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A microdosimeter is perhaps the only active detector capable of directly determining the mean radiation quality of a mixed or unknown radiation field. Therefore, the dose equivalent and effective dose can be developed, from which the radiation risk can be assessed in real time. Objectives of this research project were to develop a rugged, portable, low-power, low-mass, solid-state microdosimeter suitable for an area sensor, a spacecraft, habitat or as a personnel monitor, such as a spacesuit. Objectives also included verification of its performance through radiation source and beam tests and comparison of experimental results with radiation transport codes. The original objectives were expanded to include a student-developed instrument for the MidSTAR-I spacecraft launched in March 2007. . Original Aims
The specific objectives of the MIcroDosimeter iNstrument (MIDN) instrument are to:
While not part of this proposal, a student design effort developed an early version of a MIDN instrument that was launched on the MidSTAR-I spacecraft in 2007 with only a short time available for its design and development by the students. We have satisfied, most but not all, of our aims and instrument development objectives. We successfully evolved two sets of instrumentation: a bench-top system to evaluate instrument components without regard for power or size and two prototype flight instruments. Each instrument consists essentially of a sensor, sensor electronics, amplifiers, analog-to-digital conversion and a multichannel analyzer under computer or microprocessor control. We tested these instruments at the NASA Space Radiation Laboratory (NSRL) at Brookhaven National Laboratory (BNL). Ions examined include iron, oxygen, silicon, hydrogen, carbon and titanium. In our benchtop system with a 10 um thick sensor, we were able to achieve a dE/dx < 1keV/um in silicon that is equivalent to a lineal energy of approximately 0.4 keV/um in tissue. In our flight prototype instrument with a 10 um thick sensor, we were able to achieve a dE/dx ~ 3 keV/um in silicon that is equivalent to a lineal energy of ~ 1 keV/um in tissue. The anticipated flight system will require a power of approximately one watt, could be packaged into a volume of less than 1284 cm, and should have a dE/dx < 1keV/um in silicon that is equivalent to a lineal energy of approximately 0.4 keV/um in tissue. These are significant accomplishments that satisfy the primary objectives of the research and verify our original hypotheses that silicon microdosimetery appears to be a viable alternative to assess a mixed and unknown time-varying radiation field to estimate regulatory risk. This is the final year of this NSBRI grant.
Earth-based Applications of Research Project The use of prior methods is limited in part because of the complexity, sensitivity and lack of reliability of the most commonly used instruments, gas proportional counters. The compact system that we have developed for space applications would likewise be applicable for these situations and measurements described in the previous paragraph. We have established for the first time in a solid-state microdosimeter a lowered energy cutoff of dE/dx < 1 keV/um in silicon that is equivalent to a lineal energy cutoff of < 0.4 keV/um in tissue. Thus we have an instrument that can be used in space and terrestrially to directly assess regulatory risk.
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