Design and implementation of thermal control strategy for micro-size lunar exploration rover hakuto

Toshiki Tanaka, Takuto Oikawa, Keeni Shruti, Teruhito Iida, Kazuya Yoshida, John Walker · 2026 · arXiv

DOI: 10.48550/arXiv.2610.28127 · open-access PDF

Abstract

The research focuses on the thermal interface design of the HAKUTO Rover Flight Model (FM) and its evaluation using the final thermal vacuum experiment. Initially, an analytical thermal model was developed, dividing the rover into six distinct radiating surfaces. The surface temperature of the rover was then determined based on its orientation relative to the solar radiative flux, as well as other thermal factors such as lunar radiation, solar albedo, and conduction from the lunar regolith. By considering the impact of these heat sources, suitable mounting locations for the avionics and the an

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