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":"地球空间x射线成像仪","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":"{\"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}","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
摘要
GEO-X(地球空间x射线成像仪)是一个小型卫星任务,旨在通过x射线可视化地球磁层并揭示太阳风和磁层之间的动力学耦合。原位航天器揭示了磁层中的各种现象。近年来,x射线天文卫星观测发现软x射线发射起源于磁层。因此,我们将大视场x射线仪器的创新技术与深空探测微卫星技术相结合,开发GEO-X。GEO-X是一颗50公斤级微型卫星,携带新型紧凑x射线成像光谱仪有效载荷。具有较大δ v (<700 m/s)的微型卫星从相对较低的高度(例如,地球转移轨道)在40-60 RE时增加高度是必要的。因此,我们将18U立方体卫星与液体N2O和聚乙烯组成的混合踢腿电机结合起来。我们还开发了宽视场(5×5度)和良好的空间分辨率(10角分)x射线(0.3-2 keV)成像仪。我们利用一个微机械x射线望远镜,和一个CMOS探测器系统与光学阻塞滤波器。我们的目标是在第25次太阳活动极大期前后发射卫星。
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.