Thermal design verification of a large deployable antenna for a communications satellite
Author:
Affiliation:
1. NTT Radio Communication Systems Laboratories, Yokosuka, Kanagawa 238-03, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26345
Reference8 articles.
1. Thermal control of large spacecraft antenna reflectors
2. INTELSAT V thermal design, testing and flight performance
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2. Microdynamics of Lightweight Precision Deployable Spacecraft Structures;IUTAM-IASS Symposium on Deployable Structures: Theory and Applications;2000
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