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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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Dettagli Bibliografici
Autore principale: Martín-Moreno, Almudena (auth)
Altri autori: Becedas, Jonathan (auth), Caparrós, Andrés (auth), Ramírez, Antonio (auth), Sarachaga, Esther (auth)
Natura: Elettronico Capitolo di libro
Lingua:inglese
Pubblicazione: InTechOpen 2018
Soggetti:
Engineering: general
polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure
Accesso online:OAPEN Library: download the publication
OAPEN Library: description of the publication
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