pisa
• Servizio Alte Tecnologie: 60 days – Gas system development, metrology and detector assembly activities (@Pisa), TB activities support (@Rome)
• Servizio Elettronico: 60 days – Detector electronics design/testing (@Pisa), TB activities support (@Rome)
• Servizio Officina Meccanica: 20 days – Frames&tools for TB testing activities (@Pisa&Rome)
• Common spaces: ½ OCRA/EEE laboratory (test bench already installed inside)
2003/07/2019
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Conclusions
• We propose an INNOVATIVE instrument for ENA detection, using well established HEP technologies in an innovative configuration
• ENA can be detected using a micro-pattern gas detector with 3D imaging capability
• simple, compact and robust device
• all the information from a single device
• Freedom in the choice of detector working conditions to match requested performances
• Drift field intensity, Detector depth and window size, Gas pressure and mixture, Multiplication stage
2103/07/2019