DocumentCode :
2067845
Title :
Performance characteristics of the CMOS SSPM tissue-equivalent space dosimeter
Author :
Johnson, Erik B. ; Chapman, Eric ; Chen, Xiao Jie ; Mukhopadhyay, Sharmistha ; Stapels, Christopher J. ; Christian, James F. ; Benton, Eric
Author_Institution :
Radiat. Monitoring Devices, Watertown, MA, USA
fYear :
2010
fDate :
6-13 March 2010
Firstpage :
1
Lastpage :
8
Abstract :
The complexity of space-flight design requires reliable, fault-tolerant equipment capable of providing real-time dosimetry during a mission, which is not feasible with the existing thermoluminescent dosimeter (TLD) technology, especially during extravehicular activity (EVA). Real-time monitoring is important for low-Earth orbiting spacecraft and interplanetary space flight to alert the crew when Solar Particle Events (SPE) increase the particle flux of the spacecraft environment. A tissue-equivalent, chip-based, personal dosimeter represents an attractive approach to meet the demanding requirements for manned space missions. A dosimeter-on-a-chip for personal dosimetry is comprised of a tissue-equivalent scintillator coupled to a solid-state photomultiplier (SSPM) built using CMOS technology. The radiation sensitive component of the dosimeter is coupled to analog signal processing components and a microprocessor, which can successfully process up to 5 × 105 events per second. The dynamic range of the dosimeter has been verified with 1-GeV protons (0.22 keV/¿m in H20) to 300 MeV/n Fe (238 keV/¿m in H20). The dosimeter reconstructed does over 6 to 36 ¿Sv from 1-GeV protons to within 3%. We present dose equivalent performance of the device, along with power consumption parameters, expected space flight performance, and design upgrades.
Keywords :
CMOS integrated circuits; dosimeters; fault tolerance; photomultipliers; space research; space vehicles; CMOS SSPM tissue-equivalent space dosimeter; CMOS technology; analog signal processing components; chip-based personal dosimeter; dosimeter-on-a-chip; electron volt energy 1 GeV; electron volt energy 300 MeV; extravehicular activity; fault-tolerant equipment; interplanetary space flight; low-Earth orbiting spacecraft; manned space missions; microprocessor; particle flux; personal dosimetry; radiation sensitive component; real-time dosimetry; real-time monitoring; solar particle events; solid-state photomultiplier; space-flight design; spacecraft environment; thermoluminescent dosimeter technology; tissue-equivalent scintillator; CMOS technology; Dosimetry; Fault tolerance; Monitoring; Photomultipliers; Protons; Solid state circuits; Space missions; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2010.5447005
Filename :
5447005
Link To Document :
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