Optical cooling is a novel research area for space applications, where materials are cooled through light interactions. This cooling is used to lower the temperature of a payload attached to a cooling element. To maximize cooling power, a thermal link is placed between the payload and cooling material, designed to conduct maximum heat while minimizing fluorescence transmission. This study investigates the performance of a tapered thermal link based on geometrical, operational, and material parameters, aiming to establish simplified mathematical correlations for optimizing the design. A validated numerical model was developed for analysis. Results show that the length and surrounding shell temperature significantly influence the thermal link’s performance, more so than the cross-sectional area, emissivity, and refractive index. Optical transmission decreased from 0.085% to 0.065% as length increased from 0.5 cm to 2.0 cm, stabilizing at 0.06%. Heat conduction dropped from 0.139 W to 0.132 W for lengths from 0.5 cm to 3.0 cm, while radiation load increased from 0.057 W to 0.085 W. A 240% rise in radiation load was observed with emissivity increases from 0.06 to 0.20.
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