Comparative Study of Deployable Satellite Solar Panel Structure between Carbon Fiber Reinforced Polymer and Al-7075 Honeycomb
Author:
Affiliation:
1. Research Center for Satellite Technology BRIN,Bogor,Indonesia
2. Research Center of Satellite Technology BRIN,Bogor,Indonesia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9993425/9992293/09993517.pdf?arnumber=9993517
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1. Configuration design and modeling of an efficient small satellite structure
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3. Design and Reliability Simulation of a $G$-Band Traveling-Wave Tube Multistage Depressed Collector With Curving Radiators Using FEA Method;IEEE Transactions on Plasma Science;2024
4. Electromagnetic Shielding Performance of Twill Carbon Fiber Reinforced Polymer with Free Space Method in UHF, L Band, and S Band Frequency Range;2023 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES);2023-10-26
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