航天器
线性能量转移
轨道(动力学)
物理
火箭(武器)
辐射
质子
粒子辐射
航程(航空)
艾伦皮带车辐射
比例计数器
谱线
宇宙射线对健康的威胁
粒子(生态学)
等效剂量
粒子探测器
空间环境
校准
航空航天工程
带电粒子
核物理学
探测器
光学
天文
工程类
磁层
离子
日冕物质抛射
量子力学
地质学
等离子体
海洋学
太阳风
作者
Guohong Shen,Zheng Chang,Huanxin Zhang,Chunqin Wang,Ying Sun,Zida Quan,Xianguo Zhang,Yueqiang Sun
出处
期刊:Atmosphere
[Multidisciplinary Digital Publishing Institute]
日期:2024-06-12
卷期号:15 (6): 705-705
被引量:2
标识
DOI:10.3390/atmos15060705
摘要
Based on the characteristics of space particle radiation in the Sun-synchronous orbit (SSO), a space particle radiation effect comprehensive measuring instrument (SPRECMI) was installed on the orbital platform of the upper stage of the Chinese CZ-4C carrier rocket, which can acquire the high-energy proton energy spectra, linear energy transfer (LET) spectra of particles, and radiation dose rate. The particle radiation detection data were obtained at 1000 km altitude for the first time, which can be used mainly for scientific research of the space environment, in-orbit fault analysis, and the operational control management of spacecraft, and can also serve as reference data for component validation tests. After SPRECMI’s development, accelerator calibration and simulations were conducted, and the results demonstrated that all the measured indicators, including the high-energy proton spectra (energy range: 21.8–275.0 MeV, precision: <3.3%), total radiation dose (dose range: 0–1.04 × 106 rad, sensitivity: 6.2 µrad/h), and the LET spectra (range: 0.001–37.20 MeV/(mg/cm2), >37.2 MeV/(mg/cm2)), met the relevant requirements. Furthermore, the in-orbit flight test revealed that the detection results of the load components were consistent with the physical characteristics of the particle radiation environment of the spacecraft’s orbit.
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