Heat transfer influence of solar panel on spacecraft

Reem Almehisni; Fadi Al Naimat

doi:10.1109/ICASET.2018.8376815

Heat transfer influence of solar panel on spacecraft

Reem Almehisni, Fadi Al Naimat

Department of Mechanical and Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

3 Citations (Scopus)

Abstract

In this paper, thermal analysis is carried out on solar panels used in space applications. Solar panels on spacecraft undergo harsh thermal environment of space where they experience extreme high temperature exceeding 120°C and a very low temperature around -170°C. This study investigates the thermal effect of solar panel heat flux, with temperature range between -60°C to 100 °C subjected to a spacecraft's structure. In addition, thermal analysis simulation for different heat transfer paths between a solar panel and a spacecraft has been investigated. The different heat paths are compared in the study to predict the most effective heat path.

Original language	English
Title of host publication	2018 Advances in Science and Engineering Technology International Conferences, ASET 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1-6
Number of pages	6
ISBN (Electronic)	9781538623992
DOIs	https://doi.org/10.1109/ICASET.2018.8376815
Publication status	Published - Jun 8 2018
Event	2018 Advances in Science and Engineering Technology International Conferences, ASET 2018 - Dubai, Sharjah, Abu Dhabi, United Arab Emirates Duration: Feb 6 2018 → Apr 5 2018

Publication series

Name	2018 Advances in Science and Engineering Technology International Conferences, ASET 2018

Other

Other	2018 Advances in Science and Engineering Technology International Conferences, ASET 2018
Country/Territory	United Arab Emirates
City	Dubai, Sharjah, Abu Dhabi
Period	2/6/18 → 4/5/18

Keywords

Heat Transfer
Spacecraft
solar panels

ASJC Scopus subject areas

Energy Engineering and Power Technology
Renewable Energy, Sustainability and the Environment
Civil and Structural Engineering
Mechanics of Materials
Safety, Risk, Reliability and Quality
Waste Management and Disposal
Water Science and Technology

Access to Document

10.1109/ICASET.2018.8376815

Cite this

Almehisni, R., & Al Naimat, F. (2018). Heat transfer influence of solar panel on spacecraft. In 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018 (pp. 1-6). (2018 Advances in Science and Engineering Technology International Conferences, ASET 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICASET.2018.8376815

Heat transfer influence of solar panel on spacecraft. / Almehisni, Reem; Al Naimat, Fadi.
2018 Advances in Science and Engineering Technology International Conferences, ASET 2018. Institute of Electrical and Electronics Engineers Inc., 2018. p. 1-6 (2018 Advances in Science and Engineering Technology International Conferences, ASET 2018).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Almehisni, R & Al Naimat, F 2018, Heat transfer influence of solar panel on spacecraft. in 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018. 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018, Institute of Electrical and Electronics Engineers Inc., pp. 1-6, 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018, Dubai, Sharjah, Abu Dhabi, United Arab Emirates, 2/6/18. https://doi.org/10.1109/ICASET.2018.8376815

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abstract = "In this paper, thermal analysis is carried out on solar panels used in space applications. Solar panels on spacecraft undergo harsh thermal environment of space where they experience extreme high temperature exceeding 120°C and a very low temperature around -170°C. This study investigates the thermal effect of solar panel heat flux, with temperature range between -60°C to 100 °C subjected to a spacecraft's structure. In addition, thermal analysis simulation for different heat transfer paths between a solar panel and a spacecraft has been investigated. The different heat paths are compared in the study to predict the most effective heat path.",

keywords = "Heat Transfer, Spacecraft, solar panels",

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AB - In this paper, thermal analysis is carried out on solar panels used in space applications. Solar panels on spacecraft undergo harsh thermal environment of space where they experience extreme high temperature exceeding 120°C and a very low temperature around -170°C. This study investigates the thermal effect of solar panel heat flux, with temperature range between -60°C to 100 °C subjected to a spacecraft's structure. In addition, thermal analysis simulation for different heat transfer paths between a solar panel and a spacecraft has been investigated. The different heat paths are compared in the study to predict the most effective heat path.

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T3 - 2018 Advances in Science and Engineering Technology International Conferences, ASET 2018

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Heat transfer influence of solar panel on spacecraft

Abstract

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Keywords

ASJC Scopus subject areas

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