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The PFA focal plane camera
Jiang WeiChun (IHEP) on behalf of the eXTP–PFA Consortium
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OUTLINE Top Level Requirements PFA Focal Plan Design
PFA Assembly and Integration PFA Calibration
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OUTLINE Top Level Requirements PFA Focal Plan Design
PFA Assembly and Integration PFA Calibration
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PFA instrumental requirements
Item Requirement Goal Energy range 2-10keV Effective area(for 4 PFAs) Energy resolution Field of view (FWHM) 7.9 arcmin (limited by detector size) Angular resolution 30 arcsec (HPD) 15 arcsec(HPD) Point source localization TBC TBC Time resolution <500 μs <100 μs Dead time Background MDP (minimum detectable polarization) <3% <2% Maximum source flux (steady, peak) >0.5Crab, >5 Crab upto 24 houres >1Crab, >20 Crab upto 12 houres
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PFA functional requirements
Functions: Focusing focal optics Polarimetry focal plane camera Timing focal plane camera Spectrometry --focal plane camera Operating modes: Observation mode –normal working Calibration mode –on-board calibration Protection mode –shut down HV in SAA Self-testing mode –ASIC self-test
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OUTLINE Top Level Requirements PFA Focal Plan Design
PFA Assembly and Integration PFA Calibration
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PFA functional breakdown
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PFA focal plane assembly performance
Item Specifications Detector size 1.2cm×1.2cm Window 50μm Be Working gas 0.8atm(pure DME) Efficiency See figure Position resolution 80μm Modulation factor keV, see figure System err <1% Energy range 2~10keV Energy resolution ASIC pixels 105600 Relative time accuracy ≤10μs Absolute time accuracy 50μs(TBC) Dead time ≤500μs Operating temperature 25±1℃(TBC) Storage temperature -15℃~45℃(TBC)
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Focal plane assembly functional design
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Gas Pixel Detector (GPD)
Designed by the INFN-Pisa group (Bellazzini et al.) Detecting Area:12mm×12mm Pixel distance: 50μm,352×300 pixels Noise level: 50e-
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Imaging test of GPD Gas: Pure PSF:FWHM = 80 μm
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GPD measurements of the polarized X-rays
Modulation Curve Modulation factor Consistent with simul.
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The sensitivity limit (systematics)
Upper limit 0.8% (99% C.L.) or 0.6% (90% C.L.) Without a P = π/2 component With a P = π/2 component χ2/dof = /97 χ2/dof = 85.0/95 DoM = 0.091% DoM = 0.090% 99% DoM upper limit = 0.43% μ = 0.54 99% DoP upper limit = 0.80% 90% upper limit is 0.6%
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PFA filters wheel assembly performance
Item Specifications Positional accuracy 1’ Hole number 5~6(TBC) Motor lifetime 108 circles X ray tube operating voltage (as needed) 10kV(TBC) Polarized source number 1~2(TBC) Unpolarized source number 2(TBC)
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Filters wheel assembly functional design
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Rotating mechanism The rotating mechanism has flown on several past missions, the designing lifetime of the double coils stepper motor is 108 circles.
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Filters wheel 1.Collimator to reduce the background,
2.Polyimide film to protect the GPD from micrometeoroid etc., 3. Two kinds of unpolarized calibration sources, 4. Polarized source based on a radioactive source or a X ray tube?
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X ray tube VS. radioactive source
Polarized source based on a radioactive source or a X ray tube? X ray tube Radioactive source Advantage More kinds of energy, Can reach 100% polarization, Can turn off the X ray No need to deal with high voltage, Easy to realize compact design. Disadvantage Need high voltage supply and control circuit, Need to deal with high voltage safety, low pressure discharge etc. Hard to reach 100% polarization, Radioactivity Polarized source based on Fe55 devised by IASF-Rome X ray tube on ASTRO-H
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The accelerator group at Tsinghua
Already produced very compact e-beam Is thermal cathode possible?
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PFA production tree
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GPD with ceramic wing New: Original: 1.Mounted by ceramic wing
1.Mounted on PCB 2.Center of mass is high New: 1.Mounted by ceramic wing 2.Mechanical property is improved
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GPD of original design
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GPD with ceramic wing
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PFA preliminary design
CAD design for FPA The dimensions is 200mm×200mm×155mm,the mass is about 6.5Kg。
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FPA preliminary mechanics analysis results
Model analysis results: 1、The first-order natural frequency of components is 520Hz,which is the flexible cables local vibration。 2、There are several natural frequencies of electronics board from 590Hz to 910Hz。 Vibration analysis results 1、Input:15grms; 2、Max response:185grms; 3、Max response location:flexible cables; 4、Electronics board response:70-90grms; 5、Reference HXMT results,all the results are reasonable。
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FPA preliminary thermal analysis results
Conditions: ASIC: 0.5W, Power modules: 0.75W×6, Boundary: Mounting surface of case is 20℃, Surrounding is 20℃. Temperature distribution of the inner shell of the ceramic spacer for GPD
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One PFA budget PFA mass budget:
Item mass(kg) FPA 10 FWA 4 PFA power budget (not including thermal control): Item power(W) FPA 10 FWA 1 PFA telemetry budget: source generation rate (Mbps) compressed rate (Mbps) PFA crab crab
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OUTLINE Top Level Requirements PFA Focal Plan Design
PFA Assembly and Integration PFA Calibration
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AIT flow
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Assembling for GPD
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Integration of FPA
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Integration of FWA
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Focal plane assembly and filters wheel assembly
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Focal plane assembly and filters wheel assembly
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OUTLINE Top Level Requirements PFA Focal Plan Design
PFA Assembly and Integration PFA Calibration
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Preliminary PFA calibration requirements
Item Requirement Opportunity Conditions Energy range 2-10keV FPA, FMA, combined Clean room, vacuum, normal temperature Radioactive source, X ray tube, calibration beam line Effective area(for 4 PFAs) Energy resolution Field of view (FWHM) 7.9 arcmin (limited by detector size) vacuum, normal temperature calibration beam line Angular resolution 30 arcsec (HPD) FMA, Point source localization TBC
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Preliminary PFA calibration requirements
Item Requirement Opportunity Conditions Time resolution <500 μs FPA Clean room, normal temperature Radioactive source, X ray tube Dead time Background TBC No need MDP (minimum detectable polarization) <3% FPA, combined Clean room, vacuum, normal temperature Radioactive source, X ray tube, calibration beam line Maximum source flux (steady, peak) >0.5Crab, >5 Crab upto 24 houres
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Summary PFA instrumental requirements is stated,
Focal plane camera consists of focal plane assembly(FPA) and filters wheel assembly(PWA), The preliminary design of FPA and PWA is stated, The preliminary thermal analysis results for FPA is shown, The preliminary mechanics analysis results is shown, Preliminary conception of AIT and calibration is stated. Thanks! Thanks!
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