熱工学コンファレンス講演論文集
Online ISSN : 2424-290X
セッションID: C114
会議情報

宇宙用逆止弁付振動流型ヒートパイプの軌道上実証結果
安藤 麻紀子岡本 篤田中 洸輔杉田 寛之
著者情報
会議録・要旨集 フリー

詳細
抄録

An oscillating heat pipe (OHP) is desired as an excellent thermal control device for the thermal management system of future spacecraft with larger heat dissipation, and a flat-plate heat pipe (FHP), a type of OHP with check valves, has been developed. Applying FHP to spacecraft, the heat transfer characteristics of FHP under micro-gravity conditions should be examined. The on-orbit experiment of FHP had been conducted since 2012 as one of the Small Demonstration Satellite-4 (SDS-4) missions. FHP showed good heat transfer characteristics, the same as those under 1g conditions, and no degradation was seen for almost 4 years on orbit.

著者関連情報
© 2016 一般社団法人 日本機械学会
前の記事 次の記事
feedback
Top