In-situ gamma spectrometer with mobile equipment can be used for rapid determination of radioactivity in the environment within a very short interval. 2”×2” NaI(Tl) scintillator are used to build a mobile radiation measurement system (called as Monitoring of Ambient Radiations of KAERI for Backpack, MARK-B3) with a signal processing unit, and GPS and interface units to a PC for wireless controlling system. Development of the survey system is to measure ambient gamma-ray spectrometry for estimating ground radioactivity and radiation dose in the environment. The ambient dose rate is estimated using G-factor method. For determination of G-factor, we conducted MCNP simulations in assumptions of various incident photons into the detector system. And the scintillator was exposed to Cs-137 source in the range of 1- 300 mGy/hr. Calculated dose rates for different simulation results were compared to the irradiated dose rate to derive correction factor of G-factor. To evaluate performance of the MARK-B3, in-situ gamma spectrometry was conducted in Jeju island.

This study was performed to assess the cosmic-ray effect caused by altitude in the aerial gammaray measurement. For the gamma-ray measurement experiment by altitude, the aerial survey system composed of four 4×4×16 inches large volume NaI (Tl) detectors was used. The aerial survey system was installed in a rotor-craft to stably keep its flight altitude and position. In addition, in order to avoid to time-dependent shielding effects with the amount of fuel, a rotor-craft of which the fuel tank is not located beneath the cabin floor was selected. In this study, the ROI (Region Of Interest) was set to the 3~6 MeV range to assess the cosmic-ray contribution to the gamma-ray spectrum that could ignore the contribution of the dominant natural radionuclides. The gamma-ray spectra measured inside and outside of the rotor-craft on the ground were compared to evaluate the shielding effects of the aircraft body. As a result, the count rate of the 40K photo peak was decreased by about 10% when measuring the inside compared to the outside. On the other hand, the total count rate of the 3~6 MeV region was decreased by about 0.7% under the same condition. Therefore, the aircraft body effect was insignificant in 3~6 MeV region considering the relative uncertainty of 0.04~0.78% (1σ). In addition, the count rate in the 3~6 MeV range according to altitude was evaluated to assess the cosmic-ray effect. In order to evaluate the change in the ROI count rate according to the altitude, the gamma-ray spectrum was measured in the range of 300~2,000 m above the sea to avoid the effect of terrestrial radiation. As a result, the relationship between altitude and count rate in the 3~6 MeV range showed a high correlation with the R2 value of 0.99, when the approximate equation was derived in the form of a quadratic polynomial. Also, the count rate of 3~6 MeV at 50~500 m above the ground was estimated using the correlation equation, and this value was compared with the measured count rate. As a result of comparing the average value of estimated count rate and measured count rate, the relative difference is less than 2%. Considering the relative uncertainty of 0.78~4.11% (1σ), it was possible to evaluate the count rate of the 3~6 MeV region relatively accurately. The results of this study could be used for further study on background dose corrections in aerial survey.

일반적으로 방사선 선원의 강도는 거리의 역자승 법칙을 따른다. 그러나 방사선 선원과 검출기와의 거리가 가까울수록 거리의 역자승 법칙 실험은 이론과 실험의 일치하지 못하는 오류를 가져오게 된다. 본 연구에서는 방사선 선원과검출기와의 거리에 따른 거리의 역자승 법칙이 실제 실험에서는 정확하게 성립하지 않는 이유를 실험적으로 확인하였다. 그리고 이 문제를 해결하기 위하여 측정된 방사능을 보정하기 위하여 보정계수를 실험적으로 얻었다. 측정에 사용한 검출기는 2˝×2˝ø NaI(Tl) 신틸레이션 검출기를 사용하였고, 방사선에너지의 변화에 따른 효과를 확인하기 위하여감마선 선원 60Co(1.174 MeV, 1.333 MeV)와 137Cs(0.662 MeV)에 대한 실험도 병행하였다. 측정에서 얻어진 거리의역자승 법칙의 결과들을 보정계수를 이용하여 측정값들을 보정한 결과 거리의 역자승 법칙과 매우 일치하는 경향을 보였고, 오류에 대한 원인을 실험적으로 확인하였다. 이러한 결과는 유한한 체적을 가진 검출기를 사용하여 방사선의 강도가 거리의 역자승에 반비례하는 실험을 할 경우 모두 해당되는 문제이므로 본 연구의 결과는 방사선계측 분야에 매우 유용하게 사용되어질 것으로 사료된다.