Analytical studies on design optimization of movable louvers for space use
Author:
Affiliation:
1. National Space Development Agency of Japan, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28018
Reference8 articles.
1. Analysis of movable louvers for temperature control
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1. Passive thermal control systems in spacecrafts;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-02-18
2. Testing of Louver Operability after Spacecraft Launch Distortions;2022 IEEE Aerospace Conference (AERO);2022-03-05
3. Preliminary design and comparative study of thermal control in a nanosatellite through smart variable emissivity surfaces;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-08-22
4. Louvers;Spacecraft Thermal Control;2012
5. Numerical and experimental investigation of thermal louvers for space applications;Journal of the Brazilian Society of Mechanical Sciences;2001
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