Toshiki Tanaka, Takuto Oikawa, Keeni Shruti, Teruhito Iida, Kazuya Yoshida, John Walker · 2026 · arXiv
DOI: 10.48550/arXiv.2610.28127 · open-access PDF
Penelitian ini berfokus pada desain antarmuka termal dari Model Penerbangan HAKUTO Rover (FM) dan evaluasinya menggunakan percobaan vakum termal akhir. Awalnya, model termal analitis dikembangkan, membagi rover menjadi enam permukaan radiasi yang berbeda. Suhu permukaan rover kemudian ditentukan berdasarkan orientasinya relatif terhadap aliran radiasi matahari, serta faktor termal lainnya seperti radiasi bulan, albedo solar, dan konduksi dari regulit bulan.
Machine translation (Meta M2M100); the English original follows.
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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