A review of the processing, composition and temperature-dependent mechanical and thermal properties of dielectric technical ceramics

Files in This Item:
 File SizeFormat
DownloadDe_Faoite_-_2012_-_A_Review_of_the_Processing,_Composition_and_Temperature-Dependent.pdf485.97 kBAdobe PDF
Title: A review of the processing, composition and temperature-dependent mechanical and thermal properties of dielectric technical ceramics
Authors: de Faoite, DaithíBrowne, David J.Chang-Díaz, Franklin R.Stanton, Kenneth T.
Permanent link: http://hdl.handle.net/10197/8477
Date: May-2012
Online since: 2017-05-05T12:27:11Z
Abstract: The current review uses the material requirements of a new space propulsion device, the Variable Specific Impulse Magnetoplasma Rocket (VASIMR®) as a basis for presenting the temperature dependent properties of a range of dielectric ceramics, but data presented could be used in the engineering design of any ceramic component with complementary material requirements. A material is required for the gas containment tube (GCT) of VASIMR® to allow it to operate at higher power levels. The GCT's operating conditions place severe constraints on the choice of material. A dielectric is required with a high thermal conductivity, low dielectric loss factor, and high thermal shock resistance. There is a lack of a representative set of temperature-dependent material property data for materials considered for this application and these are required for accurate thermo-structural modelling. This modelling would facilitate the selection of an optimum material for this component. The goal of this paper is to determine the best material property data values for use in the materials selection and design of such components. A review of both experimentally and theoretically-determined temperature-dependent & room temperature properties of several materials has been undertaken. Data extracted are presented by property. Properties reviewed are density, Young's, bulk and shear moduli, Poisson's ratio, tensile, flexural and compressive strength, thermal conductivity, specific heat capacity, thermal expansion coefficient and the factors affecting maximum service temperature. Materials reviewed are alumina, aluminium nitride, beryllia, fused quartz, sialon and silicon nitride.
Funding Details: FAS Science Challenge Programme
Type of material: Journal Article
Publisher: Springer
Journal: Materials Science
Volume: 47
Issue: 10
Start page: 4211
End page: 4235
Copyright (published version): 2011 Springer
Keywords: Electric propulsionPlasmaSpace materialsGas containment tubeThermal propertiesMechanical propertiesCeramics
DOI: 10.1007/s10853-011-6140-1
Language: en
Status of Item: Peer reviewed
This item is made available under a Creative Commons License: https://creativecommons.org/licenses/by-nc-nd/3.0/ie/
Appears in Collections:Mechanical & Materials Engineering Research Collection

Show full item record

Citations 5

Last Week
Last month
checked on Sep 11, 2020

Page view(s)

Last Week
Last month
checked on Jan 23, 2022

Download(s) 20

checked on Jan 23, 2022

Google ScholarTM



If you are a publisher or author and have copyright concerns for any item, please email research.repository@ucd.ie and the item will be withdrawn immediately. The author or person responsible for depositing the article will be contacted within one business day.