The structural design and thermo-mechanical performance of the FXT for the EP 
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Wang, uan; Eder, Josef; Ma, Jia; Yang, YanJi; Cui, WeiWei; Yang, XiongTao; Duan, XuLiang; Feng, JianChao; Zhang, XiaoFeng; Lu, Bing; Lv, He; Sun, WenXin; Lu, FangJun; Han, DaWei; Wang, YuSa; Chen, Tianxiang; Zhang, Qian; Bi, Xiyan; Li, DongTai; Zhang, JiaWei; Friedrich, Peter; Hartmann, Katinka; Keereman, Arnoud; Santovincenzo, Andrea; Vernani, Dervis; Bianucci, Giovanni; Valsecchi, Giuseppe; Tang, QingJun; Chen, HouLei; Chen, Yong

doi:10.1007/s10686-023-09889-6

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The structural design and thermo-mechanical performance of the FXT for the EP mission

Wang, u., Eder, J., Ma, J., Yang, Y., Cui, W., Yang, X., et al. (2023). The structural design and thermo-mechanical performance of the FXT for the EP mission. Experimental Astronomy. doi:10.1007/s10686-023-09889-6.

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Item Permalink: https://hdl.handle.net/21.11116/0000-000D-0233-7 Version Permalink: https://hdl.handle.net/21.11116/0000-000D-0234-6

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Creators:
Wang, uan, Author
Eder, Josef¹, Author
Ma, Jia, Author
Yang, YanJi, Author
Cui, WeiWei, Author
Yang, XiongTao, Author
Duan, XuLiang, Author
Feng, JianChao, Author
Zhang, XiaoFeng, Author
Lu, Bing, Author
Lv, He, Author
Sun, WenXin, Author
Lu, FangJun, Author
Han, DaWei, Author
Wang, YuSa, Author
Chen, Tianxiang, Author
Zhang, Qian, Author
Bi, Xiyan, Author
Li, DongTai, Author
Zhang, JiaWei, Author
Friedrich, Peter¹, Author Hartmann, Katinka¹, Author Keereman, Arnoud, AuthorSantovincenzo, Andrea, AuthorVernani, Dervis, AuthorBianucci, Giovanni, AuthorValsecchi, Giuseppe, AuthorTang, QingJun, AuthorChen, HouLei, AuthorChen, Yong, Author more..

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1High Energy Astrophysics, MPI for Extraterrestrial Physics, Max Planck Society, ou_159890

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Abstract: The Follow-up X-ray Telescope (FXT) is one of the key payloads onboard EP. It is a Wolter-I type X-ray focusing telescope equipped with two telescope modules (focal length 1.6 m), with a total effective area of ~ 600 cm2 at 1.25 keV and an energy range of 0.3–10 keV. FXT is mainly composed of an X-ray focusing mirror assembly (MA) and a camera assembly with a PNCCD detector module. The two FXT modules are completely independent from each other, thus avoiding a single point failure. We completed the internal composites of FXT structural design, which meets the function and performance requirements of mechanical, thermal, contamination control and X-ray optics. The FXT passed successfully the mechanical, thermal qualification level tests on the spacecraft platform in the phase C.

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Language(s): eng - English

Dates: Published Online: 2023-02-01

Publication Status: Published online

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Rev. Type: Peer

Identifiers: DOI: 10.1007/s10686-023-09889-6

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Title: Experimental Astronomy

Abbreviation : Exp. Astron.

Source Genre: Journal

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Pages: - Volume / Issue: - Sequence Number: - Start / End Page: - Identifier: ISSN: 0922-6435
ISSN: 1572-9508