DESIGN AND FABRICATION OF LABORATORY PILOT FOR OSL DOSIMETER SYSTEM FOR SPACE APPLICATIONS

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

AGHAEI A.; SADEGHI H.; JAHANBAKHSH H.; TAHERI R.; MOUSAVI A.; NIKO A.M.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2013 | Volume:6 | Issue:3 (16) Page(s): 67-73

Download Full-Text

Persian Verion

View:

651

Download:

Cites:

Information Journal Paper

Title

DESIGN AND FABRICATION OF LABORATORY PILOT FOR OSL DOSIMETER SYSTEM FOR SPACE APPLICATIONS

Author(s)

Keywords

OSL DOSIMETRY SYSTEMQ2

LUMINESCENCEQ2

CALIBRATIONQ2

OSL MATERIALQ2

THERMO LUMINESCENCEQ2

Abstract

OSL dosimeter system was introduced first time in 1963 and it has been used for space application science 2005 by space organizations. In this work we try to design and fabricate this system in Iran for the first time .Basic physical quantum of this system is optically stimulated LUMINESCENCE. This system consist of OSL MATERIAL, Optical section for Stimulation and reader section. In this work, first the basic theory of OSL phenomena has been reviewed, then the space applications and the advantage of this system has been compared with other dosimeter system. Afterward laboratory construction of this system and some characterizations of that such as primary CALIBRATION by Co-60 source, has been introduced. Finally, results of evaluation of this system shows that, this fabricated system has linear response function in rang of 1-10 Gy.

Cites

No record.

References

No record.

Cite

APA: Copy

AGHAEI, A., SADEGHI, H., JAHANBAKHSH, H., TAHERI, R., MOUSAVI, A., & NIKO, A.M.. (2013). DESIGN AND FABRICATION OF LABORATORY PILOT FOR OSL DOSIMETER SYSTEM FOR SPACE APPLICATIONS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 6(3 (16)), 67-73. SID. https://sid.ir/paper/150020/en

Vancouver: Copy

AGHAEI A., SADEGHI H., JAHANBAKHSH H., TAHERI R., MOUSAVI A., NIKO A.M.. DESIGN AND FABRICATION OF LABORATORY PILOT FOR OSL DOSIMETER SYSTEM FOR SPACE APPLICATIONS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2013;6(3 (16)):67-73. Available from: https://sid.ir/paper/150020/en

IEEE: Copy

A. AGHAEI, H. SADEGHI, H. JAHANBAKHSH, R. TAHERI, A. MOUSAVI, and A.M. NIKO, “DESIGN AND FABRICATION OF LABORATORY PILOT FOR OSL DOSIMETER SYSTEM FOR SPACE APPLICATIONS,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 6, no. 3 (16), pp. 67–73, 2013, [Online]. Available: https://sid.ir/paper/150020/en

Related Journal Papers