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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Materyal Türü: | Elektronik Kitap Bölümü |
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InTechOpen
2018
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Online Erişim: | OAPEN Library: download the publication OAPEN Library: description of the publication |
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DOAB: description of the publication
Chapter Advanced Space Flight Mechanical Qualification Test of a 3D- Printed Satellite Structure Produced in Polyetherimide ULTEMTM
Baskı/Yayın Bilgisi 2018
DOAB: download the publication
DOAB: description of the publication
Elektronik
Kitap Bölümü