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Isro to launch Astrosat to study the skies - The Times of India



MANGALORE: Indian Space Research Organisation (ISRO) is in the process of launching Astrosat to study the skies over India and thereby give a great contribution from India to the study of astronomy, said K Radhakrishnan, secretary, department of space, and chairman, space commission and ISRO. Astrosat will be launched aboard a PSLV in 2015, will have six instruments and can be described as a multi wave length observatory in space.

Delivering the 32nd annual convocation address of Mangalore University here on Monday and giving an insight into ISROs future space programmes, Radhakrishnan said earth observation capabilities too is high on ISROs agenda with plans afoot to study objects 0.25 metres on the ground with satellites that are 500-600kms in space. "We will use heavy high powered satellites for this," he said. Studying the skies too will be taken up with Astrosat.

This satellite will have ultra-violet, visible and x-ray instruments. It is getting ready now, he said, adding that the satellite will be integrated by 2015. The instruments that will be used on board Astrosat are being built by several institutions across India including the Tata Institute of Fundamental Research, Mumbai, the Indian Institute of Astrophysics, Bangalore, and at ISRO itself, Radhakrishnan noted adding this is a joint effort of various institutions.

Dwelling on two critical missions that ISRO embarked upon in recent past, Radhakrishnan said, in November last Mars orbiter spacecraft embarked on a journey towards Mars, making it the first Made In India object to leave the Earth's sphere of influence. The Mars orbiter is on course for its arrival near Mars on September 24, 2014, he said adding that the crucial operation of reducing its velocity and placing it around Mars will take place then.

The successful flight test of cryogenic stage in the beginning of this year is another milestone in space programme. Noting the success as result of hard work of teams for two decades and development of a host of test facility and infrastructure, Radhakrishnan said nearly 850 wind tunnel tests and 45 ground tests were conducted before proceeding for flight. Several hard technical and managerial decisions had to be arrived at for its success, he noted.


Astrosat - Wikipedia, the free encyclopedia

Astrosat is India's first dedicated astronomy satellite and is scheduled to launch on board the PSLV in 2014.[1]
After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996, the Indian Space Research Organization (ISRO) approved (in 2004) further development for a full fledged astronomy satellite: Astrosat. It was originally hoped to be launched about 2008/9.[2]
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 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 visible (320-530 nm), near UV (180-300 nm), far UV (130-180 nm), soft X-ray (0.3-8 keV and 2-10 keV) and hard X-ray (3-80 keV and 10-150 keV) regions of the electromagnetic spectrum.












Launch date2015 (planned)
Launch siteSatish Dhawan Space Centre
Launch vehiclePSLV-XL
Mission length5 years
Mass1,650 kg (3,640 lb)
Type of orbitNear-equatorial
Orbit height650 km (400 mi)
Orbit period5 years
WavelengthMulti-wavelength
Instruments
UVITUltraViolet Imaging Telescope
SXTSoft X-ray telescope
LAXPCX-ray timing and low-resolution spectral studies
CZTIHard X-ray imager




Mission[edit]


Artist's conception of a binary star system with one black hole and one main sequence star
Astrosat will be a proposal-driven general purpose observatory, with main scientific focus on:
  • Simultaneous multi-wavelength monitoring of intensity variations in a broad range of cosmic sources
  • Monitoring the X-ray sky for new transients
  • Sky surveys 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
Astrosat will carry out multi-wavelength observations covering spectral bands from radio, optical, IR, UV, X-ray and Gamma ray regions both for study of specific sources of interest and in survey mode. While radio, optical, IR observations would be coordinated through ground-based telescopes, the high energy regions, i.e., UV, X-rays and Gamma rays would be covered by the dedicated satellite borne instrumentation of Astrosat.[3]
The mission would also study near simultaneous muti-wavelength data from different variable sources. In a binary system, for example, regions near the compact object emit predominantly in X-rays, the accretion disc emitting most of its light in the UV/optical waveband, whereas the mass of the donating star is brightest in the optical band.
The observatory will also carry out:
  1. Low to moderate resolution spectroscopy over wide energy band with the primary emphasis on studies of X-ray emitting objects
  2. Timing studies of periodic and aperiodic phenomenon in X-ray binaries
  3. Studies of pulsations in X-ray pulsars
  4. QPOs, flickering, flaring, and other variations in X-ray binaries
  5. Short and long term intensity variations in AGNs
  6. Time lag studies in low/hard X-rays and UV/optical radiation
  7. Detection and study of x-ray transients.[4]
In particular, the mission will train its instruments at active galactic nuclei at the core of the Milky Way that is believed to have a super massive black hole.[5]
Payloads[edit]
The scientific payload has a total mass of 750 kg and contains six instruments.
  • The UltraViolet Imaging Telescope (UVIT) - The UltraViolet Imaging Telescope will perform imaging simultaneously in three channels: 130-180 nm, 180-300 nm, and 320-530 nm. The field of view is a circle of ~ 28 arcmin diameter and the angular resolution is 1.8" for the ultraviolet channels and 2.5" for the visible channel. In each of the three channels a spectral band can be selected through a set of filters mounted on a wheel; in addition, for the two ultraviolet channels a grating can be selected in the wheel to do slitless spectroscopy with a resolution of ~100.
  • Soft X-ray imaging Telescope (SXT)- The soft X-ray telescope on Astrosat will employ focussing optics and a deep depletion CCD camera at the focal plane to perform X-ray imaging in 0.3-8.0 keV band. The optics will consist of 41 concentric shells of gold-coated conical foil mirrors in an approximate Wolter-I configuration. The focal plane CCD camera will be very similar to that flown on SWIFT XRT. The CCD will be operated at a temperature of about −80 °C by thermoelectric cooling.
  • The LAXPC Instrument - For X-ray timing and low-resolution spectral studies over a broad energy band (3-80 keV) Astrosat will use a cluster of 3 co-aligned identical Large Area X-ray Proportional Counters (LAXPCs), each with a multi-wire-multi-layer configuration and a Field of View of 1° × 1°. These detectors are designed to achieve (I) wide energy band of 3-80 keV, (II) high detection efficiency over the entire energy band, (III) narrow field of view to minimize source confusion, (IV) moderate energy resolution, (V) small internal background and (VI) long lifetime in space.
  • Cadmium Zinc Telluride Imager (CZTI) - Astrosat will carry a hard X-ray imager in the form of CZTI. It will consist of a Pixellated Cadmium-Zinc-Telluride detector array of ~1000 cm2 geometric area. These detectors have very good detection efficiency, close to 100% up to 100 keV, and have a superior energy resolution (~2% at 60 keV) compared to scintillation and proportional counters. Their small pixel size also facilitates medium resolution imaging in hard x-rays. The CZTI will be fitted with a two dimensional coded mask, for imaging purposes. The sky brightness distribution will be obtained by applying a deconvolution procedure to the shadow pattern of the coded mask recorded by the detector.
  • Scanning Sky Monitor (SSM) - The Scanning Sky Monitor will consist of three position sensitive proportional counters, each with a one-dimensional coded mask, very similar in design to the All Sky Monitor on NASA's RXTE satellite. The gas-filled proportional counter will have resistive wires as anodes. The ratio of the output charge on either ends of the wire will provide the position of the x-ray interaction, providing an imaging plane at the detector. The coded mask, consisting of a series of slits, will cast a shadow on the detector, from which the sky brightness distribution will be derived.
  • Charged Particle Monitor (CPM) - A charged particle monitor (CPM) will be included as a part of Astrosat payloads to control the operation of the LAXPC, SXT and SSM. Even though the orbital inclination of the satellite will be 8 deg or less, in about 2/3 of the orbits, the satellite will spend a considerable time (15 – 20 minutes) in the South Atlantic Anomaly (SAA) region which has high fluxes of low energy protons and electrons. The high voltage will be lowered or put off using data from CPM when the satellite enters the SAA region to prevent damage to the detectors as well as to minimize ageing effect in the Proportional Counters.
Ground support[edit]
The Ground Command and Control Centre for Astrosat will be located at ISAC, Bangalore, India. Commanding and data download will be possible during every visible pass over Bangalore. Ten out of 14 orbits per day will be visible to the ground station. The satellite is capable of gathering 420 gigabits of data every day that can be down loaded in 10 to 11 orbits visible at Tracking and Data receiving center of ISRO in Bangalore.[citation needed] A third 11-meter antenna at the Indian Deep Space Network (IDSN) was operational in July 2009 to track Astrosat.
Current status[edit]
April 2009 : Scientists from Tata Institute of Fundamental Research (TIFR) have completed the developmental phase of complex science payloads and have begun integrating them before delivery of the 1,650 kg satellite Astrosat. A payload from RRI (Raman Research Institute) is under development, awaiting delivery. The challenges in the design of payloads and Attitude Control System have been overcome and in a recent review committee meeting, it was decided that the delivery of the payload to ISRO satellite Centre will begin from the middle of 2009 and continue till early 2010 to enable the launch of ASTROSAT in 2010 using ISRO workhorse PSLV.[6]
Two of the instruments were harder than expected to complete. "The satellite’s soft x-ray telescope proved to be a huge challenge that took 11 years..."[2] As of April 2012, the launch has been rescheduled to 2014.[1]
Participants[edit]
The Astrosat project is a collaborative effort of a growing list of research institutions. The current participants are:


Payloads

astrosat_table_1.png
 
Last edited:
Isro to launch Astrosat to study the skies - The Times of India



MANGALORE: Indian Space Research Organisation (ISRO) is in the process of launching Astrosat to study the skies over India and thereby give a great contribution from India to the study of astronomy, said K Radhakrishnan, secretary, department of space, and chairman, space commission and ISRO. Astrosat will be launched aboard a PSLV in 2015, will have six instruments and can be described as a multi wave length observatory in space.

Delivering the 32nd annual convocation address of Mangalore University here on Monday and giving an insight into ISROs future space programmes, Radhakrishnan said earth observation capabilities too is high on ISROs agenda with plans afoot to study objects 0.25 metres on the ground with satellites that are 500-600kms in space. "We will use heavy high powered satellites for this," he said. Studying the skies too will be taken up with Astrosat.

This satellite will have ultra-violet, visible and x-ray instruments. It is getting ready now, he said, adding that the satellite will be integrated by 2015. The instruments that will be used on board Astrosat are being built by several institutions across India including the Tata Institute of Fundamental Research, Mumbai, the Indian Institute of Astrophysics, Bangalore, and at ISRO itself, Radhakrishnan noted adding this is a joint effort of various institutions.

Dwelling on two critical missions that ISRO embarked upon in recent past, Radhakrishnan said, in November last Mars orbiter spacecraft embarked on a journey towards Mars, making it the first Made In India object to leave the Earth's sphere of influence. The Mars orbiter is on course for its arrival near Mars on September 24, 2014, he said adding that the crucial operation of reducing its velocity and placing it around Mars will take place then.

The successful flight test of cryogenic stage in the beginning of this year is another milestone in space programme. Noting the success as result of hard work of teams for two decades and development of a host of test facility and infrastructure, Radhakrishnan said nearly 850 wind tunnel tests and 45 ground tests were conducted before proceeding for flight. Several hard technical and managerial decisions had to be arrived at for its success, he noted.


Astrosat - Wikipedia, the free encyclopedia

Astrosat is India's first dedicated astronomy satellite and is scheduled to launch on board the PSLV in 2014.[1]
After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996, the Indian Space Research Organization (ISRO) approved (in 2004) further development for a full fledged astronomy satellite: Astrosat. It was originally hoped to be launched about 2008/9.[2]
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 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 visible (320-530 nm), near UV (180-300 nm), far UV (130-180 nm), soft X-ray (0.3-8 keV and 2-10 keV) and hard X-ray (3-80 keV and 10-150 keV) regions of the electromagnetic spectrum.












Launch date2015 (planned)
Launch siteSatish Dhawan Space Centre
Launch vehiclePSLV-XL
Mission length5 years
Mass1,650 kg (3,640 lb)
Type of orbitNear-equatorial
Orbit height650 km (400 mi)
Orbit period5 years
WavelengthMulti-wavelength
Instruments
UVITUltraViolet Imaging Telescope
SXTSoft X-ray telescope
LAXPCX-ray timing and low-resolution spectral studies
CZTIHard X-ray imager




Mission[edit]


Artist's conception of a binary star system with one black hole and one main sequence star
Astrosat will be a proposal-driven general purpose observatory, with main scientific focus on:
  • Simultaneous multi-wavelength monitoring of intensity variations in a broad range of cosmic sources
  • Monitoring the X-ray sky for new transients
  • Sky surveys 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
Astrosat will carry out multi-wavelength observations covering spectral bands from radio, optical, IR, UV, X-ray and Gamma ray regions both for study of specific sources of interest and in survey mode. While radio, optical, IR observations would be coordinated through ground-based telescopes, the high energy regions, i.e., UV, X-rays and Gamma rays would be covered by the dedicated satellite borne instrumentation of Astrosat.[3]
The mission would also study near simultaneous muti-wavelength data from different variable sources. In a binary system, for example, regions near the compact object emit predominantly in X-rays, the accretion disc emitting most of its light in the UV/optical waveband, whereas the mass of the donating star is brightest in the optical band.
The observatory will also carry out:
  1. Low to moderate resolution spectroscopy over wide energy band with the primary emphasis on studies of X-ray emitting objects
  2. Timing studies of periodic and aperiodic phenomenon in X-ray binaries
  3. Studies of pulsations in X-ray pulsars
  4. QPOs, flickering, flaring, and other variations in X-ray binaries
  5. Short and long term intensity variations in AGNs
  6. Time lag studies in low/hard X-rays and UV/optical radiation
  7. Detection and study of x-ray transients.[4]
In particular, the mission will train its instruments at active galactic nuclei at the core of the Milky Way that is believed to have a super massive black hole.[5]
Payloads[edit]
The scientific payload has a total mass of 750 kg and contains six instruments.
  • The UltraViolet Imaging Telescope (UVIT) - The UltraViolet Imaging Telescope will perform imaging simultaneously in three channels: 130-180 nm, 180-300 nm, and 320-530 nm. The field of view is a circle of ~ 28 arcmin diameter and the angular resolution is 1.8" for the ultraviolet channels and 2.5" for the visible channel. In each of the three channels a spectral band can be selected through a set of filters mounted on a wheel; in addition, for the two ultraviolet channels a grating can be selected in the wheel to do slitless spectroscopy with a resolution of ~100.
  • Soft X-ray imaging Telescope (SXT)- The soft X-ray telescope on Astrosat will employ focussing optics and a deep depletion CCD camera at the focal plane to perform X-ray imaging in 0.3-8.0 keV band. The optics will consist of 41 concentric shells of gold-coated conical foil mirrors in an approximate Wolter-I configuration. The focal plane CCD camera will be very similar to that flown on SWIFT XRT. The CCD will be operated at a temperature of about −80 °C by thermoelectric cooling.
  • The LAXPC Instrument - For X-ray timing and low-resolution spectral studies over a broad energy band (3-80 keV) Astrosat will use a cluster of 3 co-aligned identical Large Area X-ray Proportional Counters (LAXPCs), each with a multi-wire-multi-layer configuration and a Field of View of 1° × 1°. These detectors are designed to achieve (I) wide energy band of 3-80 keV, (II) high detection efficiency over the entire energy band, (III) narrow field of view to minimize source confusion, (IV) moderate energy resolution, (V) small internal background and (VI) long lifetime in space.
  • Cadmium Zinc Telluride Imager (CZTI) - Astrosat will carry a hard X-ray imager in the form of CZTI. It will consist of a Pixellated Cadmium-Zinc-Telluride detector array of ~1000 cm2 geometric area. These detectors have very good detection efficiency, close to 100% up to 100 keV, and have a superior energy resolution (~2% at 60 keV) compared to scintillation and proportional counters. Their small pixel size also facilitates medium resolution imaging in hard x-rays. The CZTI will be fitted with a two dimensional coded mask, for imaging purposes. The sky brightness distribution will be obtained by applying a deconvolution procedure to the shadow pattern of the coded mask recorded by the detector.
  • Scanning Sky Monitor (SSM) - The Scanning Sky Monitor will consist of three position sensitive proportional counters, each with a one-dimensional coded mask, very similar in design to the All Sky Monitor on NASA's RXTE satellite. The gas-filled proportional counter will have resistive wires as anodes. The ratio of the output charge on either ends of the wire will provide the position of the x-ray interaction, providing an imaging plane at the detector. The coded mask, consisting of a series of slits, will cast a shadow on the detector, from which the sky brightness distribution will be derived.
  • Charged Particle Monitor (CPM) - A charged particle monitor (CPM) will be included as a part of Astrosat payloads to control the operation of the LAXPC, SXT and SSM. Even though the orbital inclination of the satellite will be 8 deg or less, in about 2/3 of the orbits, the satellite will spend a considerable time (15 – 20 minutes) in the South Atlantic Anomaly (SAA) region which has high fluxes of low energy protons and electrons. The high voltage will be lowered or put off using data from CPM when the satellite enters the SAA region to prevent damage to the detectors as well as to minimize ageing effect in the Proportional Counters.
Ground support[edit]
The Ground Command and Control Centre for Astrosat will be located at ISAC, Bangalore, India. Commanding and data download will be possible during every visible pass over Bangalore. Ten out of 14 orbits per day will be visible to the ground station. The satellite is capable of gathering 420 gigabits of data every day that can be down loaded in 10 to 11 orbits visible at Tracking and Data receiving center of ISRO in Bangalore.[citation needed] A third 11-meter antenna at the Indian Deep Space Network (IDSN) was operational in July 2009 to track Astrosat.
Current status[edit]
April 2009 : Scientists from Tata Institute of Fundamental Research (TIFR) have completed the developmental phase of complex science payloads and have begun integrating them before delivery of the 1,650 kg satellite Astrosat. A payload from RRI (Raman Research Institute) is under development, awaiting delivery. The challenges in the design of payloads and Attitude Control System have been overcome and in a recent review committee meeting, it was decided that the delivery of the payload to ISRO satellite Centre will begin from the middle of 2009 and continue till early 2010 to enable the launch of ASTROSAT in 2010 using ISRO workhorse PSLV.[6]
Two of the instruments were harder than expected to complete. "The satellite’s soft x-ray telescope proved to be a huge challenge that took 11 years..."[2] As of April 2012, the launch has been rescheduled to 2014.[1]
Participants[edit]
The Astrosat project is a collaborative effort of a growing list of research institutions. The current participants are:


Payloads

astrosat_table_1.png
Hey, do you know I am doing the GEANT4 simulation of astrosat LAXPC detectors ? Also I am part of the CZTl detector. he he he. Son going to publish the paper.

Isro to launch Astrosat to study the skies - The Times of India



MANGALORE: Indian Space Research Organisation (ISRO) is in the process of launching Astrosat to study the skies over India and thereby give a great contribution from India to the study of astronomy, said K Radhakrishnan, secretary, department of space, and chairman, space commission and ISRO. Astrosat will be launched aboard a PSLV in 2015, will have six instruments and can be described as a multi wave length observatory in space.

Delivering the 32nd annual convocation address of Mangalore University here on Monday and giving an insight into ISROs future space programmes, Radhakrishnan said earth observation capabilities too is high on ISROs agenda with plans afoot to study objects 0.25 metres on the ground with satellites that are 500-600kms in space. "We will use heavy high powered satellites for this," he said. Studying the skies too will be taken up with Astrosat.

This satellite will have ultra-violet, visible and x-ray instruments. It is getting ready now, he said, adding that the satellite will be integrated by 2015. The instruments that will be used on board Astrosat are being built by several institutions across India including the Tata Institute of Fundamental Research, Mumbai, the Indian Institute of Astrophysics, Bangalore, and at ISRO itself, Radhakrishnan noted adding this is a joint effort of various institutions.

Dwelling on two critical missions that ISRO embarked upon in recent past, Radhakrishnan said, in November last Mars orbiter spacecraft embarked on a journey towards Mars, making it the first Made In India object to leave the Earth's sphere of influence. The Mars orbiter is on course for its arrival near Mars on September 24, 2014, he said adding that the crucial operation of reducing its velocity and placing it around Mars will take place then.

The successful flight test of cryogenic stage in the beginning of this year is another milestone in space programme. Noting the success as result of hard work of teams for two decades and development of a host of test facility and infrastructure, Radhakrishnan said nearly 850 wind tunnel tests and 45 ground tests were conducted before proceeding for flight. Several hard technical and managerial decisions had to be arrived at for its success, he noted.


Astrosat - Wikipedia, the free encyclopedia

Astrosat is India's first dedicated astronomy satellite and is scheduled to launch on board the PSLV in 2014.[1]
After the success of the satellite-borne Indian X-ray Astronomy Experiment (IXAE), which was launched in 1996, the Indian Space Research Organization (ISRO) approved (in 2004) further development for a full fledged astronomy satellite: Astrosat. It was originally hoped to be launched about 2008/9.[2]
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 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 visible (320-530 nm), near UV (180-300 nm), far UV (130-180 nm), soft X-ray (0.3-8 keV and 2-10 keV) and hard X-ray (3-80 keV and 10-150 keV) regions of the electromagnetic spectrum.












Launch date2015 (planned)
Launch siteSatish Dhawan Space Centre
Launch vehiclePSLV-XL
Mission length5 years
Mass1,650 kg (3,640 lb)
Type of orbitNear-equatorial
Orbit height650 km (400 mi)
Orbit period5 years
WavelengthMulti-wavelength
Instruments
UVITUltraViolet Imaging Telescope
SXTSoft X-ray telescope
LAXPCX-ray timing and low-resolution spectral studies
CZTIHard X-ray imager




Mission[edit]


Artist's conception of a binary star system with one black hole and one main sequence star
Astrosat will be a proposal-driven general purpose observatory, with main scientific focus on:
  • Simultaneous multi-wavelength monitoring of intensity variations in a broad range of cosmic sources
  • Monitoring the X-ray sky for new transients
  • Sky surveys 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
Astrosat will carry out multi-wavelength observations covering spectral bands from radio, optical, IR, UV, X-ray and Gamma ray regions both for study of specific sources of interest and in survey mode. While radio, optical, IR observations would be coordinated through ground-based telescopes, the high energy regions, i.e., UV, X-rays and Gamma rays would be covered by the dedicated satellite borne instrumentation of Astrosat.[3]
The mission would also study near simultaneous muti-wavelength data from different variable sources. In a binary system, for example, regions near the compact object emit predominantly in X-rays, the accretion disc emitting most of its light in the UV/optical waveband, whereas the mass of the donating star is brightest in the optical band.
The observatory will also carry out:
  1. Low to moderate resolution spectroscopy over wide energy band with the primary emphasis on studies of X-ray emitting objects
  2. Timing studies of periodic and aperiodic phenomenon in X-ray binaries
  3. Studies of pulsations in X-ray pulsars
  4. QPOs, flickering, flaring, and other variations in X-ray binaries
  5. Short and long term intensity variations in AGNs
  6. Time lag studies in low/hard X-rays and UV/optical radiation
  7. Detection and study of x-ray transients.[4]
In particular, the mission will train its instruments at active galactic nuclei at the core of the Milky Way that is believed to have a super massive black hole.[5]
Payloads[edit]
The scientific payload has a total mass of 750 kg and contains six instruments.
  • The UltraViolet Imaging Telescope (UVIT) - The UltraViolet Imaging Telescope will perform imaging simultaneously in three channels: 130-180 nm, 180-300 nm, and 320-530 nm. The field of view is a circle of ~ 28 arcmin diameter and the angular resolution is 1.8" for the ultraviolet channels and 2.5" for the visible channel. In each of the three channels a spectral band can be selected through a set of filters mounted on a wheel; in addition, for the two ultraviolet channels a grating can be selected in the wheel to do slitless spectroscopy with a resolution of ~100.
  • Soft X-ray imaging Telescope (SXT)- The soft X-ray telescope on Astrosat will employ focussing optics and a deep depletion CCD camera at the focal plane to perform X-ray imaging in 0.3-8.0 keV band. The optics will consist of 41 concentric shells of gold-coated conical foil mirrors in an approximate Wolter-I configuration. The focal plane CCD camera will be very similar to that flown on SWIFT XRT. The CCD will be operated at a temperature of about −80 °C by thermoelectric cooling.
  • The LAXPC Instrument - For X-ray timing and low-resolution spectral studies over a broad energy band (3-80 keV) Astrosat will use a cluster of 3 co-aligned identical Large Area X-ray Proportional Counters (LAXPCs), each with a multi-wire-multi-layer configuration and a Field of View of 1° × 1°. These detectors are designed to achieve (I) wide energy band of 3-80 keV, (II) high detection efficiency over the entire energy band, (III) narrow field of view to minimize source confusion, (IV) moderate energy resolution, (V) small internal background and (VI) long lifetime in space.
  • Cadmium Zinc Telluride Imager (CZTI) - Astrosat will carry a hard X-ray imager in the form of CZTI. It will consist of a Pixellated Cadmium-Zinc-Telluride detector array of ~1000 cm2 geometric area. These detectors have very good detection efficiency, close to 100% up to 100 keV, and have a superior energy resolution (~2% at 60 keV) compared to scintillation and proportional counters. Their small pixel size also facilitates medium resolution imaging in hard x-rays. The CZTI will be fitted with a two dimensional coded mask, for imaging purposes. The sky brightness distribution will be obtained by applying a deconvolution procedure to the shadow pattern of the coded mask recorded by the detector.
  • Scanning Sky Monitor (SSM) - The Scanning Sky Monitor will consist of three position sensitive proportional counters, each with a one-dimensional coded mask, very similar in design to the All Sky Monitor on NASA's RXTE satellite. The gas-filled proportional counter will have resistive wires as anodes. The ratio of the output charge on either ends of the wire will provide the position of the x-ray interaction, providing an imaging plane at the detector. The coded mask, consisting of a series of slits, will cast a shadow on the detector, from which the sky brightness distribution will be derived.
  • Charged Particle Monitor (CPM) - A charged particle monitor (CPM) will be included as a part of Astrosat payloads to control the operation of the LAXPC, SXT and SSM. Even though the orbital inclination of the satellite will be 8 deg or less, in about 2/3 of the orbits, the satellite will spend a considerable time (15 – 20 minutes) in the South Atlantic Anomaly (SAA) region which has high fluxes of low energy protons and electrons. The high voltage will be lowered or put off using data from CPM when the satellite enters the SAA region to prevent damage to the detectors as well as to minimize ageing effect in the Proportional Counters.
Ground support[edit]
The Ground Command and Control Centre for Astrosat will be located at ISAC, Bangalore, India. Commanding and data download will be possible during every visible pass over Bangalore. Ten out of 14 orbits per day will be visible to the ground station. The satellite is capable of gathering 420 gigabits of data every day that can be down loaded in 10 to 11 orbits visible at Tracking and Data receiving center of ISRO in Bangalore.[citation needed] A third 11-meter antenna at the Indian Deep Space Network (IDSN) was operational in July 2009 to track Astrosat.
Current status[edit]
April 2009 : Scientists from Tata Institute of Fundamental Research (TIFR) have completed the developmental phase of complex science payloads and have begun integrating them before delivery of the 1,650 kg satellite Astrosat. A payload from RRI (Raman Research Institute) is under development, awaiting delivery. The challenges in the design of payloads and Attitude Control System have been overcome and in a recent review committee meeting, it was decided that the delivery of the payload to ISRO satellite Centre will begin from the middle of 2009 and continue till early 2010 to enable the launch of ASTROSAT in 2010 using ISRO workhorse PSLV.[6]
Two of the instruments were harder than expected to complete. "The satellite’s soft x-ray telescope proved to be a huge challenge that took 11 years..."[2] As of April 2012, the launch has been rescheduled to 2014.[1]
Participants[edit]
The Astrosat project is a collaborative effort of a growing list of research institutions. The current participants are:


Payloads

astrosat_table_1.png
Hey, do you know I am doing the GEANT4 simulation of astrosat LAXPC detectors ? Also I am part of the CZTl detector. he he he. Son going to publish the paper.
 
Hey, do you know I am doing the GEANT4 simulation of astrosat LAXPC detectors ? Also I am part of the CZTl detector. he he he. Son going to publish the paper.


Hey, do you know I am doing the GEANT4 simulation of astrosat LAXPC detectors ? Also I am part of the CZTl detector. he he he. Son going to publish the paper.

Great ! you should tell us more about CZTI detector and LAXPC then ...

You are lucky to have opportunity to work on such grand project ...Congrats !
 
Great ! you should tell us more about CZTI detector and LAXPC then ...

You are lucky to have opportunity to work on such grand project ...Congrats !
LAXPC is Large Area Xenon Proportional Counter, having 12 anode cells(individual counters) in row and 5 in a column. That constitute 1 unit. ASTROSAT has 3 such units. Each anode cw3ll is filled with 90% Xenon + 10 % methane. A central anode wire of thickness around 20 micron is there. Each LAXPC unit is covered by Aluminized Mylar Sheet of 25-50 micron. The gas pressure is 2~3 atmosphere and the anode voltage is around 3000 volt. rest of the information is classified.
 
LAXPC is Large Area Xenon Proportional Counter, having 12 anode cells(individual counters) in row and 5 in a column. That constitute 1 unit. ASTROSAT has 3 such units. Each anode cw3ll is filled with 90% Xenon + 10 % methane. A central anode wire of thickness around 20 micron is there. Each LAXPC unit is covered by Aluminized Mylar Sheet of 25-50 micron. The gas pressure is 2~3 atmosphere and the anode voltage is around 3000 volt. rest of the information is classified.

are these both instruments totally indigenous ?

why the information is classified if these are just scientific payloads ?

How and what are you planning to publish paper of otherwise classified project ?
 
are these both instruments totally indigenous ?

why the information is classified if these are just scientific payloads ?

How and what are you planning to publish paper of otherwise classified project ?

Yes . these instruments are indigenous, made by TIFR, IUCAA, IIT etc. I have not yet published the results. so I can not give you the information. That is why I said it is classified. Recently I have delivered a seminar on my simulation results in an international seminar where some of these Astrosat people were there. I will publish it in ELSEVIER. One of my publication you can see on ELSEVIER in this link.

Influence of microscopic particle interaction models on the flux of atmospheric antiprotons

Like this, I will publish. I am waiting waiting for the final experimental results of this instrument.
 
Yes . these instruments are indigenous, made by TIFR, IUCAA, IIT etc. I have not yet published the results. so I can not give you the information. That is why I said it is classified. Recently I have delivered a seminar on my simulation results in an international seminar where some of these Astrosat people were there. I will publish it in ELSEVIER. One of my publication you can see on ELSEVIER in this link.

Influence of microscopic particle interaction models on the flux of atmospheric antiprotons

Like this, I will publish. I am waiting waiting for the final experimental results of this instrument.

Is this project funded by GOI or institutes have used intramural funding ?
Do you have any idea regarding cost of these projects ?

and can you elaborate little bit more about scientific objectives of these instruments ...

Is there anything unique or special about Astrosat ? and how does it compare with other international projects of same nature ?
 
Is this project funded by GOI or institutes have used intramural funding ?
Do you have any idea regarding cost of these projects ?

and can you elaborate little bit more about scientific objectives of these instruments ...

Is there anything unique or special about Astrosat ? and how does it compare with other international projects of same nature ?
Now this is the problem. That is why I said most of the information I can not furnish now. It is funded by GOI. Scientific objective is same as other missions like FERMI or RXTe etc. But regarding uniqueness, I can not say anything now. I am sorry. I will let you know within 2 months. There is a reason why this launch was delayed time to time. it was schedule to launch 2010-11. But the launch was postponed because of a reason. I can not tell you that reason now. Let me publish first.
 
Now this is the problem. That is why I said most of the information I can not furnish now. It is funded by GOI. Scientific objective is same as other missions like FERMI or RXTe etc. But regarding uniqueness, I can not say anything now. I am sorry. I will let you know within 2 months. There is a reason why this launch was delayed time to time. it was schedule to launch 2010-11. But the launch was postponed because of a reason. I can not tell you that reason now. Let me publish first.

Sure...can understand your constrain...and will await time of your publication. hope you will come back and share some thoughts about your work .

Best of luck for your publications as well as eventual fructification of your work in the form of launch of Astrosat .
 
Sure...can understand your constrain...and will await time of your publication. hope you will come back and share some thoughts about your work .

Best of luck for your publications as well as eventual fructification of your work in the form of launch of Astrosat .
thank you. after 3-4 months i will be called as Dr. Biplab Bijay. he he he
 
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