Selective laser melting for production of a novel high temperature electrothermal propulsion system
Selective laser melting for production of a novel high temperature electrothermal propulsion system
This paper presents the design, manufacturing and analysis of additively manufactured metal components of a novel resistojet thruster for spacecraft. The hardware includes two heat exchanger configurations with integrated nozzle and support structures. Optical analysis is used for investigation of metrology, surface characteristics and morphology. High-resolution micro Computed Tomography (CT) is used as a tool for non-destructive inspection, since the complex geometry of the thruster does not allow internal examination. The CT volume data is used to determine a surface mesh to perform coordinate measurement, nominal/actual comparison and wall thickness analysis.
Romei, F.
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Grubisic, Angelo
a4cab763-bbc0-4130-af65-229ae674e8c8
Gibbon, D.
5eadcfce-74f3-4bd5-a2c5-f9b09a440914
Lane, O.
16728929-ed1c-45e3-b28c-e8ac3dc8bd22
2016
Romei, F.
2c01d8c3-430b-49f8-9c8c-e30d0d135f89
Grubisic, Angelo
a4cab763-bbc0-4130-af65-229ae674e8c8
Gibbon, D.
5eadcfce-74f3-4bd5-a2c5-f9b09a440914
Lane, O.
16728929-ed1c-45e3-b28c-e8ac3dc8bd22
Romei, F., Grubisic, Angelo, Gibbon, D. and Lane, O.
(2016)
Selective laser melting for production of a novel high temperature electrothermal propulsion system.
67th International Astronautical Congress (IAC 2016), , Guadalajara, Mexico.
26 - 30 Sep 2016.
15 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
This paper presents the design, manufacturing and analysis of additively manufactured metal components of a novel resistojet thruster for spacecraft. The hardware includes two heat exchanger configurations with integrated nozzle and support structures. Optical analysis is used for investigation of metrology, surface characteristics and morphology. High-resolution micro Computed Tomography (CT) is used as a tool for non-destructive inspection, since the complex geometry of the thruster does not allow internal examination. The CT volume data is used to determine a surface mesh to perform coordinate measurement, nominal/actual comparison and wall thickness analysis.
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Accepted/In Press date: 21 April 2016
e-pub ahead of print date: September 2016
Published date: 2016
Venue - Dates:
67th International Astronautical Congress (IAC 2016), , Guadalajara, Mexico, 2016-09-26 - 2016-09-30
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 401469
URI: http://eprints.soton.ac.uk/id/eprint/401469
PURE UUID: f3081f1d-a9d8-451b-85de-76a945d2d088
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Date deposited: 17 Oct 2016 14:13
Last modified: 09 Apr 2024 23:24
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Contributors
Author:
D. Gibbon
Author:
O. Lane
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