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Published March 11, 2003 | Published
Book Section - Chapter Open

EXIST: mission design concept and technology program

Abstract

The Energetic X-ray Imaging Survey Telescope (EXIST) is a proposed very large area coded aperture telescope array, incorporting 8m^2 of pixelated Cd-Zn-Te (CZT) detectors, to conduct a full-sky imaging and temporal hard x-ray survey each 95min orbit. With a sensitivity of ~0.05mCrab, it will extend the ROSAT soft x-ray and proposed ROSITA medium x-ray surveys into the hard x-ray band and enable identifiaiton and study of sources ~10-20X fainter than with the ~15-100keV survey planned for the upcoming Swift mission. At ~100-600keV, the ~1mCrab sensitivity is 300X that achieved in the only previous all-sky survey. EXIST will address a broad range of key science objectives: from obscured AGN and surveys for black holes on all scales, which constrain the acretion history of the universe, to the highest sensitivity and resolution studies of gamma-ray bursts it will conduct as the Next Generation Gamma-Ray Burst mission. We summarize the science objectives and mission drivers, and the results of a mission design study for implementation as a free flyer mission, with Delta IV launch. Key issues affecting the telescope and detector design are discussed, and a summary of some of the current design concepts being studied in support of EXIST is presented for the wide-field but high resolutoin coded aperture imaging and very large area array of imaging CZT detectors. Overall mission design is summarized, and technology development needs and a development program are outlined which would enable the launch of EXIST by the end of the decade, as recommended by the NAS/NRC Decadal Survey.

Additional Information

© 2003 Society of Photo-Optical Instrumentation Engineers (SPIE). We thank the EXIST Science Working Group (see http://existgsfc.nasa.gov) for input on the mission science and goals, S. Barthelmy, A. Parsons, C. Hailey and G. Fishman for technical assistance in the ISAL and IMDC mission studies at GSFC, R. Carter and S. DePaolo for management of the mission study at GSFC, T. Narita, J. Jenkins and W. Cook for detector and readout design discussions, and T. Decker and R. Hill for mechanical design assistance. This work was supported in part by NASA SR&T grant NAG5-5729 and support from NASA HQ for the design studies at GSFC is gratefully acknowledged.

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