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Chapter Advanced Space Flight Mechanical Qualification Test of a 3D- Printed Satellite Structure Produced in Polyetherimide ULTEMTM

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The aim of this work is to demonstrate the use of additive manufacturing with thermoplastic material in the whole functional structure of spacecraft and to mechanically qualify it for space flight. For such purpose, an 8 U CubeSat structure was manufactured in polyetherimide (PEI) ULTEM™ through 3D...

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Bibliographic Details
Main Author: Martín-Moreno, Almudena (auth)
Other Authors: Becedas, Jonathan (auth), Caparrós, Andrés (auth), Ramírez, Antonio (auth), Sarachaga, Esther (auth)
Format: Electronic Book Chapter
Language:English
Published: InTechOpen 2018
Subjects:
Engineering: general
polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure
Online Access:DOAB: download the publication
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