Qualification of Composite Structure for Cubesat Picosatellites as a Demonstration for Small Satellite Elements-Reference-Cited by-同舟云学术

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Qualification of Composite Structure for Cubesat Picosatellites as a Demonstration for Small Satellite Elements

Published:2014-09-02 Issue: Volume: Page:1-10
ISSN:2470-4415
Container-title:International Journal of Aeronautical Science & Aerospace Research
language:
Short-container-title:IJASAR

Author:

A Ampatzoglou, ,A Baltopoulos,A Kotzakolios,V Kostopoulos, , ,

Publisher

SciDoc Publishers LLC

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Modular Multifunctional Composite Structure for CubeSat Applications: Embedded Battery Prototype Modal Analysis;Aerospace;2023-11-30

2. Optimization of 1U nanosatellite on the basis of strength and weight using different Materials: A numerical approach;Materials Today: Proceedings;2022

3. Alternative proposal, based on systems-engineering methods, aimed at substituting with carbon-epoxy laminates the load-bearing aluminum sandwiches employed in the structure of a small satellite;Advances in Space Research;2020-07

4. Thermal properties and degradation kinetics of epoxy-γ-alumina and epoxy-zinc oxide light weight composites;Revista Mexicana de Física;2020-07-01

5. Modular Multifunctional Composite Structure for CubeSat Applications: Preliminary Design and Structural Analysis;Aerospace;2020-02-24

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