## Abstract High‐powered satellites need larger heat rejection areas. A deployable radiator is one of the key technologies for a high‐powered satellite bus. A Reservoir Embedded Loop Heat Pipe (RELHP) is a two‐phase heat transfer device that constitutes the deployable radiator. RELHP has an evapora
Study on heat transfer characteristics of reservoir embedded loop heat pipe (1st report, Influence of evaporator orientation against gravity and charged liquid weight on heat transfer characteristics)
✍ Scribed by Hiroaki Ishikawa; Tetsuro Ogushi; Takehide Nomura; Takeshi Iwakami; Hiroyuki Noda; Takahiro Yabe
- Publisher
- John Wiley and Sons
- Year
- 2007
- Tongue
- English
- Weight
- 596 KB
- Volume
- 36
- Category
- Article
- ISSN
- 1099-2871
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✦ Synopsis
Abstract
High‐powered satellites need larger heat rejection areas. A deployable radiator is one of the key technologies for a high‐powered satellite bus. A Reservoir Embedded Loop Heat Pipe (RELHP) is a two‐phase heat transfer device that constitutes a deployable radiator. RELHP has an evaporator core which is used as a liquid reservoir to enhance operational reliability. This paper presents the heat transport characteristics of a RELHP under changing evaporator orientation against gravity and charged ammonia weight by experiment and calculation. Liquid slug position in the reservoir has a great influence on heat transport characteristics, caused by changing heat transfer coefficients between returned liquid into the evaporator and vapor in the reservoir. © 2007 Wiley Periodicals, Inc. Heat Trans Asian Res, 36(3): 143– 157, 2007; Published online in Wiley InterScience (www.interscience.wiley.com). DOI 10.1002/htj.20150
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