Ground-engineering study on solar HP/TES receiver for future ISS-JEM experiment program

Hitoshi Naito; Takeshi Hoshino; Tsutomu Fujihara; Kunihisa Eguchi; Kotaro Tanaka; Akira Yamada; Yuichi Ohtani

doi:10.4271/1999-01-2587

Ground-engineering study on solar HP/TES receiver for future ISS-JEM experiment program

Hitoshi Naito, Takeshi Hoshino, Tsutomu Fujihara, Kunihisa Eguchi, Kotaro Tanaka, Akira Yamada, Yuichi Ohtani

Research output: Contribution to journal › Conference article › peer-review

Abstract

A fundamental study was performed to develop a high efficiency solar heat receiver for a solar energy experiment mission on the Japan experiment module - exposed facility of the international space station. It is composed of a solar heat absorber, thermal energy storage and heat pipes. This system is aimed to transport solar thermal energy to a bottoming system with an efficiency of 80 %. Thermal analysis of each component was performed to assess its design approach. One ground testing model of the solar receiver was designed and fabricated in 1998, and then would be experimentally evaluated in 1999 at a test vacuum chamber of National Aerospace Laboratory.

Original language	English
Journal	SAE Technical Papers
DOIs	https://doi.org/10.4271/1999-01-2587
Publication status	Published - 1999 Jan 1
Externally published	Yes
Event	34th Intersociety Energy Conversion Engineering Conference - Vancouver, BC, Canada Duration: 1999 Aug 2 → 1999 Aug 5

ASJC Scopus subject areas

Automotive Engineering
Safety, Risk, Reliability and Quality
Pollution
Industrial and Manufacturing Engineering

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10.4271/1999-01-2587

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title = "Ground-engineering study on solar HP/TES receiver for future ISS-JEM experiment program",

abstract = "A fundamental study was performed to develop a high efficiency solar heat receiver for a solar energy experiment mission on the Japan experiment module - exposed facility of the international space station. It is composed of a solar heat absorber, thermal energy storage and heat pipes. This system is aimed to transport solar thermal energy to a bottoming system with an efficiency of 80 %. Thermal analysis of each component was performed to assess its design approach. One ground testing model of the solar receiver was designed and fabricated in 1998, and then would be experimentally evaluated in 1999 at a test vacuum chamber of National Aerospace Laboratory.",

author = "Hitoshi Naito and Takeshi Hoshino and Tsutomu Fujihara and Kunihisa Eguchi and Kotaro Tanaka and Akira Yamada and Yuichi Ohtani",

year = "1999",

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language = "English",

journal = "SAE Technical Papers",

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note = "34th Intersociety Energy Conversion Engineering Conference ; Conference date: 02-08-1999 Through 05-08-1999",

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T1 - Ground-engineering study on solar HP/TES receiver for future ISS-JEM experiment program

AU - Naito, Hitoshi

AU - Hoshino, Takeshi

AU - Fujihara, Tsutomu

AU - Eguchi, Kunihisa

AU - Tanaka, Kotaro

AU - Yamada, Akira

AU - Ohtani, Yuichi

PY - 1999/1/1

Y1 - 1999/1/1

N2 - A fundamental study was performed to develop a high efficiency solar heat receiver for a solar energy experiment mission on the Japan experiment module - exposed facility of the international space station. It is composed of a solar heat absorber, thermal energy storage and heat pipes. This system is aimed to transport solar thermal energy to a bottoming system with an efficiency of 80 %. Thermal analysis of each component was performed to assess its design approach. One ground testing model of the solar receiver was designed and fabricated in 1998, and then would be experimentally evaluated in 1999 at a test vacuum chamber of National Aerospace Laboratory.

AB - A fundamental study was performed to develop a high efficiency solar heat receiver for a solar energy experiment mission on the Japan experiment module - exposed facility of the international space station. It is composed of a solar heat absorber, thermal energy storage and heat pipes. This system is aimed to transport solar thermal energy to a bottoming system with an efficiency of 80 %. Thermal analysis of each component was performed to assess its design approach. One ground testing model of the solar receiver was designed and fabricated in 1998, and then would be experimentally evaluated in 1999 at a test vacuum chamber of National Aerospace Laboratory.

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SN - 0148-7191

T2 - 34th Intersociety Energy Conversion Engineering Conference

Y2 - 2 August 1999 through 5 August 1999

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