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SSD Science Specification Table 14 keV - 250 keV for neutral particles 40 cm 2 image plane Electronic Noise 3 keV FWHM Proton Dead Layer <4 keV Focal Length.

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Presentation on theme: "SSD Science Specification Table 14 keV - 250 keV for neutral particles 40 cm 2 image plane Electronic Noise 3 keV FWHM Proton Dead Layer <4 keV Focal Length."— Presentation transcript:

1 SSD Science Specification Table 14 keV - 250 keV for neutral particles 40 cm 2 image plane Electronic Noise 3 keV FWHM Proton Dead Layer <4 keV Focal Length 6.16 to 6.95 cm FOV 40 degrees Pixel size 4 x 4 mm 256 Energy Levels (10 Bit A/D) Taylor UniversityHENA CDR July 9 &10 1997

2 Engineering Specification Table Sensors: XY Position Si solid state sensors –Two vendors used: Canberra and Micron Analog Electronics 240 A225 preamplifiers 15 ASIC amplifiers Total Power 3 Watts (at supply voltages) Voltages +/- 5 analog, +5 dig., and bias voltage (-70V) Planned Temperature Operation 0 o C + - 20 o C Survival Temperature: +60 o C to -50 o C Taylor UniversityHENA CDR July 9 & 10 1997

3 SENSOR SPECIFICATIONS MEASURES NEUTRALS E>14 keV 4 - 60 ELEMENT ARRAY (12 X 5) ACTIVE AREA: 48.7mm x 20.8mm per SSD THICKNESS: >200 MICRONS THIN WINDOW: <5 keV H+ ENERGY LOSS (Si) BIAS APPLIED TO THIN WINDOW SIDE OPPOSITE PIXELS LEAKAGE CURENT: <10nA ELECTRONIC NOISE RESOLUTION: <1KeV FWHM BOND PADS: 4 - 5 MILS BOND WIRES: < 1.25 MILS Taylor UniversityHENA CDR July 9 & 10 1997

4 SSD Design Features Parallel processing (240 channels) High resolution (240 pixel array @ 256 Energy levels) Adjustable Thresholds and Control Logic Low Power Single Box Assembly Taylor UniversityHENA CDR July 9 & 10 1997

5 Design Philosophy Use Existing Technology Use Well Proven Analog Gate Array Technology –High reliability, Parallel Processing, Low Power, and Low Complexity Rigorous Testing and Burn-In of Subsystems State-of-the-Art Instrument Taylor UniversityHENA CDR July 9 & 10 1997

6 System Design Taylor UniversityHENA CDR July 9 & 10 1997

7 SSD Detector Holder Rendering Taylor UniversityHENA CDR July 9 & 10 1997 SSD Metalized PC Card Shields Platform

8 SSD Mounting Assembly Taylor UniversityHENA CDR July 9 & 10 1997

9 SSD Detector Assembly Taylor UniversityHENA CDR July 9 & 10 1997

10 Shield Holder

11 Taylor UniversityHENA CDR July 9 & 10 1997 PC Board Shield

12 Taylor UniversityHENA CDR July 9 & 10 1997

13 PC Board

14 Taylor UniversityHENA CDR July 9 & 10 1997

15 Preamplifier Board Rendering Taylor UniversityHENA CDR July 9 & 10 1997 60 A225 Preamps 4 FEA Chips MDM Connector Flex Cable Connection Actel Chip

16 A225 Preamplifier Repackaging Taylor UniversityHENA CDR July 9 & 10 1997 A225 will be repackaged in A111F casing

17 HENA Middle Box Design Taylor UniversityHENA CDR July 9 & 10 1997

18 SSD Cap., Noise, Thickness Taylor UniversityHENA CDR July 9 & 10 1997

19 Pixel Angular Resolution from Center of Pin Hole Taylor UniversityHENA CDR July 9 & 10 1997

20 Ion Penetration in Silicon Standard Window N+ Side Enhanced Window N+ side Standard Window P+ junction Enhanced Window P+ junction Taylor UniversityHENA CDR July 9 & 10 1997

21 Detector Geometry

22 Taylor UniversityHENA CDR July 9 & 10 1997 Sensor Mount Finite Element Model C L PC Board Frame Sensor #1 Mount Sensor #2 Mount Nodes: 576 Size: 2.49E-2 x 10.21E-2 m Thickness: 12.7E-4 m

23 Vendor Response List Canberra Completed Design and Mask, In Fabrication, On Schedule Micron Completed Design, Mask started ~4 Weeks behind schedule Name of VendorStatus Taylor UniversityHENA CDR July 9 & 10 1997

24 FEA Microcircuit Heritage FEA Micro circuits –POLAR Satellite SEPS IPS PIXIE (Polar Ionospheric X-Ray Imaging Experiment) –SPADUS (flew on the Argos satellite) –MAXIE (Magnetospheric Atmosphere X-Ray Imaging Experiment) flew on Aug. 9, 1993 on the TIROS satellite. It measured x-rays in the range of 4 - 100 keV. Taylor UniversityHENA CDR July 9 & 10 1997 POLAR Satellite SEPS SPADUS

25 IMAGE Front-end Gate Array Features 16 amps - each has a calibration pulser input, low gain (proton mode) and high gain (electron mode) sections, and test outputs via a diagnostic MUX for each gain. 17 peak holding circuits -- 16 XY pixels and on E detector pixel. 16 electron mode comparators with individually adjustable thresholds 16 proton mode comparators with a common adjustable reference Micro computer data input to configure the chip. Logic disable gates for each pixel and each anti. Set-up latches (113 bits) to configure the chip Mode control latches. Coincidence logic with adjustable resolving time. Programmable anti coincidence logic including pile-up rejection Tri-state outputs controlled by a polling clock. Taylor UniversityHENA CDR July 9 & 10 1997

26 PHA/ Scaler Gate Array Features 16-channel stacked discriminator (log/linear) with programmable endpoints set by two 8-bit DACs Eight 16-bit scalers with overflow bits and buffers 16-bit computer bus interface Set-up latches (24 bits) State logic directs the collection and storage of spectra in a dedicated 8K x 8 RAM The RAM is organized as 4K 16-bit words Data router and increment logic accumulate up to 256 16-channel spectra Control logic to multiplex four front-end chips and isolate them from the computer bus 3-to-8 decoder with five external outputs Taylor UniversityHENA CDR July 9 & 10 1997

27 Block Diagram of PHA chip Taylor UniversityHENA CDR July 9 & 10 1997

28 I/O Gate Array Features 16-bit computer interface with 4-bit address decode Control registers (44 bits) Serial input/output with an 8-bit buffer Eight-bit counter/timer with an adjustable pre-divide Watch-dog timer for resetting microprocessor Digital-to-analog converter with a pulser mode Analog-to-digital converter with an eight-input MUX Dual eight-bit bi-directional parallel ports Vectored interrupt logic (five internal). The three external interupts may be edge or level triggered. Status register Crystal oscillator (generates computer clock) Power-on reset circuit Taylor UniversityHENA CDR July 9 & 10 1997

29 I/O Chip Block Diagram Taylor UniversityHENA CDR July 9 & 10 1997

30 A225 Characteristics Operation Temp: -55 o C to + 125 o C Operation Voltage: +4 to +25 VDC Sensitivity: 240 mv/Mev (Si) Noise: 2.4 Kev FWHM (Si) Noise Slope: 50 ev/pf (Si) Radiation Resistance: 10 5 Rads Input: 5 mV, 2  s Output: 175mV, 6  s Taylor UniversityHENA CDR July 9 & 10 1997

31 ASIC’s Amplifier Chain Schematic Taylor UniversityHENA CDR July 9 & 10 1997

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33 Main Electrical SSD Components Taylor UniversityHENA CDR July 9 & 10 1997

34 Interface Signals Taylor UniversityHENA CDR July 9 & 10 1997

35 Memory MAP Taylor UniversityHENA CDR July 9 & 10 1997

36 PHA Register Map Taylor UniversityHENA CDR July 9 & 10 1997

37 Front-End Register Map Taylor UniversityHENA CDR July 9 & 10 1997

38 IO Chip Register Map Taylor UniversityHENA CDR July 9 & 10 1997

39 Actel Chip Signals Win[0..14]Event windows, one from each FEA AntiEvent anti--on tri-state bus--poll FEA to activate PORPower-on reset--from I/O gate array CS*Chip select--from PHA decoder ALEAddress latch enable--from DPU WR*Write strobe--from DPU RD*Read strobe--from DPU (may not need) DPU[0..7]Time-of-flight data--from DPU CLK3.2 MHz clock--from I/O gate array Poll[0..14]Poll strobes--one to each FEA Pixel[0..7]Pixel/FEA ID register--to DPU and PHA CDPU[0..2]Compressed time-of-flight data--to RAM address bits A[13..15] RSTReset--to FEA gate arrays; only polled FEA will reset StartStarts PHA cycle EtrigEvent trigger--to DPU ACIEL ACT1 FPGA signals: AD[0..7]8-bit bi-directionaladdress/data bus Inputs: Outputs:

40 FE Chip Signals Taylor UniversityHENA CDR July 9 & 10 1997

41 PHA Signals Taylor UniversityHENA CDR July 9 & 10 1997


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