Y. Ezoe, R. Funase, H. Nagata, Y. Miyoshi, H. Nakajima, I. Mitsuishi, K. Ishikawa, Yosuke Kawabata, Shintaro Nakajima, Landon Kamps, M. Numazawa, T. Yoneyama, K. Hagino, Y. Matsumoto, K. Hosokawa, S. Kasahara, J. Hiraga, K. Mitsuda, M. Fujimoto, M. Ueno, A. Yamazaki, H. Hasegawa, T. Mitani, Y. Kawakatsu, T. Iwata, H. Koizumi, H. Sahara, Y. Kanamori, K. Morishita
{"title":"GEO-X (GEOspace X-ray imager)","authors":"Y. Ezoe, R. Funase, H. Nagata, Y. Miyoshi, H. Nakajima, I. Mitsuishi, K. Ishikawa, Yosuke Kawabata, Shintaro Nakajima, Landon Kamps, M. Numazawa, T. Yoneyama, K. Hagino, Y. Matsumoto, K. Hosokawa, S. Kasahara, J. Hiraga, K. Mitsuda, M. Fujimoto, M. Ueno, A. Yamazaki, H. Hasegawa, T. Mitani, Y. Kawakatsu, T. Iwata, H. Koizumi, H. Sahara, Y. Kanamori, K. Morishita","doi":"10.1117/12.2629107","DOIUrl":null,"url":null,"abstract":"GEO-X (GEOspace X-ray imager) is a small satellite mission aiming at visualization of the Earth’s magnetosphere by X-rays and revealing dynamical couplings between solar wind and magnetosphere. In-situ spacecraft have revealed various phenomena in the magnetosphere. In recent years, X-ray astronomy satellite observations discovered soft X-ray emission originated from the magnetosphere. We therefore develop GEO-X by integrating innovative technologies of the wide FOV X-ray instrument and the microsatellite technology for deep space exploration. GEO-X is a 50 kg class microsatellite carrying a novel compact X-ray imaging spectrometer payload. The microsatellite having a large delta v (<700 m/s) to increase an altitude at 40-60 RE from relatively lowaltitude (e.g., Geo Transfer Orbit) piggyback launch is necessary. We thus combine a 18U Cubesat with the hybrid kick motor composed of liquid N2O and polyethylene. We also develop a wide FOV (5×5 deg) and a good spatial resolution (10 arcmin) X-ray (0.3-2 keV) imager. We utilize a micromachined X-ray telescope, and a CMOS detector system with an optical blocking filter. We aim to launch the satellite around the 25th solar maximum.","PeriodicalId":137463,"journal":{"name":"Astronomical Telescopes + Instrumentation","volume":"13 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-08-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Astronomical Telescopes + Instrumentation","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1117/12.2629107","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
GEO-X (GEOspace X-ray imager) is a small satellite mission aiming at visualization of the Earth’s magnetosphere by X-rays and revealing dynamical couplings between solar wind and magnetosphere. In-situ spacecraft have revealed various phenomena in the magnetosphere. In recent years, X-ray astronomy satellite observations discovered soft X-ray emission originated from the magnetosphere. We therefore develop GEO-X by integrating innovative technologies of the wide FOV X-ray instrument and the microsatellite technology for deep space exploration. GEO-X is a 50 kg class microsatellite carrying a novel compact X-ray imaging spectrometer payload. The microsatellite having a large delta v (<700 m/s) to increase an altitude at 40-60 RE from relatively lowaltitude (e.g., Geo Transfer Orbit) piggyback launch is necessary. We thus combine a 18U Cubesat with the hybrid kick motor composed of liquid N2O and polyethylene. We also develop a wide FOV (5×5 deg) and a good spatial resolution (10 arcmin) X-ray (0.3-2 keV) imager. We utilize a micromachined X-ray telescope, and a CMOS detector system with an optical blocking filter. We aim to launch the satellite around the 25th solar maximum.