Status of the Astrosat mission

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Presentation transcript:

Status of the Astrosat mission A R Rao Tata Institute of Fundamental Research, India

Plan Astrosat Astrosat Instruments: - Ultraviolet Imaging Telescope (UVIT) - Large Area Xenon Proportional Counters (LAXPC) - Soft X-ray Telescope (SXT) - Cadmium Zinc Telluride Imager (CZTI) - Scanning Sky Monitor (SSM) Calibration - CZT – Imager Conclusions 13-May-14 A.R. Rao IACHEC meeting

ASTROSAT UVIT LAXPC SXT CZTI Star Sensors SSM 13-May-14 A.R. Rao IACHEC meeting

Participating Institutes… ISRO Centers Satellite, rocket, T&E, Launch, Orbit, SSM, Level 1&2 software + overall management Research Institutes Tata Institute of Fundamental Research LAXPC, CZTI, SXT Indian Institute of Astrophysics UVIT IUCAA SSM, CZTI RRI LAXPC PRL, Universities, Leicester Uty (SXT), Canadian Space Agency (UVIT) 13-May-14 A.R. Rao IACHEC meeting

ASTROSAT IRS (Indian Remote Sensing) Class Launch PSLV from SHAR Altitude : 650 km; Inclination : 6 deg. Mass 1550 kg. (780 kg. Payloads) Power : 2200 watts 200 Gb (210 Mb/sec) Satellite Positioning System for orbit and time data Payload pointing (3 ): 0.05 degree Slew rate : 0.6 deg/sec Launch: Second quarter of 2015 Operational life > 5 years 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: K S Sarma

UVIT: Two Telescopes, Three Bands 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) Getting ready for satellite integration (next 2 months). 13-May-14 A.R. Rao IACHEC meeting

Soft X-ray Telescope (SXT) Telescope Length: 2465 mm (Telescope + camera + baffle + door) Focal Length: 2000 mm Epoxy Replicated Gold Mirrors on Al substrates in conical Approximation to Wolter I geometry. Radii of mirrors: 65 - 130 mm; Reflector Length: 100 mm No. of nested shells : 40 No. of reflectors: 320 (40 per quadrant) Detector : E2V CCD-22 (Frame-Store) 600 x 600 Field of view : 41.3 x 41.3 arcmin PSF: ~ 2 arcmins Sensitivity (expected): 15 Crab (0.5 cps/mCrab) Calibrated and Integrated with satellite (next talk: A. Read) A.R. Rao IACHEC meeting 13-May-14 Slide courtesy: K P Singh

Large area Xenon-filled Proportional Counters LAXPC: Large area Xenon-filled Proportional Counters Energy range : 3 – 80 keV Time Resolution: 10 sec Area : 6000 cm2 (7980) E /E ~ 3 - 7 Three identical xenon filled proportional counters. Multi layer and multi cell geometry with 60 anode cells and 28 anti cells Xenon + methane mixture at a pressure 1500 mm of Hg. 50 micron thick aluminized Mylar window with a FOV of 1ox1o One Unit calibrated and delivered for satellite integration. 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: Ravi Manchanda

CZT-Imager Size: 482 x 458 x 603 mm Weight - 50 kg Power – 60 Watts Side joining plates Collimator CZT top hsg. CZT bottom hsg. Radiator Heat pipes Optical cube Alpha tag source Handling brackets CFRP support CAM Size: 482 x 458 x 603 mm Weight - 50 kg Power – 60 Watts Collimator: 6 x 6 Degree 17 x 17 Degree

Area 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; 104 s) Calibrated; final testing going on (Satellite Integration in next 2 months) 13-May-14 A.R. Rao IACHEC meeting

Scanning Sky Monitor (SSM) 3 PSPC; Area 60 cm2 (5 keV); Ang res. : 2.5o & 12’ Energy Res 20%@ 6 keV Flight Models are being tested (Satellite Integration in next 2 months) 13-May-14 A.R. Rao IACHEC meeting

Payload integration, alignment & testing: December 2014; Launch: mid-2015 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: S S Sarma

Astrosat: Special Features Low Inclination Continuous time-tagged individual photon data (LAXPC & CZTI) – a few tens of micro-second accuracy Bright source observing capability of SXT Facility to change/ adjust observation time of SSM pointing. Hard X-ray (above ~ 80 keV) monitoring capability. 13-May-14 A.R. Rao IACHEC meeting

Astrosat calibration: ground & onboard 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: G C Dewangan

CCD: X-ray illumination CCD: Optical illumination Mn Kα, Kβ 145 eV resn. 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: K P Singh

LAXPC Calibration Radio-active sources for Spectral Calibration. GEANT4 simulation for background estimation 13-May-14 A.R. Rao IACHEC meeting

CZT Calibration 4 Quadrants 64 Detectors 16,000 pixels Multi- temperature, multi-sources 13-May-14 A.R. Rao IACHEC meeting

Physics based model and fraction of counts in tail Mu-Tau based method: Photo-peak Efficiency 59.54 keV 81 keV 122 keV 99% 87% 84% 13-May-14 A.R. Rao IACHEC meeting

CAM calibration: 2m length A few arc-seconds could be achieved. 13-May-14 A.R. Rao IACHEC meeting

The time difference (Delta T) in units of micro-seconds, is well within the expected calibration for pulse from a normal (1 ppm) clock. 13-May-14 A.R. Rao IACHEC meeting

Polarization Crab 3 sigma detection in < 1 day Next (%) 1:2 3:4 4:5 Obs 2.4+0.1 4.3+0.2 0.8+0.1 8.0+2.0 Monte Carlo 2.43 4.9 1.0 10.0 13-May-14 A.R. Rao IACHEC meeting

10.78 % edge modulation fator 4.8 % corner modulation factor Modulation Curve at 0 degree -7.802 % edge modulation fator 2.57 % corner modulation factor 13-May-14 A.R. Rao IACHEC meeting Modulation Curve at 90 degree

Polarization measurement capability of CZTI Arrows represent incident polarization direction Slide courtesy: Santosh Vadawale

Onboard Calibration Low Energy: standard sources High energy: Crab 13-May-14 A.R. Rao IACHEC meeting

ASTROSAT: Observation Phases and Data Policy 13-May-14 A.R. Rao IACHEC meeting Slide courtesy: K S Sarma

Science Working Group and Payload Science Teams PI: S Seetha (seetha@isro.gov.in) UVIT: S. Tandon (sntandon@iucaa.ernet.in) LAXPC: J. S. Yadav (jsyadav@tifr.res.in) SXT: K.P. Singh (singh@tifr.res.in) CZTI: A. R. Rao (arrao@tifr.res.in) SSM: M. C. Ramadevi (ramadevi@isac.gov.in) 13-May-14 A.R. Rao IACHEC meeting

`Hard X-ray Astronomy: Astrosat and Beyond’ A conference in Goa: September 24 - 26, 2014 13-May-14 A.R. Rao IACHEC meeting

Conclusions Wide band X-ray spectroscopy is the strength of Astrosat. Extensive ground calibrations completed. Results are as expected. New features (individual photon counting and possibly polarization) will enhance the observation capabilities. Onboard calibration will center around Crab observation for high energy instruments. 13-May-14 A.R. Rao IACHEC meeting