Dose measurements in space by the Hungarian Pille TLD system

被引:17
作者
Apáthy, I
Deme, S
Fehér, I
Akatov, YA
Reitz, G
Arkhanguelski, VV
机构
[1] KFKI, Atom Energy Res Inst, H-1525 Budapest, Hungary
[2] State Sci Ctr, Inst Biomed Problems, Moscow 123007 A, Russia
[3] DLR, Inst Aerosp Med, D-51147 Cologne, Germany
关键词
Cosmic rays - Earth (planet) - Energy utilization - Problem solving;
D O I
10.1016/S1350-4487(02)00071-9
中图分类号
TL [原子能技术]; O571 [原子核物理学];
学科分类号
0827 ; 082701 ;
摘要
Exposure of crew, equipment, and experiments to the ambient space radiation environment in low Earth orbit poses one of the most significant problems to long-term space habitation. Accurate dose measurement has become increasingly important during the assembly (extravehicular activity (EVA)) and operation of space stations such as on Space Station Mir. Passive integrating detector systems such as thermoluminescent dosemeters (TLDs) are commonly used for dosimetry mapping and personal dosimetry on space vehicles. The well-known advantages of passive detector systems are their independence of power supply, small dimensions, high sensitivity, good stability, wide measuring range, resistance to environmental effects, and relatively low cost. Nevertheless, they have the general disadvantage that for evaluation purposes they need a laboratory or large-in mass and power consumption-terrestrial equipment, and consequently they cannot provide time-resolved dose data during long-term space flights. KFKI Atomic Energy Research Institute (KFKI AEKI) has developed and manufactured a series of thermoluminescent dosemeter systems for measuring cosmic radiation doses in the 10 muGy to 10 Gy range, consisting of a set of bulb dosemeters and a compact, self-contained, TLD reader suitable for on-board evaluation of the dosemeters. By means of such a system, highly accurate measurements were carried out on board the Salyut-6, -7 and Mir Space Stations as well as on the Space Shuttle. A detailed description of the system is given and the comprehensive results of these measurements are summarised. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:381 / 391
页数:11
相关论文
共 11 条
[1]  
Akatov YuA, 1984, Adv Space Res, V4, P77, DOI 10.1016/0273-1177(84)90227-8
[2]  
Apathy I, 1996, RADIAT PROT DOSIM, V66, P441, DOI 10.1093/oxfordjournals.rpd.a031772
[3]   Active dosimetry on recent space flights [J].
Beaujean, R ;
Kopp, J ;
Reitz, G .
RADIATION PROTECTION DOSIMETRY, 1999, 85 (1-4) :223-226
[4]  
BENTON ER, 2002, RAD MEAS
[5]   Doses due to the South Atlantic Anomaly during the Euromir'95 mission measured by an on-board TLD system [J].
Deme, S ;
Reitz, G ;
Apáthy, I ;
Héjja, I ;
Láng, E ;
Fehér, I .
RADIATION PROTECTION DOSIMETRY, 1999, 85 (1-4) :301-304
[6]   Extra dose due to extravehicular activity during the NASA4 mission measured by an on-board TLD system [J].
Deme, S ;
Apáthy, I ;
Héjja, I ;
Láng, E ;
Fehér, I .
RADIATION PROTECTION DOSIMETRY, 1999, 85 (1-4) :121-124
[7]  
Feher I, 1981, Adv Space Res, V1, P61, DOI 10.1016/0273-1177(81)90244-1
[8]  
FEHER I, 1983, NEW ADV TLD SYSTEM S
[9]  
FEHER I, 1985, UNPUB REAL TIME THER
[10]  
REITZ G, 1996, ESA, P183