Ablative thermal protection systems. The project will study ablative reentry heat shields by experiments simulating hypervelocity atmospheric flight. The results will enable the design of the advanced spacecraft which are needed to extend mans exploration of the universe. Data will be validated by comparison with flights such as the Japanese Hayabusa asteroid sample return mission.
Discovery Early Career Researcher Award - Grant ID: DE190101152
Funder
Australian Research Council
Funding Amount
$404,000.00
Summary
Micro/nano-mechanical testing methodologies for interfacial adhesion. This project aims to develop reliable approaches for measuring the toughness of a variety of metal/polymer interfaces integral to contemporary flexible devices. Adhesion between metal thin film conductors and polymer substrates is a critical factor influencing the reliability of the emerging polymer-based flexible electronics. This project will develop new methodologies for understanding the behaviour of these metal/polymer in ....Micro/nano-mechanical testing methodologies for interfacial adhesion. This project aims to develop reliable approaches for measuring the toughness of a variety of metal/polymer interfaces integral to contemporary flexible devices. Adhesion between metal thin film conductors and polymer substrates is a critical factor influencing the reliability of the emerging polymer-based flexible electronics. This project will develop new methodologies for understanding the behaviour of these metal/polymer interfaces. This project will be a crucial enabler to accelerating the development of new flexible microelectronic technologies, from solar panels to electronic skin. This innovation will enable Australia to maintain an important connection to the rapidly-evolving international microelectronic industry and add significant value to Australian manufacturing industries.Read moreRead less
Most eye diseases have a genetic contribution, whether rare disorders affecting children such as retinoblastoma or congenital cataracts through to common disorders of older people such as myopia, age-related macular degeneration or glaucoma. We will continue our successful research to find genes that cause these diseases and use this to improve patient care and prevent blindness. We will work out how families can use this genetic information to participate in trials to develop new treatments.
Flow physics of porous wall fuel injection for scramjet combustion and drag reduction. This project combines world-class Australian scramjet science with German advanced high temperature materials, exploring potentially transformational technology for satellite launch. Australia’s credentials in the international space arena will strengthen, contributing to assured access to the space-based applications upon which we heavily depend.
Discovery Early Career Researcher Award - Grant ID: DE240101231
Funder
Australian Research Council
Funding Amount
$411,837.00
Summary
Quinoid Polymers for Organic Electrochemical Transistors and Bioelectronics. This project aims to develop organic semiconductors (OSCs) with excellent mechanical flexibility and biocompatibility to exploit their potentials in bioelectronics. It connects the electronic world with ionic world of biology to push the biomedical application of OSCs a big step forward. Interdisciplinary knowledge, intellectual properties (IPs), top-notch publications, invited talks, and international collaborations ar ....Quinoid Polymers for Organic Electrochemical Transistors and Bioelectronics. This project aims to develop organic semiconductors (OSCs) with excellent mechanical flexibility and biocompatibility to exploit their potentials in bioelectronics. It connects the electronic world with ionic world of biology to push the biomedical application of OSCs a big step forward. Interdisciplinary knowledge, intellectual properties (IPs), top-notch publications, invited talks, and international collaborations are expected. Additionally, it will earn Australia a commercial lead in the biomedical sector to attract more talents to serve Australia. This project also matches well with several government’s strategic research priorities, attracting industries to realise IPs transfer to bring “great value for money” to feed back Australia.Read moreRead less
Radiation and Ablation in Rapidly Expanding Flows. The aim of the project is to record the spectra of radiation from a region of rapidly expanding flow representative of the passage of the shock layer on a re-entry capsule from the windward to the leeward surfaces. The significance of this work is that it addresses a critical area of spacecraft where the uncertainties of our design techniques are of the order of 300 per cent in terms of surface heat transfer, and current vehicles have to use lar ....Radiation and Ablation in Rapidly Expanding Flows. The aim of the project is to record the spectra of radiation from a region of rapidly expanding flow representative of the passage of the shock layer on a re-entry capsule from the windward to the leeward surfaces. The significance of this work is that it addresses a critical area of spacecraft where the uncertainties of our design techniques are of the order of 300 per cent in terms of surface heat transfer, and current vehicles have to use large safety factors to ensure survivability. The outputs from the project will be a data base of radiative parameters which should enable accurate models of the flow to be developed, which is expected to facilitate the design of advanced spacecraft with greater safety and reliability, and with lower structural mass.Read moreRead less
Discovery Early Career Researcher Award - Grant ID: DE170100263
Funder
Australian Research Council
Funding Amount
$360,000.00
Summary
Magnetohydrodynamic aerobraking to land heavy payloads on Mars. This project aims to decelerate space vehicles by applying a magnetic field to the hot ionised gases that form around the vehicle. In the thin atmosphere of Mars, aerodynamic drag alone is not enough to land a spacecraft larger than 1 tonne. A human mission to Mars requires landing of payloads up to 80 tonnes. Interaction of the magnetic field with the ionised flow dissipates kinetic energy and can reduce surface heating. This proje ....Magnetohydrodynamic aerobraking to land heavy payloads on Mars. This project aims to decelerate space vehicles by applying a magnetic field to the hot ionised gases that form around the vehicle. In the thin atmosphere of Mars, aerodynamic drag alone is not enough to land a spacecraft larger than 1 tonne. A human mission to Mars requires landing of payloads up to 80 tonnes. Interaction of the magnetic field with the ionised flow dissipates kinetic energy and can reduce surface heating. This project could make Mars-return missions feasible by enabling greatly increased payloads. It also aims to evaluate magnetohydrodynamic braking and heat mitigation at true flight conditions.Read moreRead less
Non-equilibrium reacting shock layers. This project aims is to study the non-equilibrium aerodynamic processes involved in hypervelocity flight. The design of vehicles for high speed flight is critically dependent on modelling the interactions between the flow field and the airframe, and the current lack of understanding is restricting the scope and benefit of viable activities in space. The expected outcomes include the ability to design optimised heat shields and air-frames with minimum mass a ....Non-equilibrium reacting shock layers. This project aims is to study the non-equilibrium aerodynamic processes involved in hypervelocity flight. The design of vehicles for high speed flight is critically dependent on modelling the interactions between the flow field and the airframe, and the current lack of understanding is restricting the scope and benefit of viable activities in space. The expected outcomes include the ability to design optimised heat shields and air-frames with minimum mass and maximum payload, precisely targeting specific flight conditions and vehicle shapes. The prospective benefits include increased productivity and reliability and reduced cost of missions to and from space, and a proliferation of new applications which this understanding will facilitate.Read moreRead less
Turbulent heat transfer during Mars Venus and Earth atmospheric entry. This project aims to design better heat shields for spacecraft. Designing heat shields for re-entry vehicles needs good models to predict aerodynamic heating. Conventional wind tunnels cannot measure aerodynamic heating in ground tests in the region of peak heating, making design uncertain and risky. This project will use a free-piston-driven expansion tunnel that can produce flows fast and dense enough to measure heating for ....Turbulent heat transfer during Mars Venus and Earth atmospheric entry. This project aims to design better heat shields for spacecraft. Designing heat shields for re-entry vehicles needs good models to predict aerodynamic heating. Conventional wind tunnels cannot measure aerodynamic heating in ground tests in the region of peak heating, making design uncertain and risky. This project will use a free-piston-driven expansion tunnel that can produce flows fast and dense enough to measure heating for turbulent boundary layers at the highest speeds encountered during re-entry. This should allow scientists to test and develop theoretical and numerical models of heating and so improve spacecraft design.Read moreRead less