CURRENT and FUTURE X-RAY SPECTROMETERS Spectroscopy School, MSSL, March 17-18, 2009 Frits Paerels Columbia Astrophysics Laboratory Columbia University,

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Presentation transcript:

CURRENT and FUTURE X-RAY SPECTROMETERS Spectroscopy School, MSSL, March 17-18, 2009 Frits Paerels Columbia Astrophysics Laboratory Columbia University, New York

Overview: Diffractive vs Non-diffractive Spectrometers Diffractive Spectrometers: gratings, crystals Non-diffractive spectrometers: CCD’s, calorimeters Specific instruments: Chandra, XMM-Newton; Astro-H, IXO

Diffractive vs Non-diffractive Spectrometers Non-diffractive spectrometers: convert energy of single photon into ‘countable objects’ (electrons, broken Cooper pairs, phonons) Example: Si CCD: ionization energy w, photon energy E, nr of electrons N = E/w variance on N: σ 2 = FN; F: Fano factor, < 1 (!!), so ΔE/E = ΔN/N = (wF/E) 1/2 (Si: w = 3.7 eV, F = 0.12) Resolution ΔE, or resolving power E/ΔE, slow function of E Other examples: Superconductors (very small w!!), calorimeters ‘constant ΔE devices’

Diffractive spectrometers: constructive interference of light along several cleverly chosen paths; no limit to resolution (no ‘natural scale’, like w) Example: two slits: d θ Path length difference: d sin θ ‘constant Δλ devices’

Resolving Power Chandra LETGS Chandra HETGS ΔE = 2 eV Micro- calorimeter CCD XMM RGS

Dispersive spectrometers Diffraction Grating Spectrometers(*); Chandra HETGS and LETGS XMM-Newton RGS IXO XGS (*) Only one crystal spectrometer on astrophysics observatory: FPCS on Einstein ( )

1. Chandra HETGS Dispersion equation: sin θ = mλ/d (θ: dispersion angle, d: grating period, m: spectral order Spectral resolution: Δλ = (d/m)cos θ Δθ ≅ (d/m)Δθ: dominated by telescope image (Δθ) Claude Canizares et al., Publ. Astron. Soc. Pac., 117, 1144 (2005)

Chandra HETGS diffraction grating assembly

Chandra HETGS spectrum Focal plane image CCD/dispersion diagram (‘banana’) NB: CCD energy resolution sufficient to separate spectral orders (m = ±1,±2, …)

HETGS Spectral Resolution: /0.025 Å; approximately constant Example: radial velocities in Capella (G8 III + G1 III; approx 2.5 M O each) Very accurate wavelength scale: Δv/c ~ 1/10,000 ! The G8 III primary turns out to be the dominant source of X-ray emission Ishibashi et al., 2006, ApJ, 644, L117

2. Chandra LETGS

Effect of support grid: Cross dispersion When read out with the HRI/S: no order separation (HRI no energy resolution); Fully calibrated and predictable! Chandra LETGS Spectral image

Spectral resolution: ~0.05 Å; low dispersion: goes out to 170 Å, R ~ 3000! Ness et al., 2002, Astron. Astrophys., 387, 1032 note the long wavelengths

3. XMM-Newton Reflection Grating Spectrometer (RGS) Den Herder et al., 2001, Astron. Astrophys., 365, L7 Compared to Chandra: lower resolution, much bigger effective area; Compensate by designing much larger dispersion angles

αβ Dispersion equation: cos β = cos α + mλ/d (as if dispersion by grating with equivalent line density equal to density projected onto incident wavefront) Spectral resolution: telescope blur Δα: Δλ = (d/m) sin α Δα (suppressed by large dispersion) grating alignment: Δλ = (d/m) (sin α + sin β) Δα and a few other terms RGS: α = 1.58 deg, β = 2.97 deg at 15 Å; d = micron (!) Large dispersion due to small incidence angle; offsets telescope blur Grating reflectivity of order 0.3 ! Basics of grazing incidence X-ray reflection gratings

(Photo courtesy of D. de Chambure, XMM-Newton Project, ESA/ESTEC)

RGS spectral imageWavelength, 5-35 Å  RGS ‘banana’ plot

XMM RGS, Werner et al., 2009, MNRAS, in press. Fe XVII A suppressed in core of galaxy by resonance scattering! Source of finite extent: large dispersion of RGS still produces useable spectrum as long as compact (in angular size; Δα < 1 arcmin or so; no slit!)

Effective area = geometric aperture x mirror throughput x grating efficiency x detector quantum efficiency x ‘other factors(…)’

Current Diffraction Grating Spectrometers: Quirks; Calibration not all properties completely encoded in matrix to required accuracy! EXERCISE PROPER CAUTION! Just because something doesn’t fit, that does not mean it’s something astrophysical! wavelength scale: HETGS: about 1 in 10,000 accurate, averaged over entire band LETGS: similar RGS: Δλ ~ 8 mÅ, or about 1 in 2,000 (average); improvement by factor 2 under way instrumental profile shape (‘LSF’): RGS profile depends noticeably on wavelength (mainly due to rapidly varying contribution from scattering by micro- roughness). Also careful with estimating line fluxes, absorption line equivalent widths: non-negligible fraction of power in wings outside two times the resolution: use matrix (not just by eye, or DIY Gauss!) always watch out for detector features (dead spots, cool spots, hot spots, …) effective area: absolute flux measurement probably reliable to level of remaining cross-calibration discrepancies: of order, or smaller than 10%

Non-dispersive spectrometers 1.CCD Spectrometers (Chandra ACIS, XMM-Newton EPIC, Suzaku XIS) Resolving power limited; see above Obvious advantage: high efficiency, spatial resolution (imaging) Credit: NASA/CXC/SAO/D.Patnaude et al. Supernova remnant Cas A, Chandra ACIS-I

2. Microcalorimeter Spectrometers (a.k.a. single photon calorimeter, X-ray quantum calorimeter, Transition Edge Sensor (TES) microcalorimeter(*)) Directly measure heat deposited by single X-ray photon (*) refers to clever, sensitive thermometer principle; not to principles of the μCal)

Temperature jump: ΔT = E/c V c V : heat capacity, E photon energy; make c V small: big ΔT for given E Classically: c V = 3Nk, independent of T (equipartition theorem) (N: number of atoms, k Boltzmann’s constant) Example: 1 mm 3 of Si: N = 5 x atoms; c V = 2 x 10 4 erg/K E = 1 keV = 1.6 x erg: ΔT = 8 x K !! So what is so great about microcalorimeters? Principle of a microcalorimeter

Quantum mechanics: At low T, harmonic oscillators go into ground state; c V collapses! Debye’s famous calculation: And Θ is the Debye temperature; kΘ ~ ħω of the highest-frequency vibration in the crystal. For Si, Θ = 640 K, so for low T (T = 0.1 K), c V is ~ (0.1/640) 3 = 3 x 10 8 times smaller than classical value! (e.g. Kittel: Thermal Physics; Peierls: the Quantum Theory of Solids)

Proportional to temperature XQC rocket experiment; McCammon et al. (2002) Energy resolution set by spontaneous temperature fluctuations; From thermodynamics, straightforward: = c V kT 2 ; T ~ 0.1 K: ΔE rms ~ few eV!

First astrophysical microcalorimeter spectrum: Diffuse soft X-ray emission from the sky (π steradians) X-ray Quantum Calorimeter rocket experiment; McCammon et al. 2002

So: what is so great about microcalorimeters? ‘no limit’ to energy resolution (gets better with lower T, N; higher signal sampling rate; also practical improvements: TES sensors) Can make imaging arrays! (not trivial, because not based on charge collection, but current modulation) But remember, even at ΔE = 2 eV, resolving power < current grating spectrometers, E < 1 keV!

2013: Astro-H/ 完成予想図 -4 (US/Japan/ESA) XCS/X-ray Calorimeter Spectrometer: ΔE = 7 eV, keV

International X-ray Observatory (IXO) F = 20 m; A = 3 m 1 keV Microcalorimeters, CCDs, gratings, polarimeter, ultrafast photometer

Resources: Chandra HETGS: Claude Canizares et al., Publ. Astron. Soc. Pac., 117, 1144 (2005) Nice entry into detailed understanding of HETGS, with discussion of manufacturing and scientific results; follow references. XMM-Newton RGS: den Herder et al., 2001, Astron. Astrophys., 365, L7 Early instrument paper; good description of the instrument, with references F. Paerels: Future X-ray Spectroscopy Missions, in X-ray Spectroscopy in Astrophysics, Lecture Notes in Physics, 520, p.347 (Springer, 1999) (accessible through ADS) recent results: see lecture 1