Research Papers
A collection of my academic and research publications:
Multi-point design optimisation of microwave electrothermal thruster nozzles for robust in-space operation
Authors: Jack Gale, Madeline Farrugia, Keisuke Suenaga, Suk Hyun Yeo, Gail N. Iles, Hideaki Ogawa
Published in: Aerospace Science & Technology, 2026
~In preparation~Multi-Point Design Optimisation of Microwave Electrothermal Thruster Nozzles for Robust In-Space Operation
Authors: Madeline Farrugia, Keisuke Suenaga, Suk Hyun Yeo, Jack Gale, Gail Iles, Hideaki Ogawa
Published in: IAC, 2025
Microwave electrothermal thrusters (METs), characterised by their considerably high thrust and a broad specific impulse range, offer advantages over other electric propulsion systems in terms of operational lifetime, thruster efficiency, and propellant selection. However, the complex phenomena associated with the multi-physics behaviour of MET operation pose challenges in optimising system components. One notable challenge arises with miniaturised nozzles, caused by significant boundary layer effects, necessitating meticulous consideration in the design process. Multi-objective design optimisation is performed for MET nozzles by incorporating computational fluid dynamics simulations coupled with evolutionary algorithms supported by surrogate model predictions based on machine learning for multiple operating conditions. This approach enables global design optimisation of MET nozzles to maximise performance with respect to flow velocity, thereby enhancing thrust and specific impulse for robust operation against variations in MET chamber conditions. The flowfields within the nozzle and their effects on performance are scrutinised for selected optimal geometries, offering valuable insights into the underlying physical phenomena. Covariance-based sensitivity analysis is performed to identify key design variables and understand their interactions and interdependencies in the physical characterisation and modelling of miniaturised nozzles. Significant effects of the nozzle divergent angle and throat radius on performance have been identified, as they play crucial roles in shaping the flowfield at the nozzle exit, consequently influencing thrust generation.
Read More →LithoSpace: A Democratised Spatial Data Platform for Extraterrestrial Geoscience and Geochemical Mapping
Authors: Wayne Noble, Fabian Kohlmann, Jack Gale, Ben Dib, Gail Iles, Brandon Mahan, Moritz Theile
Published in: EGU General Assembly, 2025
This study showcases how LithoSpace's unique cloud-based geochemistry tools can visualise slight variations in geochemical composition using existing, standardised, and cleaned lunar and martian geochemical data. The analysis confirms previously known findings, such as the basaltic geochemical composition of Apollo 11 samples and the wide range of geochemical composition of rocks on Mars as analysed by the Curiosity rover. However, it more importantly highlights how LithoSpace facilitates improved, user-friendly analytics, enabling “on-the-fly” calculation, interpretations and rock classifications. As more data is collected, LithoSpace will enhance our ability to develop new theories about planetary formation and assist with improved geological mapping of extra-terrestrial bodies.
Read More →Honours Thesis
My thesis submitted in fulfillment of the requirements for the degree of Bachelor of Science (Physics) (Honours) at R.M.I.T.
Investigation into Geometric Characteristics of Micro Parabolic Nozzle and Multi-Objective Design Optimisation
Submitted: October, 2025
Brief summary: Evolutionary algorithms, a type of advanced machine learning, are used to optimise a millimetre scale satellite thruster nozzle. Differences between the mathematical optimal design and physical reality occur due to performance losses, namely friction along the walls which generates a boundary layer effect. This study aimed to utilise this machine learning to optimise a parabolic nozzle shape at the millimetre scale. Parabolic nozzles, characterised by their curved shape, are regarded as one of the best designs for rocketry at the metre scale. This study provides evidence that the parabolic geometry still outperforms conical geometry at the millimetre scale. The optimised parabolic nozzles excelled in directing exhaust flow out of the nozzle in the correct direction, while also producing high thrust and fuel efficiency.
Download PDF →Other Work
Additional work that I have produced that I'm particularly proud of and want to document: