Shape memory polymer composite based thin shell structures for modular construction of deployable lunar habitats

PhD by Publication


Jayalath, Henaka Thenennehelage Sandaruwan. 2025. Shape memory polymer composite based thin shell structures for modular construction of deployable lunar habitats. PhD by Publication Doctor of Philosophy. University of Southern Queensland. https://doi.org/10.26192/zzz76
Title

Shape memory polymer composite based thin shell structures for modular construction of deployable lunar habitats

TypePhD by Publication
AuthorsJayalath, Henaka Thenennehelage Sandaruwan
Supervisor
1. FirstA/Pr Jayantha Epaarachchi
2. SecondDr Madhubhashitha Herath
2. SecondMr. Eduardo Trifoni
2. SecondTerry Gdoutos
2. SecondBandu Samarasekara
Institution of OriginUniversity of Southern Queensland
Qualification NameDoctor of Philosophy
Number of Pages326
Year2025
PublisherUniversity of Southern Queensland
Place of PublicationAustralia
Digital Object Identifier (DOI)https://doi.org/10.26192/zzz76
Abstract

Recent global efforts to return to the moon have intensified research into lunar habitats, favouring deployable and rigid structures. Moreover, the durability in unexplored harsh environmental conditions and lower weight are the governing factors of materials for these structures. In this context, shape memory polymer-based composites (SMPCs) are ideal for these habitats because of their potential to create lightweight thin-shell structures and their proven ability to revert to their original shape when stimulated by external factors such as heat. Bisphenol-A Cyanate Ester (BACE) and Polyethylene Glycol (PEG) based shape memory polymers (SMPs) were identified as promising materials due to their high glass transition temperatures and stable thermomechanical properties. Combining BACE with PEG enhances mechanical and shape memory properties, allowing for tailorable thermomechanical properties. The synthesised SMP demonstrated stable thermomechanical properties at the highest lunar ambient temperature (125±2°C) and excellent shape programming at ~170°C. Combined with glass fibre layers and graphene nanoplatelets (GNP), it produced an SMPC with excellent quasi-isotropic properties for manufacturing thin-shell structural components. Adding GNP further enhanced thermal conductivity, increasing the shape recovery effect while acting as a barrier against Atomic Oxygen (AO). The developed SMPC was used to fabricate modular thin-shell hemispherical components. The fabricated components were assembled to demonstrate a hemispherical thin-shell section as a part of a hemispherical dish-end pressure vessel. The fabricated components experimentally showed mechanical integrity and shape memory behaviour, which agreed with their finite element models. The SMPC underwent a series of lunar and space environment-simulated durability tests that showed minimal effect on its mechanical, thermomechanical, and shape-memory properties. This highly durable SMPC is suitable for deployable rigid lunar habitats and space applications, reflecting numerous advancements in future space exploration.

KeywordsDurability of shape memory polymer composites; thin-shell structures; space applications; lunar habitats; high-temperature applications; load-bearing applications
Related Output
Has partDurability and long-term behaviour of shape memory polymers and composites for the space industry - A review of current status and future perspectives
Has partEffect of atomic oxygen and vacuum thermal aging on graphene and glass fibre reinforced cyanate ester-based shape memory polymer composite for deployable thin wall structures
Has partCyanate ester and polyethylene glycol based high temperature resistant shape memory polymer development for space applications
Has partCyanate esters as a high performing shape memory polymer: A review
Has partLay-up configuration of glass fibre on cyanate ester based shape memory polymer composites
Contains Sensitive ContentDoes not contain sensitive content
ANZSRC Field of Research 2020401602. Composite and hybrid materials
400101. Aerospace materials
400199. Aerospace engineering not elsewhere classified
401609. Polymers and plastics
401605. Functional materials
400499. Chemical engineering not elsewhere classified
Public Notes

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Byline AffiliationsSchool of Engineering
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Effect of atomic oxygen and vacuum thermal aging on graphene and glass fibre reinforced cyanate ester-based shape memory polymer composite for deployable thin wall structures
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