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An X-Ray Calorimeter Spectrometer for IXO the X-Ray Microcalorimeter Spectrometer (XMS) Superconducting Transition Edge Thermometer A fundamentally new approach for imaging x-ray spectroscopy: Measure energies of individual x-ray photons as heat Measure position using array of calorimeters X-Ray Calorimeter Technology Transition Edge Sensor 8 x 8 array of TES devices ~ 4000 pixel array Cryogen-free design Multiplexed SQUID readout: enables larger arrays and low power dissipation Multi-stage ADRs Cryocooler (Joule-Thomson + Pulse Tube) X-ray CCDs provide excellent imaging but have low spectral resolution Transition at ~ 100 mK and only about 1 mK wide. The Implementation of an Imaging X-Ray Spectrometer for the International X-Ray Observatory Cooling Stage Temperature Cooling Power Temperature Stability Heat Rejection Temperature Detectors, 1st stage SQUIDs 50 mK 5 µW 2 µK rms 2nd stage SQUIDs 1 K (TBR) 230 µW TBD 6 K High Technology Readiness Reference Design: 32 x 32 TES microcalorimeter array MUX SQUID readout Continuous ADR Cryocoolers TES x-ray calorimeter: Mo/Au superconducting thermometer with Au/Bi absorber Absorber extends above and out from thermometer area to cover traces and provide high fill factor. substrate TES technology well-suited for high-speed SQUID multiplexing. 8 8 TES calorimeter array (GSFC) NASA/Goddard Spectral resolution of ~ 2 eV possible throughout 1-10 keV band with ~ arcsec imaging at the focus of IXO R.L. Kelley 1 , S. R. Bandler 2 , R. P. Brekosky 3 , A.D. Brown 1 , J. A. Chervenak 1 , M. J. DiPirro 1 , W. B. Doriese 4 , M. E. Eckart 1 , F. M. Finkbeiner 1 , G. C. Hilton 4 , K. D. Irwin 4 , C. A. Kilbourne 1 , F. Porter 1 , C. D. Reintsema 4 , P. Shirron 1 , S. J. Smith 1 , J. N. Ullom 4 , P. L. Whitehouse 1 1 NASA's GSFC, 2 CRESST and University of Maryland, 3 Northrop Grumman Corporation, 4 National Institute of Standards and Technology. Results of a 2-column by 8-row multiplexing demonstration using a microcalorimeter array developed at Goddard and SQUID multiplexing electronics developed at NIST/Boulder (see Poster 457.13 - Randy Doriese et al. "Progress Toward A Kilopixel Time-division Multiplexer For IXO”) The black points show histograms of MnK X-rays from an 55 Fe source for each pixel acquired simultaneously, with vertical offsets for clarity and fits overlaid in blue/red. Multi-stage adiabatic demagnetization refrigerator (ADR) works by continuously transferring heat of magnetization to “upstream” salt pill, and eventually to cryocooler. Continuous removal of up to 5 μW at 50 mK. Front View Rear View X-Ray Mirror XMS Functional Block Diagram Main Shell Preamplifier/ Bias Box (PBB) Pulse Processing Electronics (PPE) Filter Wheel Control Power Distribution Unit (PDU) 115V From S/C Bus Cryocooler Control Electronics (CCE) ADR Electronics (ADR) SpaceWire To Spacecraft CPU/Storage 0.9 K 5.0 K ADR Stage 2 45 mK 0.275 K 50 mK ADR Stage 3 0.25 K 1 K 1 K 4.5 K 50 mK 15 K 45 K 150 K Loop Heat Pipe to Radiator 260-300 K Precooler Compressor Precooler Compressor Calorimeter/ADR insert heat switch detector package filters thermal link superconducting cable conductive bond cryostat shells Cryocooler cold head JT stage x-rays filter s x-rays filter s Antico detector Microcalorimeter Antico detector Antico detector Microcalorimeter Readout Amplifier (SQUIDs) JT Compressor JT Compressor Filter wheel Vent Valve Pyro Drivers SpaceWire To S/C CPU Instrument Radiator On AFT sunshade Loop Heat Pipe Condenser Gate Valve Impedance Network ADR Stage 5 S/C Power Spacewire I/F ADR Stage 4 Feedback/Controller Box (FCB) Pyro Control From S/C Bus 0.25 K 1 K Translation Mechanism Focus Mechanism Mechanical Control Electronics (MCE) Power Control From S/C S/C function (Not part of XMS instrument) Multi Absorber TES - 1 TES, 4 absorbers absorber R 1 R 3 R 4 R 2 thermometer Heat sink Simple approach to extend focal plane coverage: Separate absorbers (e.g., 4) connected to a single TES, each with a different thermal conductance. Rise times easily distinguished 5-6 eV already demonstrated! Reference Array Design: Inner array with 300 μm pixels 3 arcsec pixels; 2.1 arc min FOV 2.5 eV energy resolution (FWHM) ~ 150 - 300 μsec time constants Outer Array with 600 μm pixels 6 arcsec pixels; 5.4 arcmin FOV < 10 eV energy resolution (FWHM) ~ 1-2 msec time constant Demonstration of multiplexed read-out of TES array
Transcript
Page 1: XMS Functional Block Diagram - Astrophysics · XMS Functional Block Diagram Main Shell Preamplifier/ Bias Box (PBB) Pulse Processing Electronics (PPE) Filter Wheel Control Power Distribution

An X-Ray Calorimeter Spectrometer for IXO –

the X-Ray Microcalorimeter Spectrometer (XMS)

Superconducting

Transition Edge

Thermometer

A fundamentally new approach for imaging x-ray spectroscopy:

Measure energies of individual x-ray photons as heat

Measure position using array of calorimeters

X-Ray Calorimeter Technology – Transition Edge Sensor

8 x 8 array of TES devices

~ 4000 pixel array

Cryogen-free design

Multiplexed SQUID

readout: enables

larger arrays and

low power

dissipation

Multi-stage

ADRs

Cryocooler

(Joule-Thomson

+ Pulse Tube)

X-ray CCDs

provide

excellent

imaging but

have low

spectral

resolution

Transition at

~ 100 mK

and only

about 1 mK

wide.

The Implementation of an Imaging X-Ray Spectrometer for the International X-Ray Observatory

CoolingStage

TemperatureCoolingPower

TemperatureStability

HeatRejection

Temperature

Detectors,1st stageSQUIDs

50 mK 5 µW 2 µK rms

2nd stageSQUIDs

1 K (TBR) 230 µW TBD

6 K

High Technology Readiness

Reference Design:

• 32 x 32 TES

microcalorimeter array

• MUX SQUID readout

• Continuous ADR

• Cryocoolers

TES x-ray calorimeter: Mo/Au superconducting

thermometer with Au/Bi absorber

Absorber extends above and out from

thermometer area to cover traces and

provide high fill factor. substrate

TES technology well-suited for

high-speed SQUID multiplexing.

8 8 TES

calorimeter array

(GSFC)

NASA/Goddard

Spectral resolution of ~ 2 eV possible throughout 1-10 keV band with ~ arcsec imaging

at the focus of IXO

R.L. Kelley1, S. R. Bandler2, R. P. Brekosky3, A.D. Brown1, J. A. Chervenak1, M. J. DiPirro1, W. B. Doriese4, M. E. Eckart1, F. M. Finkbeiner1,

G. C. Hilton4, K. D. Irwin4, C. A. Kilbourne1, F. Porter1, C. D. Reintsema4, P. Shirron1, S. J. Smith1, J. N. Ullom4, P. L. Whitehouse1

1NASA's GSFC, 2CRESST and University of Maryland, 3Northrop Grumman Corporation, 4National Institute of Standards and Technology.

Results of a 2-column by 8-row multiplexing demonstration using a microcalorimeter array

developed at Goddard and SQUID multiplexing electronics developed at NIST/Boulder (see

Poster 457.13 - Randy Doriese et al. "Progress Toward A Kilopixel Time-division Multiplexer For

IXO”) The black points show histograms of MnK X-rays from an 55Fe source for each pixel

acquired simultaneously, with vertical offsets for clarity and fits overlaid in blue/red.

Multi-stage adiabatic demagnetization refrigerator (ADR) works by continuously transferring heat of magnetization

to “upstream” salt pill, and eventually to cryocooler. Continuous removal of up to 5 μW at 50 mK.

Front View

Rear View

X-Ray Mirror

XMS Functional Block Diagram

Main Shell

Preamplifier/

Bias Box (PBB)

Pulse Processing

Electronics (PPE)

Filter Wheel

Control

Power

Distribution

Unit (PDU)

115V

From

S/C

Bus

Cryocooler

Control

Electronics

(CCE)

ADR Electronics

(ADR)

SpaceWire

To Spacecraft

CPU/Storage

0.9 K

5.0 K

ADR Stage 245 mK

0.275 K

ADR Stage 1 50 mK

ADR Stage 3 0.25 K

1 K

1 K

4.5 K

50 mK

15 K

45 K

150 K

Loop Heat

Pipe to

Radiator

260-300 K

Precooler

Compressor

Precooler

Compressor

Calorimeter/ADR insert

heat switch

detector package

filters

thermal link

superconducting cable

conductive bond

cryostat shells

Cryocooler

cold head

JT stage

x-rays

filter

s

x-rays

filter

s

Antico detector

Microcalorimeter

Antico detectorAntico detector

Microcalorimeter Readout Amplifier (SQUIDs)

JT

Compressor

JT

Compressor

Filter wheel

Vent Valve

Pyro

Drivers

SpaceWire

To S/C CPU

Instrument Radiator

On AFT sunshadeLoop Heat

Pipe

Condenser

Gate

Valve

Imp

edan

ce

Net

work

ADR Stage 5

S/C Power

Spacewire I/F

ADR Stage 4

Feedback/Controller

Box (FCB)

Pyro Control

From S/C Bus

0.25 K

1 K

Translation

Mechanism

Focus

Mechanism

Mechanical

Control

Electronics

(MCE)

Power

Control

From

S/C

S/C function (Not part

of XMS instrument)

Multi Absorber TES - 1 TES, 4 absorbers

absorber

R1 R3 R4R2

thermometer

Heat sink

Simple approach to extend focal plane coverage:

Separate absorbers (e.g., 4) connected to a

single TES, each with a different thermal

conductance.

Rise times easily

distinguished

5-6 eV already demonstrated!

Reference Array Design:

Inner array with 300 μm pixels

3 arcsec pixels; 2.1 arc min FOV

2.5 eV energy resolution (FWHM)

~ 150 - 300 μsec time constants

Outer Array with 600 μm pixels

6 arcsec pixels; 5.4 arcmin FOV

< 10 eV energy resolution (FWHM)

~ 1-2 msec time constant

Demonstration of multiplexed read-out of TES array

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