A study of the mechanism of proton irradiation effects in the in-orbit operation of the backside illuminated CMOS image sensor (BSI CIS) used for imaging by the Fine Guidance Sensor (FGS) is presented in this paper. According to the proton irradiation environment of the Halo L2 orbit where FGS is located and the duration of in orbit operation, proton irradiation experiments were conducted on the BSI CIS, the core imaging device of FGS. Results show that proton irradiation is expected to cause a significant increase in the dark current of the BSI CIS of the FGS after four years of its in orbit, with the peak of the dark signal distribution shift to the right and an exponential trailing of the tail of the dark signal distribution when the proton fluence reached 6.71 × 1010p/cm2. This is the result of a combination of ionization defects and displacement damage defects. In addition, we also report about the device gain, which is of particular interest in space astronomical exploration. We performed a more detailed single pixel gain test of the device gain and found that the degradation of the gain appears to be correlated with the intensity of the ionization defects. The results of this study can provide theoretical basis for the radiation hardening by design of FGS to some extent.
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