eprintid: 10198831 rev_number: 10 eprint_status: archive userid: 699 dir: disk0/10/19/88/31 datestamp: 2024-10-24 10:06:44 lastmod: 2024-10-24 10:06:44 status_changed: 2024-10-24 10:06:44 type: proceedings_section metadata_visibility: show sword_depositor: 699 creators_name: Kataza, H creators_name: Kano, R creators_name: Gouda, N creators_name: Hirabayashi, M creators_name: Isobe, N creators_name: Kamizuka, T creators_name: Kashima, S creators_name: Kawahara, H creators_name: Kawata, D creators_name: Kohara, N creators_name: Kondo, I creators_name: Mase, I creators_name: Miyakawa, K creators_name: Ohsawa, R creators_name: Ozaki, M creators_name: Shimizu, R creators_name: Suematsu, Y creators_name: Tada, S creators_name: Tsuzuki, T creators_name: Uraguchi, F creators_name: Usui, F creators_name: Utsunomiya, S creators_name: Wada, T creators_name: Yamada, Y creators_name: Yano, T title: Conceptual design of the satellite payload for the JASMINE mission ispublished: pub divisions: UCL divisions: B04 divisions: C06 divisions: F63 note: This version is the version of record. For information on re-use, please refer to the publisher's terms and conditions. abstract: To investigate the evolution of our Galaxy, we plan to measure the distances and motions of stars in the Galactic center region. Additionally, our goal is to detect planets within the habitable zone around mid-M-type stars using transit phenomena. To achieve these objectives, we initiated the Japan Astrometry Satellite Mission for Infrared Exploration (JASMINE) project, targeting a 40 microarcsecond annual parallax measurement and aiming photometric accuracy of less than 0.3% for mid-M-type stars. A conceptual study of the observation instrument was conducted. As a result, the telescope is designed with high stability in orbit through carefully chosen materials and a special thermal design. A three-year operation is planned to collect sufficient data for annual parallax measurements. The telescope, with a diameter of 36 cm, covers wavelengths from 1.0 to 1.6 microns using InGaAs detectors. This paper will detail how instrument parameters were selected based on scientific objectives. date: 2024 date_type: published publisher: Society of Photo-Optical Instrumentation Engineers (SPIE) official_url: http://dx.doi.org/10.1117/12.3018609 oa_status: green full_text_type: pub language: eng primo: open primo_central: open_green verified: verified_manual elements_id: 2328918 doi: 10.1117/12.3018609 lyricists_name: Kawata, Daisuke lyricists_id: DKAWA39 actors_name: Flynn, Bernadette actors_id: BFFLY94 actors_role: owner full_text_status: public pres_type: paper publication: Proceedings of SPIE - The International Society for Optical Engineering volume: 13092 pagerange: 1-9 event_title: Space Telescopes and Instrumentation 2024: Optical, Infrared, and Millimeter Wave event_location: Yokohama, Japan event_dates: 16th-22nd June 2024 book_title: Proceedings of SPIE - The International Society for Optical Engineering editors_name: Coyle, Laura E editors_name: Perrin, Marshall D editors_name: Matsuura, Shuji citation: Kataza, H; Kano, R; Gouda, N; Hirabayashi, M; Isobe, N; Kamizuka, T; Kashima, S; ... Yano, T; + view all <#> Kataza, H; Kano, R; Gouda, N; Hirabayashi, M; Isobe, N; Kamizuka, T; Kashima, S; Kawahara, H; Kawata, D; Kohara, N; Kondo, I; Mase, I; Miyakawa, K; Ohsawa, R; Ozaki, M; Shimizu, R; Suematsu, Y; Tada, S; Tsuzuki, T; Uraguchi, F; Usui, F; Utsunomiya, S; Wada, T; Yamada, Y; Yano, T; - view fewer <#> (2024) Conceptual design of the satellite payload for the JASMINE mission. In: Coyle, Laura E and Perrin, Marshall D and Matsuura, Shuji, (eds.) Proceedings of SPIE - The International Society for Optical Engineering. (pp. pp. 1-9). Society of Photo-Optical Instrumentation Engineers (SPIE) Green open access document_url: https://discovery.ucl.ac.uk/id/eprint/10198831/1/130920A.pdf