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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Bulgarelli, Andrea
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (10/10 displayed)
- 2018Magnetic shielding of soft protons in future X-ray telescopes: the case of the ATHENA Wide Field Imagercitations
- 2014DAS: A Data Management System for Instrument Tests and Operations
- 2014CIWS-FW: A Customizable Instrument Workstation Software Framework for Instrument-independent Data Handling
- 2009SuperAGILE Data Processing Services
- 2008A magnetic diverter for charged particle background rejection in the SIMBOL-X telescopecitations
- 2006The Mini-Calorimeter detector for the AGILE missioncitations
- 2004The Test Equipment of the AGILE Minicalorimeter Prototype
- 2004AGILE, a satellite for high energy γ-ray astrophysics: prospects for the Mini-Calorimetercitations
- 2004The mini-calorimeter of the AGILE satellite
- 2004The MCAL science console software for the minicalorimeter of the AGILE missioncitations
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article
The Test Equipment of the AGILE Minicalorimeter Prototype
Abstract
AGILE is an ASI (Italian Space Agency) Small Space Mission for high energy astrophysics in the range 30 MeV - 50 GeV. The AGILE satellite is currently in the C phase and is planned to be launched in 2005. The Payload shall consist of a Tungsten-Silicon Tracker, a CsI Minicalorimeter, an anticoincidence system and a X-Ray detector sensitive in the 10-40 KeV range. The purpose of the Minicalorimeter (MCAL) is twofold. It shall work in conjunction with the Tracker in order to evaluate the energy of the interacting photons, and it shall operate autonomously in the energy range 250KeV-250 MeV for detection of transients and gamma ray burst events and for the measurement of gamma ray background fluctuations. We present the architecture of the Test Equipment we have designed and developed in order to test and verify the MCAL Simplified Electrical Model prototype which has been manufactured in order to validate the design of the MCAL Proto Flight Model.