5/21/2015g.c.stewart berlin 1 astrosat: a multi-wavelength satellite 1st dedicated indian...
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ASTROSAT: A Multi-Wavelength Satellite1st Dedicated Indian Astronomical Mission
ISRO Satellite Centre (ISAC), Bangalore
Tata Institute of Fundamental Research, Mumbai
University of Leicester
Indian Institute of Astrophysics (IIA), Bangalore
Inter-University Centre for Astronomy & Astrophysics (IUCAA), Pune.
Canadian Space Agency
Raman Research Institute, Bangalore
Vikram Sarabhai Space Centre, Trivandrum
X-RAY
UV/Opt
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ASTROSAT (1.55 tons 600 kms, nearly equatorial orbit by PSLV, 3
gyros and 2 star trackers for attitude control by reaction wheel system with a Magnetic torquer )
Soft X-ray Telescope
3 Large Area Xenon Proportional Counters
2 UV(+Opt ) Imaging Telescopes
CZTI
Folded Solar panels
Radiator PlatesFor SXT and CZT
Scanning Sky Monitor (SSM)
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UVIT: Two Telescopes f/12 RC Optics Focal Length: 4756mm Diameter: 38 cm Simultaneous Wide
Angle ( ~ 28’) images in FUV (130-180 nm) in one and NUV (180-300 nm) & VIS (320-530 nm) in the other
MCP based intensified CMOS detectors
Spatial Resolution : 1.8” Sensitivity in FUV: mag.
20 in 1000 s Temporal Resolution ~
30 ms, full frame ( < 5 ms, small window )
Gratings for Slit-less spectroscopy in FUV & NUV
R ~ 100
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UVIT: filters
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GALEX UVITFoV (Circular dia) 1.24 degrees 27 arc-min
No. of bands 2 (NUV, FUV) 2 channels (NUV, FUV) + Vis
Filters in NUV NIL 5 filters
Filters in FUV NIL 5 filters [multiple colour-colour diagrams]
Spectroscopy Grism Grating
Resolution R ~ 100-120 R ~ 100
No. of grism/grating 1 per band 2 per band
Angular resolution 4.5-6.0 arcsec 1.8 arc-sec (FWHM)
Saturation < 10 mag < 8.0 mag (neutral density filter)
[can image fields with bright objects]
Time resolution ~ 10 milli-sec ~ 5.0 milli-sec (window mode)
~ 30 milli-sec full field
Energy Range : 3-80 keV
(50 Mylar window, 2 atm. of 90 % Xenon + 10 % Methane)
Effective Area : 6000 cm² (@ 20 keV)
Energy Resolution : ~10% FWHM at 22 keV
Field of View : 1° x 1° FWHM
(Collimator : 50µ Sn + 25µ Cu + 100µ Al )Blocking shield on sides and bottom : 1mm Sn + 0.2 mm Cu
Timing Accuracy: 10 μsec in time tagged mode
(oven-controlled oscillator).
Onboard purifier for the xenon gas
Large Area Xenon Proportional Counter (LAXPC): Characteristics
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LAXPC: Effective Area
Large Area X-ray Proportional Counter (LAXPC)
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LAXPC: Collimator
CZT Imager characteristicsArea 1024 cm 2
Pixels 16384
Pixel size 2.4 mm X 2.4 mm (5 mm thick)
Read-out ASIC based (128 chips of 128 channels)
Imaging method Coded Aperture Mask (CAM)
Field of View 17 X 17 deg2 (uncollimated)
6 X 6 (10 – 100 keV) – CAM
Angular resolution 8 arcmin
Energy resolution 5% @ 100 keV
Energy range 10 – 100 keV - Up to 1 MeV (Photometric)
Sensitivity 0.5 mCrab (5 sigma; 10 4 s)
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CZT-Imager with a coded mask
(Qualification Model)
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CZT Detector 4 cm X 4 cm
CZT crystal
Connectors HV Connector
Thermalconductor
Thermalconductor
ASIC
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SXT CharacteristicsTelescope Length: 2465 mm (Telescope + camera + baffle + door)
Top Envelope Diameter: 386 mm Focal Length: 2000 mmEpoxy Replicated Gold Mirrors on Al substrates in conical Approximation to Wolter I geometry.Radius of mirrors: 65 - 130 mm; Reflector Length: 100 mmReflector thickness: 0.2 mm (Al) + Epoxy (~50 microns) + gold (1400 Angstroms)
Minimum reflector spacing: 0.5 mmNo. of reflectors: 320 (40 per quadrant) Detector (Swift Heritage): E2V CCD-22 600 x 600
Field of view : 41.3 x 41.3 arcmin
PSF: 3 – 4 arcminsSensitivity (expected): few x 10-14 cgs (1 cps/mCrab)
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Soft X-ray Telescope
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•Four Fe-55 calibration (corner) sources•One Fe 55 calibration door source•Optical Blocking Filter•CCD Assy. including TEC•PCB with front-end electronics
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SXT Engineering and Flight Models
Astrosat SXT FM FPCA in Thermal Vacuum Chamber at Birmingham
University
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CCD Performance Nominal•Noise ~6 – 10 e-
•Resolution at Mn ~157 eV (Lab Electronics)
SXT CCD (Eng.) Data with TIFR built Electronics
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5.9 and 6.4 keV peaks
Si escape peaks3.70 and 4.15 keV
Isolated pixels only
Resolution ~140 eV
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Door and Corner X-ray Calibration Sources
Optical LED Image
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SXT Effective Area vs. Energy (after subtraction of shadowing effects due to holding structure)
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Scanning Sky Monitor (SSM) Detector : 3 x Proportional counters
with resistive anodes Ratio of signals on either ends of anode
gives position. Energy Range : 2 - 10 keV Position resolution : 1.5 mm Field of View : 10o x 90o (FWHM) Sensitivity : 30 mCrab (5 min
integration) Time resolution : 1 ms Angular resolution : ~ 10 arc min
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Status Engineering Environmental Tests almost
complete Flight Model Construction Well Advanced
(UVIT detectors and SXT CCD camera complete)
Spacecraft Assembly begun – most subsystems complete
Launcher Assigned Launch Date
ASTROSAT – Key Strengths
Simultaneous V/UV to hard X-ray measurements
LEO+ 70 inclinclination Low , stable? Background
Large area at high X-ray energies UV imaging capability Low pile-up in CCD Fast Slewing ??
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ASTROSAT – Key Projects1. AGN/Binaries: Simultaneous UV to hard X-
ray timing/monitoring2. Galactic Novae: UV to X-ray Observations
(TOO program)3. Magnetars: Multi-wave observations4. LMXBs: Persistent Pulsations and
thermonuclear bursts5. Galactic Black Holes and micro / nano
quasars6. Binary X-ray Pulsars: Cyclotron Resonance
Scattering Features (X-ray Observations)7. Clusters of galaxies: X-ray & UV
Observations
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ASTROSAT – Key Projects
10. Supernova Remnants: X-ray and UV Observations
11. UVIT observations ofa) Star Forming galaxies, b) Young stellar objects, c) Galactic Structure, d) Proto- and Planetary Nebulaee) UV Extinction in the Galaxy (Archival Data)
12. Miscellaneous: a) Study nano quasars and Compton thick sources, b) Observations of Stellar Flares, c) GLAST/INTEGRAL/BAT Sources, d) Surveys - multi wave, deep fields
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AGN (bright)
• 4/5 decade SEDs - Resolving all the spectral components : UV and soft X-rays (thermal) from accretion disk, hard X-ray reflection component, intrinsic power-law component
• Variability correlation and lags between UV, soft and hard X-rays
• Variability correlation and lags between Fe-K line and Compton Reflection
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SXT: Clusters of galaxies
C
SXT
LAXPC
CZTI
H
Spectral model from Rephaeli et al. (1999)
Binary X-ray Pulsars with AstrosatSimulated 10 ks observations of hard X-ray spectrum of Accreting Pulsar 4U
0115+63 The cyclotron lines are well resolved by ASTROSAT
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PV Phase(6 months)
Guaranteed Time(6 months
2nd Year 3rd Year 3+? Yr
X-ray Teams
67% 67% 32.5% 20% _
UVIT Team 33% 33% 17.5% 10% _
Indian Proposals
_ _ 35% 45% 65%
International Proposals
_ _ _ 10% 20%
Canada _ _ 5% 5% 5%
Leicester _ _ 3% 3% 3%
TOO _ _ 5% 5% 5%
Calibration _ _ 2% 2% 2%
Time Allocation
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Coming Next Year !
Simultaneous UV to hard X-ray spectral measurements with ASTROSAT: Blazars,
HPQs, OVVs etc.Science Drivers: Jet Physics, particle injection and
acceleration• Synchrotron X-ray emission from the highest energy e-• Electron/proton injection. • Acceleration and cooling related variability patterns in Sync. components of FSRQs and LBLs. • UV and soft X-ray variability can pin down the transition between the emission from slow and fast cooling e- and thus obtain estimates of magnetic field and Doppler factors of the jets.• Shocks in jets. Geom: viewing angle, jet opening angle.• Underlying Accretion disk in Blazars ? Can be revealed during minima when the beamed component is suppressed.
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