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Conceptual thermal design for a spacecraft employing a high-power multibeam phased array
Home
Publications
Conceptual thermal design for a spacecraft employing a high-power multibeam phased array
Conceptual thermal design for a spacecraft employing a high-power multibeam phased array
WK
W. Kelly
W. Kelly
JR
J. Reisenweber
J. Reisenweber
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18 June 1990
conference paper
Published by
American Institute of Aeronautics and Astronautics (AIAA)
https://doi.org/10.2514/6.1990-1670
Abstract
No abstract available
Cited by 2 articles