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

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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Bibliografische gegevens
Hoofdauteur:	Martín-Moreno, Almudena (auth)
Andere auteurs:	Becedas, Jonathan (auth), Caparrós, Andrés (auth), Ramírez, Antonio (auth), Sarachaga, Esther (auth)
Formaat:	Elektronisch Hoofdstuk
Taal:	Engels
Gepubliceerd in:	InTechOpen 2018
Onderwerpen:	Engineering: general polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure
Online toegang:	DOAB: download the publication DOAB: description of the publication
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DOAB: download the publication
DOAB: description of the publication

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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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