1. The Small Satellite-Based, Imaging X-Ray Polarimeter Explorer (IXPE) Mission
- Author
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Deininger, W. D., Masciarelli, J., Kalinowski, W., Hibbard, G., Wedmore, J., Gray, S., Ferrie, M., Dolan, D., Onizuka, M., Seek, T., Sharma, D., Mitchell, S., Ferrant, K., Boree, C., Antoniak, S., Mize, R., Alexander, C., Foster, M., O'Dell, S. L., Ramsey, B. D., Santoli, F., Pinchera, M., Minuti, M., Trois, A., Monte, E. Del, and Muleri, F.
- Subjects
explorer ,x-ray ,mission ,Astrophysics::High Energy Astrophysical Phenomena ,polarimeter ,satellite ,Astrophysics::Instrumentation and Methods for Astrophysics ,imaging ,base ,small - Abstract
The Imaging X-ray Polarimeter Explorer (IXPE) focuses on high energy astrophysics in the 2—8 keV x-ray band. IXPE is designed to explore general relativistic and quantum physics effects of gravity, energy, electric and magnetic fields at extreme limits. IXPE, a NASA Small Explorer (SMEX) Mission, will add new dimensions to on-orbit x-ray science: polarization degree, polarization angle and extended object polarization imaging. Polarization uniquely probes physical anisotropies that are not otherwise measurable—ordered magnetic fields, aspheric matter distributions, or general relativistic coupling to black-hole spin. Detailed imaging enables the specific properties of extended x-ray sources to be differentiated. The IXPE Observatory consists of spacecraft and payload modules built up in parallel to form the Observatory during system integration and test. The payload includes three polarization-sensitive, x-ray detector arrays paired with three x-ray mirror module assemblies (MMA). A deployable boom provides the correct separation (focal length) between the detector units and MMAs. Currently, the boom has been delivered, all four detectors units (DU) are complete, the detectors service unit (DSU) is complete, instrument system testing has been completed (DSU with 3 DUs), three of four MMAs is built and all spacecraft components except the solar array have been delivered along with the spacecraft and payload structures. Payload and spacecraft integration and test (I&T) started in March 2020. This paper overviews the flight segment (the Observatory, payload, and spacecraft implementation concepts) with emphasis on the build status and summarizes the launch segment. Launch is planned to occur on a Falcon 9 launch vehicle during Summer 2021. The paper summarizes the impacts of switching from the ‘design-to baseline’ of Pegasus XL to the selected launch vehicle for flight, Falcon 9. COVID-19 impacts to the Project are also summarized. The paper will close with a summary of the mission development status. The Project is firmly into the build phase for both the spacecraft and payload and rapidly approaching Observatory I&T.
- Published
- 2020