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Chandra X-ray Center
Martin ElvisSmithsonian Astrophysical Observatory
Welcome
to the 4th
Chandra – CIAO
Workshop20 – 22 May 2002
Chandra X-ray Center
Chandra X-ray Observatory Overview
Martin Elvis
Smithsonian Astrophysical Observatory
CIAO Workshop
20 May 2001
Chandra X-ray Center
NASA Great Observatories
CHANDRA
Chandra X-ray Center
Focusing X-rays
Chandra X-ray Center
2 Imaging Focal Plane Science Instruments– ACIS (Advanced CCD Imaging Spectrometer)
– HRC (High Resolution Camera)
Chandra Mission Summary Launch: July 23, 1999
– STS-93/ Inertial Upper Stage / Integral Propulsion System– 10,000 km x 140,000 km, 28.4o Inclined Orbit
¼ arcsecond resolution. Sub-0.5arcsec in practice
10-m Focal Length Wolter -1 Mirror: 4 nested Mirror Pairs Energy Range: 0.1-10 keV
Design Lifetime > 5 Years (in NASA plan for 10 year life)
2 Objective Transmission Gratings for Dispersive Spectroscopy– LETG (Low-Energy Transmission Grating)
– HETG (High-Energy Transmission Grating)
Chandra X-ray Center
Mission and Observatory Description
Chandra X-ray Center
High Resolution Mirror Assembly
polished to 3A -> low scattering
high dynamic range
4 pairs of concentric thin-walled zerodur, grazing incidence Wolter Type-I mirrors ->large area. ->800cm2 E<2keV
figured to 0.5” FWHM -> sensitivity,
-> megapixel images
Focal length 10 m. -> response to 10keV
1.6”
95%
Chandra X-ray Center
Aspect Camera and Fiducial Transfer System
4.25inch dia. 15”pixels
Aspect Camera
<0.25” r ms (typical)
Chandra X-ray Center
Chandra Science Instruments
Advanced CCD Imaging Spectrometer (ACIS)– CCD array with 16’x16’ field of view (ACIS-I)– grating readout array (ACIS-S)
High Resolution Camera (HRC)– microchannel plate imager with 31’x31’ field of view (HRC-I)– low energy grating readout array (HRC-S)– High time resolution
High Energy Transmission Grating Spectrometer (HETG)– transmission grating pairs for medium and high energy
Low Energy Transmission Grating Spectrometer (LETG)– transmission grating for low energy
ACIS-I
ACIS-S
HRC-I
HRC-S
BI BI
Z+
Y+
Chandra X-ray Center
Advanced CCD Imaging Spectrometer (ACIS) Ten 1024x1024 pixel CCDs (any 6
simultaneously)– Intrinsic energy resolution ~100eV ->
imaging spectroscopy – ACIS-I: 2x2 array for imaging
(16x16 arcmin)– ACIS-S: 1x6 array for imaging
(8x8arcmin) or spectroscopy– 2 `back illuminated’ (BI) chips: good
low E QE, higher throughput
Chandra X-ray Center
ACIS IssuesCTI
Front Iluminated (FI) chips suffered proton damage just after launch. -> charge transfer inefficiency (CTI) -> much degraded energy resolution
Pileup 3.2 s full frame readout time -> for
sources >0.1ct/s suffer “pileup” I.e. 2 photons in same pixel/frame -> loss of energy information, and -> loss of PSF peak
Pileup correction (J.Davis, MIT) available in Sherpa
CTI correction (Townsley, PSU) restores linearity, most dE/E
Low Energy Calibration Non-linear gain Changing QE See L. David talk
Chandra X-ray Center
Chandra Grating Spectrometers
m=2
m=1
m=0
m=-1
m=-2
IncomingRadiation
m = d sin
d
Chandra X-ray Center
Grating Spectrometers
HETG: High Energy Transmission Gratings
– Designed for use with ACIS-S providing E/delta(E) to 1000 between 0.4 and 10.0 keV
– Two sets of gratings– Medium Energy Gratings (MEG) use outer 2 mirrors– High Energy Gratings (HEG) use inner 2 mirrors– Mounted at different angles to form an “X” dispersed pattern
LETG High Energy Transmission Gratings
– Provides highest resolving power at low energies– Designed for use with HRC-S with 0.07 – 7.29 keV– E/delta(E) > 1000 for 0.07 < E < 0.15 keV– E/delta(E) < 1000 for E > 0.15 keV
Chandra X-ray Center
Chandra Operations Mission science plan
converted to command loads and uplinked to Chandra
X-ray events collected and stored on Solid-State Recorders (SSR)
Ground contact established every ~8 hours through Deep Space Network– SSR data downlinked
– new command load uplinked (up to 72 hours of stored commands)
Data transferred to OCC through JPL for science processing
CXO
CXCOCC
sssssssssssssssssssssss
6. Chandra X-ray Center Architecture
uplinkdownlink
Chandra X-ray Center
Chandra Observing Cycle
High (66%) observing efficiency TOOs, solar flares ->big hit on
mission planning team Annual Proposal Cycle: Next Deadline: 15 March 2003
(anticipated) + Archive, Theory grants Funding expected to 2009
Chandra X-ray Center
enjoy the workshop!