Calibration and simulation of a silicon dosemeter for ambient dose equivalent in low-earth orbit space

被引:1
|
作者
Youn, Sukwon [1 ,2 ]
Nam, Uk-won [3 ]
Kim, Sunghwan [4 ]
Kim, Hongjoo [5 ]
Park, Won-Kee [3 ]
Sohn, Jongdae [3 ]
Moon, Bongkon [3 ]
Jun, Insoo [6 ]
Ye, Sung-Joon [1 ,2 ,7 ,8 ]
机构
[1] Seoul Natl Univ, Dept Appl Bioengn, Seoul 08826, South Korea
[2] Seoul Natl Univ, Rese Inst Convergence Sci, Grad Sch Convergence Sci & Technol, Seoul 08826, South Korea
[3] Korea Astron & Space Sci Inst, Space Sci Div, Daejeon 34055, South Korea
[4] Cheongju Univ, Dept Radiol Sci, Cheongju 28503, South Korea
[5] Kyungpook Natl Univ, Dept Phys, Daegu 41566, South Korea
[6] CALTECH, Jet Propuls Lab, Pasadena, CA 91109 USA
[7] Seoul Natl Univ, Adv Inst Convergence Technol, Suwon 16229, South Korea
[8] Seoul Natl Univ Hosp, Biomed Res Inst, Seoul 03080, South Korea
基金
新加坡国家研究基金会;
关键词
COSMIC-RADIATION; ENERGY; FACILITY; LIULIN; FIELD; ISS;
D O I
10.1093/rpd/ncad226
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
A particle dosemeter (PD) is a payload of NEXTSat-2 in the low-earth orbit (LEO). The absorbed dose in LEO needs to be converted into the ambient dose equivalent (H*(10)). Due to a mixed field in LEO, the calibration factors (k(low) and k(high)) should be determined for the low-and high-linear energy transfers (LET) (below and above 1.5 keV/mu m), respectively. The PD was irradiated with a Cs-137 source at the Korea Radiation Solution facility to obtain H*(10) and absorbed doses. However due to the lack of sources for the high-LET calibration, H*(10) and an absorbed dose were calculated by simulating PD for the high-energy neutron field at CERN-EU high-energy Reference Field. The measured k(low) of PD had a difference of 5.1% and 9.5% from the calculated value of PD and the measured value of Liulin detectors, respectively. However, a difference in k(high) between PD and Liulin was explained by the contribution of non-neutron components to Liulin in the measurements.
引用
收藏
页码:2118 / 2125
页数:8
相关论文
共 50 条
  • [11] Monte Carlo simulation for aerodynamic coefficients of satellites in Low-Earth Orbit
    Jin, Xuhong
    Huang, Fei
    Cheng, Xiaoli
    Wang, Qiang
    Wang, Bing
    ACTA ASTRONAUTICA, 2019, 160 : 222 - 229
  • [12] Efficiency of a radiophotoluminescence glass dosemeter for low-earth-orbit space radiation
    Yasuda, H
    Fujitaka, K
    SOLID STATE DOSIMETRY, PTS 1 AND 2, PROCEEDINGS, 2002, : 545 - 548
  • [13] Solar cycle variation of outer belt electron dose at low-earth orbit
    Brautigam, DH
    Dichter, BK
    Ray, KR
    Turnbull, WR
    Madden, D
    Ling, A
    Holeman, E
    Redus, RH
    Woolf, S
    IEEE TRANSACTIONS ON NUCLEAR SCIENCE, 2001, 48 (06) : 2010 - 2015
  • [14] Using VR to improve the performance of low-earth orbit space robot operations
    Lapointe, JF
    Massicotte, P
    CYBERPSYCHOLOGY & BEHAVIOR, 2003, 6 (05): : 545 - 548
  • [15] Orbital dynamics of laser-propelled space vehicles in low-earth orbit
    Yamakawa, Hiroshi
    Funaki, Ikkoh
    SPACE FLIGHT MECHANICS 2007, VOL 127, PTS 1 AND 2, 2007, 127 : 607 - +
  • [16] Orbital dynamics of low-earth orbit laser-propelled space vehicles
    Yamakawa, Hiroshi
    Funaki, Ikkoh
    Komurasaki, Kimiya
    BEAMED ENERGY PROPULSION, 2008, 997 : 316 - +
  • [17] FLOTILLAS TO SET SAIL FOR LOW-EARTH ORBIT
    LERMAN, L
    AEROSPACE AMERICA, 1984, 22 (10) : 74 - 76
  • [18] Accelerating architecture for low-Earth orbit and beyond
    Hall, Theodore W.
    AEROSPACE AMERICA, 2022, 60 (11) : 68 - 68
  • [20] Models and numerical simulation of velocity distribution of pickup ions at low-Earth orbit
    Zhang, YH
    Raitt, WJ
    Thompson, DC
    JOURNAL OF GEOPHYSICAL RESEARCH-SPACE PHYSICS, 2001, 106 (A12) : 29843 - 29858