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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Bibliographische Detailangaben
1. Verfasser:	Martín-Moreno, Almudena (auth)
Weitere Verfasser:	Becedas, Jonathan (auth), Caparrós, Andrés (auth), Ramírez, Antonio (auth), Sarachaga, Esther (auth)
Format:	Elektronisch Buchkapitel
Sprache:	Englisch
Veröffentlicht:	InTechOpen 2018
Schlagworte:	Engineering: general polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure
Online-Zugang:	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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