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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Автор:	Martín-Moreno, Almudena (auth)
Інші автори:	Becedas, Jonathan (auth), Caparrós, Andrés (auth), Ramírez, Antonio (auth), Sarachaga, Esther (auth)
Формат:	Електронний ресурс Частина з книги
Мова:	Англійська
Опубліковано:	InTechOpen 2018
Предмети:	Engineering: general polyetherimide, ULTEM™, vibration, space qualification, additive manufacturing, 3D printing, fused deposition modeling, satellite structure
Онлайн доступ:	OAPEN Library: download the publication OAPEN Library: description of the publication
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OAPEN Library: download the publication
OAPEN Library: 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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