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University of California - Berkeley

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Presentation on theme: "University of California - Berkeley"— Presentation transcript:

1 University of California - Berkeley
THEMIS SCIENCE WORKING TEAM MEETING SST Davin Larson University of California - Berkeley

2 Overview Overview Instrument Description Instrument Design Data Modes
Data Warnings/Pitfalls

3 Instrument Description
Solid State Telescopes: Measure Energetic Electrons and Ions Energy Range: H+: 25 keV to 6 MeV Electrons 25 keV to ~800 keV Angular Coverage: Theta 4 look directions (+55, +25, -25, -55) Resolution: ~ 30 deg FWHM Phi 32 sectors Resolution: ~20 deg FWHM Geometric Factor: ~0.1 cm2-ster (~1/3 of WIND) Mechanical Pinhole Attenuator: Lowers geometric factor by 150

4 Sensor Unit Schematic Foil Detector Al/Polyamide/Al Foil
Thick Detector Open Detector Foil Collimator Open Collimator Attenuator Attenuator Sm-Co Magnet

5 Sensor Cross Section Each sensor unit is a:
Dual-double ended solid state telescope Each double ended telescope (1/2 sensor) has: Open collimator Pinhole attenuator paddle Reduces count rate during periods of high flux Reduces radiation damage from intense fluxes of low energy ions Magnet (Open side) Filters out electrons <400 keV Leaves ion flux nearly unchanged Triplet stack of SSDs DFE board Preamp / shaping electronics Thin Polyamide Foil Filters out ions <~350 keV Leaves electron flux nearly unchanged Another attenuator paddle Foil Collimator

6 (Data Acquisition & Processing)
Block Diagram IDPU Sensor Unit 1 (2 DFEs A&B) ~2 m cable (x2) DAP Board (Data Acquisition & Processing) Sensor Unit 2 (2 DFEs A&B) ETC Board DCB Heater Power SMA Power & Backplane DFE = Detector Front End PCB (Power Control Board) SST Instrument: 2 Sensors with attenuators (4 DFEs) 2 Cable bundles 1 DAP Board (inside IDPU) Other Boards

7 SST Mechanical Design Detector Board Composition (exploded view)
DFE Board Subassembly BeCu Gasket (3) Detectors (4) KaptonHeater Spring Clamp PEEK Spacer (4) Spring Plate (2) Kapton Flex-Circuit (4) AMPTEK Shield Thermostat Detector Board Composition (exploded view)

8 DFE Board Subassembly Relative Positions
SST Mechanical Design DFE Board Subassembly Relative Positions (2 per sensor) Detector Stack Subassembly Foil Frame Multi-Layer Circuit Board (62 mil thickness) AMPTEK Shielding Thermostat

9 Sm-Co Magnet (4) (currently not visible)
SST Mechanical Design Magnet-Yoke Assembly Co-Fe Yoke (2) Sm-Co Magnet (4) (currently not visible) Aluminum Magnet Cage

10 SST Mechanical Design Attenuator Assembly SMA Lever (2) Attenuator (4)
Cam (2)

11 Honeywell SPDT Hermetically Sealed Switch (2)
SST Mechanical Design Actuators and Position Switches Honeywell SPDT Hermetically Sealed Switch (2) SMA Actuator (2)

12 SST Mechanical Design Support Structure (front section)
Rigid Mounting Flange Kinematic Flexure (2)

13 Bi-Directional Fields-of-View
SST Mechanical Design A-Open (ion) B-Foil (electron) Bi-Directional Fields-of-View A-Foil (electron) B-Open (ion)

14 SST Mechanical Design SST-1 SST-2
Sensor Orientation Relative to Spacecraft Bus SST-1 SST-2

15 Attenuator Actuation – CLOSED position
SST Mechanical Design Attenuator Actuation – CLOSED position Honeywell Switch (compressed-position) Honeywell Switch (extended-position) SMA Actuator (retracted) SMA Actuator (extended)

16 Attenuator Actuation – OPEN position
SST Mechanical Design Attenuator Actuation – OPEN position Honeywell Switch (extended-position) Honeywell Switch (compressed-position) SMA Actuator (extended) SMA Actuator (retracted)

17 SST Sensor Mass Summary: Sensor mass= 553.5 gm
Cable mass (173 cm) = 141 gm Total x2= 1389 gm

18 Detectors stacked in “Triplet” sequence:
Detector System Detectors stacked in “Triplet” sequence: Foil (F) | Thick (T) | Open (O) Area used  0.7 cm2 Front detectors F and O are 300 m thick while T is 600 m (with two detectors back to back) Detectors associated with a system of coincidence/anticoincidence logic F T O

19 Monte-Carlo simulation
Telescope Response Monte-Carlo simulation 3D ray tracings are performed: a clean electron-proton separation is obtained Particles’ angular distributions are determined ( 27  14 FWHM) Efficiency plots of the electron-proton detectors are determined for different energies

20 Calibration results Typical Proton response SST Sensor 05 - Channel 4
35 40 45 keV 30

21 Intrument Configuration
Instrument Configuration The SST Energy bins are controlled by DAP table. Can be reconfigured with table upload. Precision: 6 MeV/4096 = 1.5 keV Log spaced Only 1 mode currently defined. The SST 3D (angular) distributions are binned by ETC angle map. 5 angle maps defined: 1 angle (omni) 6 angle (RDF) 32 angle 64 angle (burst, FDF) 128 angle

22


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