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