Abstract
The Capillary Pumped Deployable radiator (CPDR) is the mission equipment to verify the radiator deployment in the space and to transfer the heat from the equipment inside the CPDR to the deployable radiator by the Capillary Pumped Loop (CPL). It was installed on the Unmanned Space Experimental Recovery System (USERS) that was launched at the Tanegashima Space Center by the H- II launch vehicle on September 10th in 2003. In this paper we describe the summary of CPDR and on-orbit experimental result of CPL that was used in the CPDR.
Original language | English |
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Pages (from-to) | 1655-1662 |
Number of pages | 8 |
Journal | Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B |
Volume | 71 |
Issue number | 706 |
Publication status | Published - 2005 Jun |
Externally published | Yes |
Keywords
- Artery-Type Evaporator
- Capillary Pumped Deployable Radiator
- Capillary Pumped Loop
- Latent Heat
- On Orbit
- Radiator
- Two-Phase Heat Transfer
- USERS
- Wick Structure
ASJC Scopus subject areas
- Mechanical Engineering