Thermal Numerical Analysis of the Primary Composite Structure of a CubeSat

Thermal Numerical Analysis of the Primary Composite Structure of a CubeSat

A thermal computational analysis for the composite structure of a CubeSat is presented. The main purpose of this investigation is to study the thermal performance of carbon fibre/epoxy resin composite materials with Zinc Oxide nanoparticles in order to be used in the panels of the primary structure...

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Bibliographic Details
Main Authors: Saul Piedra, Mauricio Torres, Saul Ledesma
Format: Article
Language:English
Published: MDPI AG 2019-09-01
Series:Aerospace
Subjects:
CubeSat
composite structure
thermal analysis
Online Access:https://www.mdpi.com/2226-4310/6/9/97

Internet

https://www.mdpi.com/2226-4310/6/9/97

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