#7451. Computational modeling of the curing of a frame of an inflatable satellite antenna in near-earth orbit

October 2026publication date
Proposal available till 18-05-2025
4 total number of authors per manuscript0 $

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Journal’s subject area:
Ocean Engineering;
Applied Mathematics;
Computational Mechanics;
Computational Mathematics;
Mechanical Engineering;
Computational Theory and Mathematics;
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Abstract:
Temperature analysis of a new technological process, curing of prepregs in near-earth orbit, is performed via computational modeling. The problem arose in connection with the currently discussed possibility of using inflatable antennas for small space satellites. Inflatable antennas have a number of advantages over classic extendable metal antennas. However, in order to ensure the continuous operation of inflatable antennas, it is necessary that they acquire rigidity over time and cease to depend on the pressure of air in them. This can be achieved using a frame made of an orbital-curable prepreg.
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