AstroSat: Difference between revisions
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{{wikify|date=May 2007}} |
{{wikify|date=May 2007}} |
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'''ASTROSAT''' is India's first dedicated [[astronomy]] satellite and is scheduled to launch in mid |
'''ASTROSAT''' is India's first dedicated [[astronomy]] satellite and is scheduled to launch in mid 2009. |
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After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996 the [[Indian Space Research Organization]] (ISRO) has approved further development for a full fledged astronomy satellite - ASTROSAT. |
After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996 the [[Indian Space Research Organization]] (ISRO) has approved further development for a full fledged astronomy satellite - ASTROSAT. |
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* Multi-wavelength studies of cosmic sources |
* Multi-wavelength studies of cosmic sources |
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* Monitoring the X-ray sky for new transients |
* Monitoring the X-ray sky for new transients |
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* |
* Sky survey in the hard X-ray and UV bands |
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* Broadband spectroscopic studies of X-ray binaries, AGN, SNRs, clusters of galaxies and stellar coronae |
* Broadband spectroscopic studies of X-ray binaries, AGN, SNRs, clusters of galaxies and stellar coronae |
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* Studies of periodic and non-periodic variability of X-ray sources |
* Studies of periodic and non-periodic variability of X-ray sources |
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* [[Nuclear Research Laboratory]], Bhabha Atomic Research Centre, Mumbai |
* [[Nuclear Research Laboratory]], Bhabha Atomic Research Centre, Mumbai |
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* [[S.N. Bose National Centre for Basic Sciences]], Kolkata |
* [[S.N. Bose National Centre for Basic Sciences]], Kolkata |
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* Canadian Space Agency |
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* University of Leicester |
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Astrosat is an X-ray/UV astronomy observatory planned for launch in mid of the year 2007. The main mission objectives are: |
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* Broadband X-ray spectroscopy |
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* Ultraviolet Sky Survey |
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* Simultaneous Multi-wavelength Monitoring of time-variable sources |
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# Large-Area Xenon-filled Proportional Counters (LAXPC) |
# Large-Area Xenon-filled Proportional Counters (LAXPC) |
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# A Coded-mask Camera with Cadmium-Zinc-Telluride detector array ( |
# A Coded-mask Camera with Cadmium-Zinc-Telluride detector array (CZTI) |
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# A Soft-Xray imaging telescope with multi-foil Wolter optics and CCD detector (SXT) |
# A Soft-Xray imaging telescope with multi-foil Wolter optics and CCD detector (SXT) |
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# A deployable boom-mounted Scanning X-ray Sky Monitor consisting of three one-dimensional coded mask cameras (SSM) |
# A deployable boom-mounted Scanning X-ray Sky Monitor consisting of three one-dimensional coded mask cameras (SSM) |
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# Two 40-cm dia Ultraviolet Telescopes for NUV and FUV coverage (UVIT) |
# Two 40-cm dia Ultraviolet Telescopes for optical, NUV and FUV coverage (UVIT) |
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# An optical monitor, which will be an attachment to the NUV telescope |
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The total weight of all the instruments will be about 750 kg, and the weight of the entire spacecraft will be about 1650 kg. It will be launched by ISRO's PSLV launcher into a Low-Earth Orbiting(altitude = 600 km) circular low-inclination (near-equatorial) orbit. |
The total weight of all the instruments will be about 750 kg, and the weight of the entire spacecraft will be about 1650 kg. It will be launched by ISRO's PSLV launcher into a Low-Earth Orbiting(altitude = 600 km) circular low-inclination (near-equatorial) orbit. |
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==External links== |
==External links== |
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*[http:// |
*[http://meghnad.iucaa.ernet.in/~astrosat/ ASTROSAT website] |
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{{India space}} |
{{India space}} |
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Revision as of 07:59, 7 February 2008
Template:Wikify is deprecated. Please use a more specific cleanup template as listed in the documentation. |
ASTROSAT is India's first dedicated astronomy satellite and is scheduled to launch in mid 2009.
After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996 the Indian Space Research Organization (ISRO) has approved further development for a full fledged astronomy satellite - ASTROSAT.
A large number of leading astronomy research institutions in India and abroad are jointly building various instruments for the satellite.
Important areas requiring broad band coverage include studies of astrophysical objects ranging from the nearby solar system objects to distant stars, to objects at cosmological distances; timing studies of variables ranging from pulsations of the hot white dwarfs to active galactic nuclei(AGN)with time scales ranging from milliseconds to few hours to days.
ASTROSAT is currently proposed as a multi-wavelength astronomy mission on an IRS-class satellite into a near-Earth, equatorial orbit by the PSLV. The 5 instruments on board cover the UV(1000-3000 A), soft and hard x-ray regimes (0.3 - 8 keV; 2 - 100 keV).
Objectives of ASTROSAT
- Multi-wavelength studies of cosmic sources
- X-ray timing, with response up to hard X-rays (~100 keV)
- Monitoring the X-ray sky for new transients
- Sky survey in the hard X-ray and UV bands
- Broadband spectroscopic studies of X-ray binaries, AGN, SNRs, clusters of galaxies and stellar coronae
- Studies of periodic and non-periodic variability of X-ray sources
- Monitoring intensity of known sources and detecting outbursts and luminosity variations
Participants
ASTROSAT project is a collaborative effort of a growing list of research institutions. The current participants are:
- Indian Space Research Organization
- Tata Institute of Fundamental Research, Mumbai
- Indian Institute of Astrophysics, Bangalore
- Raman Research Institute, Bangalore
- Inter-University Centre for Astronomy and Astrophysics, Pune
- Nuclear Research Laboratory, Bhabha Atomic Research Centre, Mumbai
- S.N. Bose National Centre for Basic Sciences, Kolkata
- Canadian Space Agency
- University of Leicester
To achieve the mission objectives, Astrosat will carry the following payloads:
- Large-Area Xenon-filled Proportional Counters (LAXPC)
- A Coded-mask Camera with Cadmium-Zinc-Telluride detector array (CZTI)
- A Soft-Xray imaging telescope with multi-foil Wolter optics and CCD detector (SXT)
- A deployable boom-mounted Scanning X-ray Sky Monitor consisting of three one-dimensional coded mask cameras (SSM)
- Two 40-cm dia Ultraviolet Telescopes for optical, NUV and FUV coverage (UVIT)
- A Charged particle monitor (CPM)
The total weight of all the instruments will be about 750 kg, and the weight of the entire spacecraft will be about 1650 kg. It will be launched by ISRO's PSLV launcher into a Low-Earth Orbiting(altitude = 600 km) circular low-inclination (near-equatorial) orbit.