The University of Southampton
University of Southampton Institutional Repository

An overview of the application of 3D printed spacecraft structures within the ReDSHIFT project

An overview of the application of 3D printed spacecraft structures within the ReDSHIFT project
An overview of the application of 3D printed spacecraft structures within the ReDSHIFT project
The investigation of additive manufacturing technology started in the 1980’s and over the previousfour decades has developed dramatically. The advantages of this technology, such as increased geometricaldesign freedom, faster production times, the possibility of increased functional integration, the reduction ofmaterial waste and reduced costs have driven the development of this technology in many market sectors.However, the benefits of additive manufacturing is only starting to be realised within the spacecraftindustry. Within the last five years there has been a growing momentum of research and development intothe application of additive manufacturing for spacecraft and in many cases, this has been constrained tothe optimisation and production of small secondary structural components. The European Union funded1Paper ID: 52963oralresearch project entitled ‘ReDSHIFT’ (Revolutionary Design of Spacecraft through Holistic Integration ofFuture Technologies) began in 2016 and focused on passive means of reducing the impact of space debrisby prevention, mitigation and protection. The main innovative aspect of the project came as a result ofa synergy between theoretical and experimental aspects, such as long term astrodynamics simulations,de-orbiting devices, hypervelocity impact testing, design for demise and the application of 3D printingfor future satellite design. This paper will present an overview of the work performed on the applicationof 3D printing to future satellite design as part of the ReDSHIFT project, which finished in March 2019,along with the key results. This work was led by the University of Southampton in the UK with thecoordination and support of the project partners and involved the design, simulation and test of manyfunctional components as well as a complete 3D printed small satellite 8U cubesat structure. The workperformed within ReDSHIFT has enabled the potential of this technology for multiple applications to bequantifiably identified.
International Astronautical Federation
Walker, Scott
f28a342f-9755-48fd-94ea-09e44ac4dbf5
Romei, Federico
cdc577fd-8552-41f2-917d-e359ef65a149
Rodriguez, Jonathan Becedas
95727f1e-1cb0-49c2-91cd-1e243530c0db
Vedova, Florio Dalla
24f1f409-b4eb-403f-97ec-8c58b8a36885
Beck, James
8246ed92-e608-420b-ad57-7a0fdcfe0b9d
Holbrough, Ian
331dd2c1-ddd0-4695-b9d8-d303aac3604d
Francesconi, Alessandro
c476137b-8c0b-49d1-9a42-7a0f44572525
Olivieri, Lorenzo
4dad3a04-79eb-4993-9750-1179d4d712fb
Caparros, Andrés
031f8bc3-aa1b-41d0-969b-1ecc2a9718f2
Rodriguez Flores, Geraldo
64b31ad7-f5b3-4741-a2a1-7dc1113c2698
Morillo, Pablo
51173a85-1196-4d04-815e-9939f2ea1bee
Stokes, Hedley
28d5ee93-2722-4fab-9ebb-9f3a4be52f15
Rossi, A
1245f3da-4350-469e-94dd-d19e43e0fbe8
Colombo, C.
9bf7fbdc-abab-4f6e-823a-a8b4ec9663b3
Walker, Scott
f28a342f-9755-48fd-94ea-09e44ac4dbf5
Romei, Federico
cdc577fd-8552-41f2-917d-e359ef65a149
Rodriguez, Jonathan Becedas
95727f1e-1cb0-49c2-91cd-1e243530c0db
Vedova, Florio Dalla
24f1f409-b4eb-403f-97ec-8c58b8a36885
Beck, James
8246ed92-e608-420b-ad57-7a0fdcfe0b9d
Holbrough, Ian
331dd2c1-ddd0-4695-b9d8-d303aac3604d
Francesconi, Alessandro
c476137b-8c0b-49d1-9a42-7a0f44572525
Olivieri, Lorenzo
4dad3a04-79eb-4993-9750-1179d4d712fb
Caparros, Andrés
031f8bc3-aa1b-41d0-969b-1ecc2a9718f2
Rodriguez Flores, Geraldo
64b31ad7-f5b3-4741-a2a1-7dc1113c2698
Morillo, Pablo
51173a85-1196-4d04-815e-9939f2ea1bee
Stokes, Hedley
28d5ee93-2722-4fab-9ebb-9f3a4be52f15
Rossi, A
1245f3da-4350-469e-94dd-d19e43e0fbe8
Colombo, C.
9bf7fbdc-abab-4f6e-823a-a8b4ec9663b3

Walker, Scott, Romei, Federico, Rodriguez, Jonathan Becedas, Vedova, Florio Dalla, Beck, James, Holbrough, Ian, Francesconi, Alessandro, Olivieri, Lorenzo, Caparros, Andrés, Rodriguez Flores, Geraldo, Morillo, Pablo, Stokes, Hedley, Rossi, A and Colombo, C. (2019) An overview of the application of 3D printed spacecraft structures within the ReDSHIFT project. In 70th International Astronautical Congress (IAC). International Astronautical Federation..

Record type: Conference or Workshop Item (Paper)

Abstract

The investigation of additive manufacturing technology started in the 1980’s and over the previousfour decades has developed dramatically. The advantages of this technology, such as increased geometricaldesign freedom, faster production times, the possibility of increased functional integration, the reduction ofmaterial waste and reduced costs have driven the development of this technology in many market sectors.However, the benefits of additive manufacturing is only starting to be realised within the spacecraftindustry. Within the last five years there has been a growing momentum of research and development intothe application of additive manufacturing for spacecraft and in many cases, this has been constrained tothe optimisation and production of small secondary structural components. The European Union funded1Paper ID: 52963oralresearch project entitled ‘ReDSHIFT’ (Revolutionary Design of Spacecraft through Holistic Integration ofFuture Technologies) began in 2016 and focused on passive means of reducing the impact of space debrisby prevention, mitigation and protection. The main innovative aspect of the project came as a result ofa synergy between theoretical and experimental aspects, such as long term astrodynamics simulations,de-orbiting devices, hypervelocity impact testing, design for demise and the application of 3D printingfor future satellite design. This paper will present an overview of the work performed on the applicationof 3D printing to future satellite design as part of the ReDSHIFT project, which finished in March 2019,along with the key results. This work was led by the University of Southampton in the UK with thecoordination and support of the project partners and involved the design, simulation and test of manyfunctional components as well as a complete 3D printed small satellite 8U cubesat structure. The workperformed within ReDSHIFT has enabled the potential of this technology for multiple applications to bequantifiably identified.

This record has no associated files available for download.

More information

Published date: 23 December 2019
Venue - Dates: 70th International Astronautical Congress, , Washington, United States, 2019-10-22 - 2019-10-25

Identifiers

Local EPrints ID: 471229
URI: http://eprints.soton.ac.uk/id/eprint/471229
PURE UUID: 2867147f-5d4f-4935-a827-d3bbe39387ff
ORCID for Federico Romei: ORCID iD orcid.org/0000-0003-2283-4658

Catalogue record

Date deposited: 01 Nov 2022 17:33
Last modified: 19 Apr 2024 17:25

Export record

Contributors

Author: Scott Walker
Author: Federico Romei ORCID iD
Author: Jonathan Becedas Rodriguez
Author: Florio Dalla Vedova
Author: James Beck
Author: Ian Holbrough
Author: Alessandro Francesconi
Author: Lorenzo Olivieri
Author: Andrés Caparros
Author: Geraldo Rodriguez Flores
Author: Pablo Morillo
Author: Hedley Stokes
Author: A Rossi
Author: C. Colombo

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×