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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Autors principals:	Martín-Moreno, Almudena, Becedas, Jonathan, Caparrós, Andrés, Ramírez, Antonio, Sarachaga, Esther
Format:	Online
Idioma:	anglès
Publicat:	InTechOpen 2021
Matèries:	polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBC Engineering: general
Accés en línia:	ONIX_20210602_10.5772/intechopen.79852_379
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