Hybrid Modeling Method for the Complex Radiative Cooling Network in the Chinese Space Station-Reference-Cited by-同舟云学术

Hybrid Modeling Method for the Complex Radiative Cooling Network in the Chinese Space Station

Published:2023-05 Issue:3 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yuan Man¹,Li Yun-Ze²,Sun Yuehang¹

Affiliation:

1. Ph.D. Student, School of Aeronautic Science and Engineering, Beihang Univ., 37 College Rd., Haidian District, Beijing 100191, China.

2. Professor, School of Aeronautic Science and Engineering, Beihang Univ., 37 College Rd., Haidian District, Beijing 100191, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4850

Reference24 articles.

1. Thermal control of a spacecraft: Backward-implicit scheme programming and coating materials analysis

2. Thermo-mechanical loads on a spacecraft in low Earth orbits

3. Hybrid Radiator for Spacecraft Thermal Control Systems

4. Thermal design, analysis, and testing of the first Turkish 3U communication CubeSat in low earth orbit

5. Thermal alternation induced vibration analysis of spacecraft with lateral solar arrays in orbit

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