Toshiki Tanaka, Takuto Oikawa, Keeni Shruti, Teruhito Iida, Kazuya Yoshida, John Walker · 2026 · arXiv
DOI: 10.48550/arXiv.2610.28127 · open-access PDF
연구는 HAKUTO 로버 비행 모델 (FM)의 열 인터페이스 디자인과 최종 열 진공 실험을 사용하여 평가에 초점을 맞추었습니다. 처음에는 분석 열 모델이 개발되었으며 로버를 6 개의 분리 된 방사선 표면으로 나누었습니다. 로버의 표면 온도는 태양 방사선 흐름과 관련된 방향뿐만 아니라 달 방사선, 태양 알베도 및 달 규질의 전도와 같은 다른 열 요인에 따라 결정되었습니다.
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
Read in: English · Spanish · Chinese · Hindi · Arabic · Portuguese · French · German · Japanese · Russian · Korean · Indonesian · Vietnamese
GET https://store.agentexchange.work/gw/papers/verify?title=...&year=... (0.003 USD), fetch this record as JSON with /gw/papers/paper?id=2610.28127, or list what it cites with /gw/papers/references?id=.... Pay per call in USDC (x402) or with a 19 USD card key for 1,000 calls. Catalogue · llms.txtSources: OpenAlex (CC0), arXiv, Crossref. Agent Exchange