Discovery Early Career Researcher Award - Grant ID: DE240100040
Funder
Australian Research Council
Funding Amount
$442,302.00
Summary
Quality Assurance of Mobile Applications by Effective Testing and Repair. This project aims to create advanced techniques that will enable software engineers to effectively develop quality assured and robust software systems. This project expects to generate new and innovative approaches that automate software testing and repair. The expected outcomes of this project include new knowledge of software engineering, development of an automated and cost-effective testing system with improved coverag ....Quality Assurance of Mobile Applications by Effective Testing and Repair. This project aims to create advanced techniques that will enable software engineers to effectively develop quality assured and robust software systems. This project expects to generate new and innovative approaches that automate software testing and repair. The expected outcomes of this project include new knowledge of software engineering, development of an automated and cost-effective testing system with improved coverage, greater bug detection and repair, and faster testing protocols. This should provide significant benefits to software users by providing reliable and user-friendly systems and to software companies to position Australia as a global leader in software development and technological advancement.Read moreRead less
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE210100050
Funder
Australian Research Council
Funding Amount
$670,000.00
Summary
Spacecraft Innovation Laboratory. The Australian Spacecraft Innovation Laboratory is designed to provide researchers and entrepreneurs with a venue to integrate and test their “cubesats”, satellites the size of a loaf of bread, and small payloads. By centralising the satellite integration function, the standard of Australian space assets can be assured, giving researchers confidence that their spacebased experiments will succeed. Knowledge transfer to space start-ups will be accelerated by easin ....Spacecraft Innovation Laboratory. The Australian Spacecraft Innovation Laboratory is designed to provide researchers and entrepreneurs with a venue to integrate and test their “cubesats”, satellites the size of a loaf of bread, and small payloads. By centralising the satellite integration function, the standard of Australian space assets can be assured, giving researchers confidence that their spacebased experiments will succeed. Knowledge transfer to space start-ups will be accelerated by easing their access to space.
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Discovery Early Career Researcher Award - Grant ID: DE230100473
Funder
Australian Research Council
Funding Amount
$410,154.00
Summary
Effective integration of human and automated analyses for security testing. This DECRA project aims to significantly improve the performance of current state-of-the-art automated security testing approaches, enabling them to discover more security bugs in strict time constraints. The key innovation of the project is its novel way to embrace human element to leverage the ingenuity of the developers. This project will help companies improve the security and reliability of their products, thwarting ....Effective integration of human and automated analyses for security testing. This DECRA project aims to significantly improve the performance of current state-of-the-art automated security testing approaches, enabling them to discover more security bugs in strict time constraints. The key innovation of the project is its novel way to embrace human element to leverage the ingenuity of the developers. This project will help companies improve the security and reliability of their products, thwarting cyberattacks that cost Australian business $29 billion each year. The knowledge from this project will be transferred and integrated into higher education subjects to train the next generations of software developers, who are responsible to build security-critical systems that we all rely on now and in the future.Read moreRead less
Learning Software Security Analysers with Imperfect Data. This project aims to systematically investigate next-generation learning-based software security analysis to detect vulnerabilities in real-world large-scale software. The expected learning-based foundation will support the handling of imperfect data in order to provide a precise, scalable and adaptive security analysis of the critical software components, thus capturing important security vulnerabilities missed by existing approaches. Th ....Learning Software Security Analysers with Imperfect Data. This project aims to systematically investigate next-generation learning-based software security analysis to detect vulnerabilities in real-world large-scale software. The expected learning-based foundation will support the handling of imperfect data in order to provide a precise, scalable and adaptive security analysis of the critical software components, thus capturing important security vulnerabilities missed by existing approaches. The success of this project will further enhance the international competitiveness of Australian research in this important field and will benefit any Australian industry and business where software systems are deeply-rooted, such as transportation, smart homes, medical devices, defence and finance.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
Discovery Early Career Researcher Award - Grant ID: DE190100849
Funder
Australian Research Council
Funding Amount
$364,000.00
Summary
Advanced thermal protection systems to enable Mars return missions. This project aims to advance the modelling of spacecraft heat shield performance to enable future returns to Earth from Mars, where vehicles will encounter heating loads an order of magnitude higher than Lunar returns. Survival depends on sacrificial heat shields which intentionally lose mass through ablation to form a protective layer. Currently, this process cannot be predicted accurately leading to compromised safety, excessi ....Advanced thermal protection systems to enable Mars return missions. This project aims to advance the modelling of spacecraft heat shield performance to enable future returns to Earth from Mars, where vehicles will encounter heating loads an order of magnitude higher than Lunar returns. Survival depends on sacrificial heat shields which intentionally lose mass through ablation to form a protective layer. Currently, this process cannot be predicted accurately leading to compromised safety, excessive weight, and increased mission cost. The expected outcome is an ablation model for vehicle design which, for the first time, is based on experiments with a realistic aerodynamic flow. The significance and benefit of this project is its potential to make ambitious missions such as a Mars return feasible.Read moreRead less