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Print from page 2 for double-sided prints. ASTRO-H Quick Reference (http://astro-h.isas.jaxa.jp/ahqr.pdf) ASTRO-H Science Office <[email protected]> Contents I. Overview IV. Figures of Merit 1. ASTRO-H mission 2. Spacecraft & Components 3. Parameters 1. 2. 3. 4. II. Telescopes V. Case Studies 1. SXT 2. HXT 1. Black holes 2. Supernova remnants 3. Clusters of galaxies III. Instruments 1. 2. 3. 4. Effective area Limiting sensitivity Energy resolution FoV & Grasp SXS SXI HXI SGD Further information Releases 2010-08-18 For A-H 1st Summer School (N. Ota, M. Tsujimoto) 2010-11-09 HXI & SGD updates (H. Takahashi) 1 I. Overview I-1. ASTRO-H Mission Overview ASTRO-H is an international X-ray observatory, which is the 6th in the series of the X-ray observatories from Japan. It is currently planned to be launched in the fiscal year 2013 with an H-IIA rocket from the Tanegashima Space Center, Kagoshima, Japan. Launch site Tanegashima Space Center Launch vehicle JAXA HII-A rocket Orbit Altitude 550 km Orbit Type Approximate circular orbit Orbit Inclination < 31 degrees Orbit Period 96 minutes Total Length 14 m Mass < 2.6 metric ton Mission life > 3 years Fig. 1 Artist's drawings of the ASTRO-H satellite. Scientific objectives ● Revealing the large-scale structure and its evolution of the Universe ● Understanding the extreme conditions in the Universe ● Exploring the diverse phenomena of non-thermal Universe ● Elucidating dark matter and dark energy Key technologies The ambitious scientific goals are made possible with many novel technologies developed for ASTRO-H, including 1. An X-ray micro-calorimeter detector which enables high resolution (5 eV) spectroscopic observations between 0.3 and 12 keV. 2. Hard X-ray telescopes to provide X-ray images and spectra to 80 keV. 3. Detectors allowing observations over an extremely large energy range of 0.3-600 keV. Fig. 2 Scientific instruments onboard the ASTRO-H satellite and energy coverage. 2 I. Overview I-2. Spacecraft & Components 3 I. Overview I-3. Parameters Table 1 Properties of ASTRO-H telescopes (current best estimate) Properties SXT HXT Diameter (cm) 45 45 Focal length (m) 5.6 12 No. of nested shells 203 213 Reflector coating Aeff (cm2) HPD (arcmin) 2 FoV (arcmin ) multilayer Al (0.03 µm) + PET(5 µm) (0.2 µm) HXT 279/312 338 (@0.5/6keV) (@30keV) 1.3 1.7 22.2 /19.8 2 6.42/5.32 (@0.5/6 keV) (@30/50keV) Stray-light reduction rate >99 (@30' >99 (@15'- off-axis) 25' off-axis) Thermal shield 70 92 transmission (%) (@0.5keV) (@5 keV) Al (0.03 µm) + polyimide SXT 2 Pt/C Au Thermal shield Properties Table 2 Properties of ASTRO-H instruments (current best estimate) SGD SGD (photo-abs) (Compton) 300 150 20 (@0.5/6 keV) (@30 keV) (@30 keV) (@100 keV) 0.3-12.0 0.4-12.0 5-80 10-600 40-600 1.3 1.3 1.7 N/A N/A Properties SXS SXI HXI Effective area 50/225 214/360 (cm2) (@0.5/6 keV) Energy range (keV) Angular resolution in HPD (arcmin) Field of view (arcmin2) Energy resolution in FWHM (eV) 33x33 (<150 keV) 3.05x3.05 38x38 9x9 600x600 (>150 keV) 5 33x33 (<150 keV) 600x600 (>150 keV) 150 < 2000 2000 4000 (@6 keV) (@60 keV) (@40 keV) (@40 keV) several x 10-5 several x 10-5 several x 10-5 Timing resolution (s) 8x10-5 4 Instrumental background 2x10-3/0.7x10-3 0.1/0.1 (/s/keV/FoV) (@0.5/6 keV) (@0.5/6 keV) 6x10-3/2x10-4 (@10/50 keV)1 2x10-3/4x10-5 (@10/50 keV)2 1 4 layers, 21 layer 1x10-4/1x10-5 (@100/600 keV) 4 II. Telescopes II-1. Soft X-ray Telescopes Basics ASTRO-H has two identical Soft X-ray Telescopes (SXTs). One is for SXS (SXT-S) and the other for SXI (SXT-I). SXT is a similar in concept to the X-Ray Telescope (XRT) of Suzaku (table 1). It is composed of 203 thin reflector shells tightly nested confocally and coaxially. A conical approximation of Wolter-I type optics is used. Table 1 Comparison of ASTRO-H/SXT and Suzaku/XRT No. of telescope Focal length (m) Diameter (cm) No. of nested shells HPD (arcmin) SXT 2 5.6 45 203 1.3 560 425 XRT-I 4 4.75 40 175 2.0 470 320 Aeff (cm2)*1 Aeff is the on-axis effective area (mirror only) at 0.5 & 6 keV. Source extraction of r=∞, or 100% photons are encircled. The value for one unit for XRT-I. *1 Technology Three different thicknesses of Al substrates (152, 229, and 305 μm) are used, in which the outer shells use the thicker substrates. This is intended for achieving a large collecting area with a better imaging quality than Suzak/XRT. The considerably better HPD than XRT (table 1) is realized by fixing the reflectors to support bars with adhesive. Stray light, or contaminating X-rays from outside of the field of view, is reduced by a stray-light baffle, which consists of coaxially-nested cylindrical aluminum blades placed above each reflector. A thermal shield is attached in front of the pre-collimator to stabilize the thermal environment of the SXT. The shield is made of Al-coated Polyimide film to ensure a large effective Fig. 1 Schematic view of SXT. The blue and red parts area in the soft energy band. are the mirror housing and pre-collimator, respectively. Performance Fig. 2 Effective area (mirror only) as a function of energy at on-axis and some off-axis angles. Source extraction from a r=1.8' circle (78% encircled energy fraction). Fig. 3 Encircled effective area, representing the sharpness of an image at several energies at on-axis and some off-axis angles. 5 II. Telescopes II-2. Hard X-ray Telescopes Basics ASTRO-H has two identical Hard X-ray Telescopes and the HXIs, with an HXI at the focus of each HXT. The global structure is very similar to that of SXTs, but the focal length, the reflector length, and the reflector coating are optimized for hard (> 10 keV) X-ray imaging. It is composed of 213 nested sets of conically approximated thin-foil Wolter-I type reflectors. Technology The surface of the reflector is coated with a stack of depth-graded Pt/C multi-layer, which reflects hard X-ray photons by Bragg reflection (fig. 1). The mirrors are fabricated by the replication Fig. 1 Schematic view of a Bragg reflection. method, in which a depth-graded Pt/C multi-layer is sputtered onto the smooth surface of a glass tube and transferred to a conically shaped aluminum substrate with epoxy glue. The “pre-collimator”, or the stray-light baffle, is mounted atop the HXT. The thermal shield is integrated on top of the pre-collimator to keep the HXT temperature within a specific range. Performance The current best estimate of the HPD is ~1.7'. The effective area is plotted vs. energy (fig. 3) and off-axis angle (fig. 4). Other performance parameters are being characterized now. Fig. 3 HXT on-axis effective area (one unit) with an interfacial roughness of 3(black), 4(red) and 5 Å(green). The blue points indicate the 1st and 2nd level requirements. Fig. 2 Schematic view of HXT. Fig. 4 The vignetting function at 10 keV (black), 30 keV (red) and 50 keV (green) calculated by the raytracing simulator for the ideal reflector case. The interfacial roughness is 3 Å assumed. 6 III. Instruments III-1. Soft X-ray Spectrometer Basics The Soft X-ray Spectrometer (SXS) is equipped with an X-ray microcalorimeter array of 6x6 pixels at the focus of the Soft X-ray Telescope (SXT), which is capable of nondispersive high-resolution (∆E~5 eV) spectroscopy and limited imaging of 3x3 field of view in the soft X-ray (0.3-12 keV) band with a large effective area. Technology The detector measures the temperature rise upon each incident X-ray photon, achieving an unprecedented energy resolution. The thermometer is made of HgTe absorbers of a 8µm HgTe thickness on micro-machined, ion-implanted Si wafer. The anticoincidence Si semiconductor detector enables rejection of background events. The mK temperature in the dewar is achieved by the cooling system comprised of adiabatic demagnetization refrigerators, He coolants, and mechanical coolers. The cooling Fig. 1 Concept of X-ray micro-calorimetry. system allows redundancy and cryogenic-free operation. The filter wheel provides a suite of attenuation filters to enhance the dynamic range of the SXS. The modulated X-ray source is planned for accurate response calibration. Performance Since the SXS is a non-dispersive spectrometer, it can be used to obtain highresolution spectra of both point and extended sources (fig. 3). The effective area of >200 cm2 at the Fe K-band is considerably larger than any other high-resolution spectrometers. The imaging capability is limited as the HPD is comparable to the FoV (fig. 2). Fig. 2 Pixel layout. The array encompasses ~74% of photons of a point source at the center. Fig. 3 Simulated spectrum of Centaurus cluster. CCD µ-calorimeter Fig. 4 Grade definition. Calorimeter resolution (∆E<10 eV) is obtained only for high-res (HR) and med-res (MR) events. Observation modes SXS has only one observation mode. All X-ray events are graded (fig 4). The digital processor is capable of handling only 250/s ~ 150 mCrab (“PSP limit”). For bright sources, it is beneficial to intentionally Fig. 5 Filter selection. reduce the incoming photons open using filters (fig. 5) and/or 25µm 50µm Be Be disabling center pixels dominated by LR events. 25% ND open OBF Fig. 6 Incident vs. observed rate. 7 III. Instruments III-2. Soft X-ray Imager Basics The Soft X-ray Imager (SXI) is equipped with X-ray CCD devices placed at the focal plane of the Soft X-ray Telescope (SXT-I). The SXI has an imaging-spectroscopic capability of a wide field (38 arcmin2) and a medium energy resolution (E/∆E~40@6keV) at the soft X-ray band (0.4-12 keV). The SXI is a successor of the XIS onboard the Suzaku observatory. Table 1 Comparison of ASTRO-H/SXI and Suzaku/XIS. No. of CCD No. of telescope Layout Pixel scale Format (one CCD) FoV (sq.arc min)*1 SXI 4 1 2x2 array 1.74” 640x 640 38x38 XIS 4 4 4 coaligned 1.04” 1024x 1024 18x18 *1 Grasp (cm2 arcdeg2) Frame time (s) Illumin ation Type Depl. layer (µm) 214 360 40 4 BIx4 p-chan 200 240 950 35 8 FIx3, BIx1 n-chan 80 (FI), 45 (BI) Aeff (cm ) 2 *2 FoV for the 2x2 array for SXI. *2Aeff is the on-axis effective area at 0.5 & 6 keV. Four CCDs combined for XIS. Technology Mechanical coolers will be used to keep the device temperature at -120 C. The p-channel CCD will have a thick depletion layer to extend the hard-band coverage. The thick depletion layer also leads to a significant background reduction above ~7 keV compared to the same BI CCD in Suzaku/XIS. The BI devices is more resistant than the FI devices to micro-meteorite hits, which made a part of the XIS dysfunctional. The design is underway to suppress contamination accumulation on the CCD chips. Onboard calibration source is under discussion. Fig 1. Schematic view. Performance The 2x2 CCD array covers a very large FoV. The nominal position is placed at the center of SXS FoV, which is 4.'3 offset from the SXI center. A gap of ~20” is between the chips. Similarly to XIS, the background level of SXI is expected to be low and stable, benefiting from the low-earth orbit of the satellite. Fig 3. Redistribution of 55Fe source measured with a proto-type CCD. Fig 2. Layout of SXI array and SXS FoV. Observation mode Several CCD clocking mode (partial read and stacking) will be supported for the main purpose of mitigating CCD pile-up. The detail is under discussion. 8 III. Instruments III-3. Hard X-ray Imager Basics The Hard X-ray Imager (HXI) is the detector assembly that comprises the hard X-ray imaging system with the Hard X-ray Telescope (HXT). ASTRO-H has two identical HXT-HXI systems. The HXI is equipped with multi-layered imaging devices, enabling hard X-ray imaging and spectroscopic observations. Technology The detector assembly consists of four-layers of double-sided Si strip detectors (DSSD; 0.5 mm) and one layer of CdTe doublesided strip detector (CdTe DSD; 0.5-1 mm) at the bottom (fig. 1). Soft X-rays (<30 keV) are absorbed by the DSSD, while hard X-rays (2080 keV) penetrate the DSSD and are captured by the newly developed CdTe DSD. The total thickness of the DSSD amounts to 2 mm, which is comparable to the HXD-PIN onboard Suzaku. The fast timing response of both DSSD and CdTe DSD detectors allows us to place the entire detector assembly at the bottom of a very deep well of the active BGO shield, which works as a veto counter. Fig. 1 Schematic view of HXI. Performance The combination of HXI + HXT will obtain images and spectra at 10 -70 keV. The HXI has good energy resolution (fig. 2), and low-level of background due to the use of a BGO active shield. Since each event is read out separately with good time resolution, the HXI can observe bright sources without pile-up. DSSD CdTe DSD ALL (4-layer DSSD + 1-layer CdTe) DSSD Top 1-layer Fig. 2 Energy spectra of DSSD (left) and CdTe DSD (right) detectors with 241Am source. Fig. 3 Detection efficiency of 1layer (0.5 mm-thick) DSSD (black) and all (4-layer DSSD + 1-layer CdTe DSD) of the HXI (red). Observation mode The HXI has only one mode. For data reduction, observers may select events in the following way depending on source fluxes, images (point/diffuse source) and spectra. - Normal (bright/hard) sources : Events detected with all of the HXI detectors. - Faint/soft sources : Events with only the top 1-layer DSSD. Soft X-rays tend to be detected by the top layer, while the background distributes over the entire detectors, especially the CdTe DSD. III. Instruments III-4. Soft γ-ray Detector Basics The SGD is a non-imaging soft gamma-ray detector covering a 10—600 keV energy range at x10 better sensitivity than the Suzaku HXD at 300 keV. It outperforms any previous soft γ-ray instruments in background rejection capability by adopting a new concept of narrow-FoV Compton telescope. SGD also has a polarimeteric capability. Technology A Compton telescope is made up of a stack of Si pad detectors and CdTe pixel detectors, which drastically reduces the background and thus improves the sensitivity. The telescope is mounted at the bottom of a well-type active shield. Incident photons of E>40 keV sometimes interact twice in the stacked detector; once by Compton scattering in the stack of Si pad detectors and another by photoelectric absorption in the CdTe detector (“Compton mode”). With the Compton kinematics, the energy and direction (as a cone in the sky) of each incident γ-ray are derived from the locations and energies of the two interactions. Events from the collimator FoV are selected (narrow FoV Compton telescope). Fig. 1 Schematic views of the SGD (left, middle) and a Compton camera unit (right). The SGD has 6 Compton camera units in total. Performance SGD uniquely performs highly sensitive observations at several hundred keV with a good energy resolution. Each event is read out separately with good time resolution. For Compton events, the SGD has the capability to study the polarization of soft gamma-rays. Fig. 2 Effective area of the Compton mode of the SGD. Fig. 3 Estimated SGD background level of the Compton mode (Red). The neutron background component (green) and the activation background component (blue) are also shown. Observation mode The SGD has only one mode. For data reduction, the following event selection is recommended depending on source flux. - Normal sources : Events detected with the Compton mode. - Bright sources : Events with the photo-absorption mode as well as the Compton mode. 9 10 IV. Figures of Merit IV-1. Effective Area Fig. 1 On-axis effective area of all ASTRO-H telescopes & detectors, SXT-I+SXI, SXT-S+SXS, HXT+HXI (2 units). Fig. 2 SXT-S+SXS on-axis effective area with filter: the open filter(red), optical blocking filter(black), 25μm/50μm Be filter (green/blue). Fig. 3 On-axis effective area of ASTRO-H, Suzaku (XIS-BI+XIS-2FI, HXD), Chandra (ACIS-S), XMM (PN+MOS1+MOS2), and NuSTAR. IV. Figures of Merit IV-2. Limiting Sensitivity Fig. 1 3σ sensitivity targets for the SXI, HXI, and SGD for continuum emissions from point source (the upper panel) and extended sources (the bottom panel) assuming an exposure time of 100 ks, and comparison with other hard X-ray instruments (Tajima et al. 2010 Proc. of SPIE). 11 12 IV. Figures of Merit IV-3. Energy Resolution (i) Strong line: FOM ~ √A (ii) Weak line: FOM ~ √(A/ΔE) (iii) Strong line: FOM ~ √(A E2/ΔE2) (iv) Weak line: FOM ~ √(A E2/ΔE3) (v) Strong line: FOM ~ √(A E4/ΔE4) (vi) Weak line: FOM ~ √(A E4/ΔE5) Fig. 1 Figures of merit (FOM) for (i) detection of strong line, (ii) detection of weak line, (iii) velocity of strong line, (iv) velocity of weak line, (v) broadening of strong line, (vi) broadening of weak line. IV. Figures of Merit IV-4. FoV and Grasp Fig. 1 Field of views of the ASTRO-H instruments, SXS, SXI, HXI (the red boxes). Chandra ACIS-I and XMM are also shown for comparison. The background image is the Coma cluster taken with ROSAT (credit: ROSAT/MPE/S. L. Snowden). Fig. 2 Grasp vs on-axis effective area at 7 keV of SXT-I+SXI, SXT-S+SXS. Suzaku XIS, Chandra ACIS-I, XMM PN are also shown for comparison. 13 14 V. Case Studies V-1. Black Holes ASTRO-H provides an unprecedented view of the motions and extreme physical conditions of matter near the event horizon. This will help us unravel how black holes grow by accreting gas and simultaneously shape their environments via the intense radiation fields and powerful, sometimes relativistic, matter outflows that accompany this accretion. Gaseous winds driven from black hole disks can carry away a substantial fraction of the gas that would otherwise accrete onto the central black hole. Such winds are hot, and most easily detected in the Fe K band via absorption lines. As shown in fig. 1, the superior resolution of SXS in the Fe K band enables the unambiguous detection of weak and narrow lines from a wind. We will be able to use these to precisely determine the radius at which the wind is launched and the mass outflow rate carried by it. This will give us strong constraints on the driving mechanism of the wind and its feedback on the accretion flow as well as the black hole’s environment. logNH=23.7 24 24.7 25 Instrumental BGD limit Fig. 1 A simulated spectrum of the black hole GRO J1655-40 with a 100ks SXS observation. The model is based on a prior Chandra observation. Fig. 2 Simulated HXI spectra of heavily obscured AGN with different absorbing columns (NH) for an exposure of 100ks (300ks for logNH=25). The continuum is assumed to be a power-law of photon index 1.9 with an intrinsic 2-10 keV flux of 1x10-11 erg/s/cm2 (based on Swift J0601.9-8636, Ueda et al. 2007). ASTRO-H will also give us key observations to investigate the co-evolution of supermassive black holes and their host galaxies. Recent observations imply the existence of a large number of Active Galactic Nuclei (AGN) that are heavily obscured by the gas and dust surrounding their supermassive black holes. Some are identified as a "new type" of AGN, so deeply buried in dense tori of gas that they show little emission in soft X-ray and visible light. While this has made such objects extremely difficult to detect and observe, this highly obscured activity may in fact represent the dominant phase of supermassive black hole growth. Understanding this phase is thus key to understanding the correlated evolution of the black hole and its host galaxy. As shown in fig. 2, the high sensitivity for hard X-rays provided by HXI allows precise spectral studies of even very obscured AGN. ASTRO-H will provide us with a large AGN sample to pursue systematic studies of the true AGN population, unbiased by obscuration effects, and to measure the co-evolution of supermassive black holes with their host galaxies. 15 V. Case Studies V-2. Supernova Remnants The high resolution X-ray spectroscopy provided by SXS will be particularly ground-breaking for supernova remnants (SNRs) because they are extended objects with rich emission-line spectra from a wide range of different elements (carbon through nickel). To determine the element abundances reliably, measurements of the relative strengths of a number of lines from each elemental species are required. Accurate element abundances provide constraints to test the explosion mechanisms of supernovae and to explore their environments. Gas motions of the rapidly expanding supernova ejecta and swept-up interstellar and/or circumstellar medium may also be measured by SXS by their Doppler shifts. Gas moving toward or away from us will show shifts in the energies of the emission lines. Velocity measurements are needed to understand how SNRs evolve, based on their age and the detailed properties of the explosion, the ejecta, and ambient medium. Fig. 1 Simulated spectra of the iron K-shell complex from the inner region of the Tycho SNR with an exposure of 100 ks with SXS. The ion temperature is assumed to be 30 billion degrees (black) or negligible (green). Red- and blue-shifted lines from the fast moving gas can be readily resolved with SXS. Particle acceleration is receiving much attention at present, but the origin of cosmic rays is still unclear 100 years after their discovery. Young SNRs with shock speeds of several 1000 km/s are among the best candidates to accelerate cosmic rays up to the knee around 10 15 eV (the highest energy accessible to Galactic accelerators). The combination of ASTRO-H's hard X-ray imaging capability and high spectral resolution will provide information to understand crucial aspects of shock acceleration in SNRs such as the maximum energy of the accelerated particles, the conditions at the acceleration sites, and the acceleration efficiency. Fig. 2 Simulated 100ks HXI image of the SN 1006 NE shell. 16 V. Case Studies V-3. Clusters of Galaxies The dominant baryonic matter component in galaxy clusters is hot intergalactic gas, heated by shocks during violent cluster mergers. By observing its emission lines with calorimetric energy resolution, the SXS will be able to detect turbulence and gas flows generated during such mergers, which may persist for billions of years. Understanding kinematics of the cluster gas is of great importance for the physics of cluster formation and for “precision cosmology”. In bright cluster cores, the SXS will be able to resolve a tangle of lines from different ions, while the low-background SXI will map the gas temperatures far in the cluster outskirts. Intracluster shocks and turbulence are believed to produce ultra-relativistic cosmic rays, which create faint radio synchrotron halos and “relics”. The HXI will detect non-thermal emission from the brightest relics, vastly enhancing our understanding of cosmic ray generation. Simulated spectra below give a sample of measurements that will push ASTRO-H capabilities to the limit. In a low surface brightness region of a nearby merging cluster A3667, the SXS will be able to detect turbulence with a Mach number (the speed of the flow compared to the speed of sound) as low as M=0.2. For the bright radio relic in A3667, believed to trace an outlying shock front, the HXI will disentangle thermal emission from the intra-cluster gas (observed by XMM) and Inverse Compton emission from ultra-relativistic electrons, producing the first unbiased estimate of the energy in cosmic rays and the cluster magnetic field. HXI spectrum of the relic in A3667 HXI IC (assuming B=1μG) T=5 keV radio contours (synchrotron emission) 100 ks A3667 z=0.05 SXS spectrum of a low-brightness region Chandra image (thermal emission) SXS 500 kpc 17 Further Information Web pages ● ASTRO-H <http://astro-h.isas.jaxa.jp/> References ● ● ● ● ● ● ● [ASTRO-H] Takahashi et al. 2010, Proc. of SPIE [SXS] Mitsuda et al. 2010, Proc. of SPIE [SXI] Tsunemi et al. 2010, Proc. of SPIE [HXI] Kokubun et al. 2010, Proc. of SPIE [SGD] Tajima et al. 2010, Proc. of SPIE [SXT] Serlemitsos et al. 2010, Proc. of SPIE [HXT] Kunieda et al. 2010, Proc. of SPIE Mailing lists ● ● ● ASTRO-H collaboration (all members) <[email protected]> Science office <[email protected]> Calibration & Software board <[email protected]> Points of Contact (Questions specific to sub-systems) [SXS] Naomi Ota (Nara Women's U.) <[email protected]> [SXI] Nasayoshi Nobukawa (Kyoto U.) <[email protected]> [HXI] Hiromitsu Takahashi (Hiroshima U.) <[email protected]> [SGD] Hiromitsu Takahashi (Hiroshima U.) <[email protected]> [SXT] Yoshito Haba (Nagoya U.) <[email protected]> [HXT] Yoshito Haba (Nagoya U.) <[email protected]> Science Task Force Leaders Stars & WDs : Jelle Kaastra (SRON) Compact objects : Jon M. Miller (Michigan) Particle acceleration : Felix Aharonian (DIAS) Supermassive black holes and their environments : Chris Reynolds (Maryland) Cluster dynamics and evolution : Maxim Markevitch (Harvard/CfA) Chemical evolution : John P. Huges (Rutgers) Feedback phenomena : Andy Fabian (Cambridge) Cosmology and GRBs : Tetsu Kitayama (Toho) Radiation processes : Frits Paerels (Columbia) Multi-wavelength follow-up and transients : Paolo Coppi (Yale)