The Imaging X-ray Polarimetry Explorer (IXPE) will add polarization to the properties (time, energy, and position) observed in x-ray astronomy. A NASA Astrophysics Small Explorer (SMEX) in partnership with the Italian Space Agency (ASI), IXPE will measure the 2–8-keV polarization of a few dozen sources during the first 2 years following its 2021 launch. The IXPE Observatory includes three identical x-ray telescopes, each comprising a 4-m-focal-length (grazingincidence) mirror module assembly (MMA) and a polarization-sensitive (imaging) detector unit (DU), separated by a deployable optical bench. The Observatory’s Spacecraft provides typical subsystems (mechanical, structural, thermal, power, electrical, telecommunications, etc.), an attitude determination and control subsystem for 3-axis stabilized pointing, and a command and data handling subsystem communicating with the science instrument and the Spacecraft subsystems.
The Imaging X-Ray Polarimetry Explorer (IXPE): technical overview II / O'Dell, S.L., Attinà, P., Baldini, L., Barbanera, M., Baumgartner, W.H., Bellazzini, R., Bladt, J., Bongiorno, S.D., Brez, A., Cavazzuti, E., Citraro, S., Costa, E., Deininger, W.D., Del Monte, E., Dietz, K.L., Di Lalla, N., Donnarumma, I., Elsner, R.F., Fabiani, S., Ferrazzoli, R., et al.. - (2019). (UV, X-Ray, and Gamma-Ray Space Instrumentation for Astronomy XXI 2019 San Diego, California; United States ) [10.1117/12.2530646].
The Imaging X-Ray Polarimetry Explorer (IXPE): technical overview II
Ferrazzoli, Riccardo;Perri, Matteo;Ratheesh, Ajay;Brienza, Daniele;Rankin, John;Sanchez, Javier;
2019
Abstract
The Imaging X-ray Polarimetry Explorer (IXPE) will add polarization to the properties (time, energy, and position) observed in x-ray astronomy. A NASA Astrophysics Small Explorer (SMEX) in partnership with the Italian Space Agency (ASI), IXPE will measure the 2–8-keV polarization of a few dozen sources during the first 2 years following its 2021 launch. The IXPE Observatory includes three identical x-ray telescopes, each comprising a 4-m-focal-length (grazingincidence) mirror module assembly (MMA) and a polarization-sensitive (imaging) detector unit (DU), separated by a deployable optical bench. The Observatory’s Spacecraft provides typical subsystems (mechanical, structural, thermal, power, electrical, telecommunications, etc.), an attitude determination and control subsystem for 3-axis stabilized pointing, and a command and data handling subsystem communicating with the science instrument and the Spacecraft subsystems.| File | Dimensione | Formato | |
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