In recent years, the method used to collect planetary samples has entailed launching a projectile from a spacecraft onto the surface of a planet at touchdown and collecting the sample raised by the impact. However, there is concern that the dust that is raised at touchdown would adhere to the radiator and affect radiative emissions from the radiator into deep space and radiative reflectance against irradiance from the sun and planets into the radiator. In other words, the dust could affect the thermal control of the spacecraft. Using electromagnetic field analysis, a new evaluation parameter was introduced in this study, and the effect of dust particles on the radiation heat transfer of a SiO2 substrate surface, which is commonly used in spacecraft radiators, was calculated. The electromagnetic field analysis was validated experimentally by spectroscopy. The effects of dust particle size, adhesion, and material on the changes in radiative properties were quantified and analyzed. It was suggested that dust particles could change the radiative properties of the radiator and adversely affect thermal control. This effect increased with increasing particle adhesion.