A new thermoluminescent dosimeter system for space research
A small, portable, vibration and shock resistant thermoluminescent dosimeter system was developed to measure cosmic radiation dose on board a spacecraft. The system consists of a small battery-operated reader and a special bulb dosimeter. Doses from 10 μGy up to 100 mGy can be measured. The electric...
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| Veröffentlicht in: | Advances in space research 1981, Vol.1 (14), p.61-66 |
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| container_title | Advances in space research |
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| creator | Fehér, I. Deme, S. Szabó, B. Vágvölgyi, J. Szabó, P.P. Csőke, A. Ránky, M. Akatov, Yu.A. |
| description | A small, portable, vibration and shock resistant thermoluminescent dosimeter system was developed to measure cosmic radiation dose on board a spacecraft. The system consists of a small battery-operated reader and a special bulb dosimeter. Doses from 10 μGy up to 100 mGy can be measured. The electrical power consumption of the reader is about 5 W, its volume is about 1 dm
3 and its mass is about 1 kg. Details are given for the construction and technical parameters of the dosimeter and reader. |
| doi_str_mv | 10.1016/0273-1177(81)90244-1 |
| format | Article |
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3 and its mass is about 1 kg. Details are given for the construction and technical parameters of the dosimeter and reader.</description><subject>Calcium Sulfate</subject><subject>Cosmic Radiation</subject><subject>Equipment Design</subject><subject>Space Flight - instrumentation</subject><subject>Spacecraft - instrumentation</subject><subject>Thermoluminescent Dosimetry - instrumentation</subject><subject>Thulium</subject><issn>0273-1177</issn><issn>1879-1948</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1981</creationdate><recordtype>article</recordtype><sourceid>EIF</sourceid><recordid>eNp9kE1LxDAQhoMouq7-A5GeRA_VmTZtUgRhWfyCBS96Dmk6YSP9WJOusv_e1l305mnm8Lzz8TB2hnCNgPkNJCKNEYW4lHhVQMJ5jHtsglIUMRZc7rPJL3LEjkN4B8BECDhkR4gZR5HAhN3Oopa-on5JvunqdeNaCobaPqq64BrqyUdhE3pqItsN7UobijwF0t4sT9iB1XWg012dsreH-9f5U7x4eXyezxaxSYH3seaGp1UBHHkFJRW2FGVRgQWbmTwHaWQOWOZoEmkKk9jSlppryAVPNRRZlk7ZxXbuyncfawq9atxwZF3rlrp1UEkqhMQMB5BvQeO7EDxZtfKu0X6jENQoTY1G1GhESVQ_0tQYO9_NX5cNVX-hnaUBuNsCNHz56cirYBy1hirnyfSq6tz_G74BMTZ7EA</recordid><startdate>1981</startdate><enddate>1981</enddate><creator>Fehér, I.</creator><creator>Deme, S.</creator><creator>Szabó, B.</creator><creator>Vágvölgyi, J.</creator><creator>Szabó, P.P.</creator><creator>Csőke, A.</creator><creator>Ránky, M.</creator><creator>Akatov, Yu.A.</creator><general>Elsevier Ltd</general><scope>CGR</scope><scope>CUY</scope><scope>CVF</scope><scope>ECM</scope><scope>EIF</scope><scope>NPM</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>1981</creationdate><title>A new thermoluminescent dosimeter system for space research</title><author>Fehér, I. ; Deme, S. ; Szabó, B. ; Vágvölgyi, J. ; Szabó, P.P. ; Csőke, A. ; Ránky, M. ; Akatov, Yu.A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c304t-a4c43d90414d0be9fb7b9d0f0f5c6608c8601b61c28c9c2fbfba4a06743a09553</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1981</creationdate><topic>Calcium Sulfate</topic><topic>Cosmic Radiation</topic><topic>Equipment Design</topic><topic>Space Flight - instrumentation</topic><topic>Spacecraft - instrumentation</topic><topic>Thermoluminescent Dosimetry - instrumentation</topic><topic>Thulium</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Fehér, I.</creatorcontrib><creatorcontrib>Deme, S.</creatorcontrib><creatorcontrib>Szabó, B.</creatorcontrib><creatorcontrib>Vágvölgyi, J.</creatorcontrib><creatorcontrib>Szabó, P.P.</creatorcontrib><creatorcontrib>Csőke, A.</creatorcontrib><creatorcontrib>Ránky, M.</creatorcontrib><creatorcontrib>Akatov, Yu.A.</creatorcontrib><collection>Medline</collection><collection>MEDLINE</collection><collection>MEDLINE (Ovid)</collection><collection>MEDLINE</collection><collection>MEDLINE</collection><collection>PubMed</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Advances in space research</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Fehér, I.</au><au>Deme, S.</au><au>Szabó, B.</au><au>Vágvölgyi, J.</au><au>Szabó, P.P.</au><au>Csőke, A.</au><au>Ránky, M.</au><au>Akatov, Yu.A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A new thermoluminescent dosimeter system for space research</atitle><jtitle>Advances in space research</jtitle><addtitle>Adv Space Res</addtitle><date>1981</date><risdate>1981</risdate><volume>1</volume><issue>14</issue><spage>61</spage><epage>66</epage><pages>61-66</pages><issn>0273-1177</issn><eissn>1879-1948</eissn><abstract>A small, portable, vibration and shock resistant thermoluminescent dosimeter system was developed to measure cosmic radiation dose on board a spacecraft. The system consists of a small battery-operated reader and a special bulb dosimeter. Doses from 10 μGy up to 100 mGy can be measured. The electrical power consumption of the reader is about 5 W, its volume is about 1 dm
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| fulltext | fulltext |
| identifier | ISSN: 0273-1177 |
| ispartof | Advances in space research, 1981, Vol.1 (14), p.61-66 |
| issn | 0273-1177 1879-1948 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_23778151 |
| source | MEDLINE; Elsevier ScienceDirect Journals Complete |
| subjects | Calcium Sulfate Cosmic Radiation Equipment Design Space Flight - instrumentation Spacecraft - instrumentation Thermoluminescent Dosimetry - instrumentation Thulium |
| title | A new thermoluminescent dosimeter system for space research |
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