| Autor: |
Zhang, XiaoFeng, Chen, Wen, Zhu, XiaoCheng, Meng, Na, He, JunWang, Bi, XingZi, Zhang, YongHe, Shi, Qi, Li, Fei, Liu, Rui, Feng, ZhengGong, Liu, Liu, Li, JinSong, Wu, HaiChen, Xu, DongXiao, Li, TaiJie, Huang, JiangJiang, Liu, Shuo, Li, TianTong, Yu, XianSheng, Gao, Yang, Zhou, Heng, Ban, HanYu, Zhang, YanLi, Zhang, YueTing, Yang, YingQuan, He, Tao, Duan, XuLiang, Chen, Xin, Wang, YaMin, Sun, AnTai, Zhang, KuoXiang, Sun, Ying, Wang, YaoBin, Fan, ChengCheng, Xiong, ShaoLin, Li, XinQiao, Wen, XiangYang, Ling, ZhiXing, Sun, XiaoJin, Zhang, Chen, Bai, XianYong, Wang, ZhanShan, Deng, YuanYong, Tian, Hui, Yang, JianFeng, Xue, HongBo, Sang, Peng, Liu, JinGuo, Zheng, HuiLong, Zhu, Xiang, He, JianWu, Li, Hui, Xu, LuXiang, Xu, ShuYan, Chen, WenWu, Liu, ZhenDong, Wang, ZhaoLi, Mao, XiangLong, Gao, Rong, Li, ZongXuan, Ding, GuoPeng, Wang, XinYu, Dou, RunJiang, Weng, LuBin, Luo, Hao, Wang, YaPing, Liang, XianFeng, Fang, ZiRuo |
| Zdroj: |
SCIENCE CHINA Technological Sciences; 20240101, Issue: Preprints p1-19, 19p |
| Abstrakt: |
The Space Advanced Technology demonstration satellite (SATech-01), a mission for low-cost space science and new technology experiments, organized by Chinese Academy of Sciences (CAS), was successfully launched into a Sun-synchronous orbit at an altitude of ∼500 km on July 27, 2022, from the Jiuquan Satellite Launch Centre. Serving as an experimental platform for space science exploration and the demonstration of advanced common technologies in orbit, SATech-01 is equipped with 16 experimental payloads, including the solar upper transition region imager (SUTRI), the lobster eye imager for astronomy (LEIA), the high energy burst searcher (HEBS), and a High Precision Magnetic Field Measurement System based on a CPT Magnetometer (CPT). It also incorporates an imager with freeform optics, an integrated thermal imaging sensor, and a multi-functional integrated imager, etc. This paper provides an overview of SATech-01, including a technical description of the satellite and its scientific payloads, along with their on-orbit performance. |
| Databáze: |
Supplemental Index |
| Externí odkaz: |
|
Full text from SpringerLink