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Australian State/Territory : QLD
Research Topic : complex study design
Socio-Economic Objective : Space transport
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  • Funded Activity

    Linkage Projects - Grant ID: LP0215943

    Funder
    Australian Research Council
    Funding Amount
    $146,000.00
    Summary
    Development of large scale expansion tubes. The aim of this proposal is to develop a high Mach number scramjet simulation capability by modifying the X3 superorbital expansion tube at UQ for high suborbital operation at very high total pressures. This will enable Australia to do true Mach number simulation at higher speeds than is possible anywhere else, and mantain an international advantage in the development of scramjet flight propulsion. It will also put Australian researchers in a strong p .... Development of large scale expansion tubes. The aim of this proposal is to develop a high Mach number scramjet simulation capability by modifying the X3 superorbital expansion tube at UQ for high suborbital operation at very high total pressures. This will enable Australia to do true Mach number simulation at higher speeds than is possible anywhere else, and mantain an international advantage in the development of scramjet flight propulsion. It will also put Australian researchers in a strong position to participate in the next generation of US ground testing facilities, foreshadowed by the recent NASA purchase of a large shock tunnel driver. It will enable Australia to maintain a position of leadership in the development of new space travel concepts.
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    Funded Activity

    Discovery Projects - Grant ID: DP0208744

    Funder
    Australian Research Council
    Funding Amount
    $284,000.00
    Summary
    Minimizing hypersonic skin-friction by boundary-layer combustion. The high drag associated with hypersonic flight has been a major obstacle to development of hypersonic aircraft. It is generally accepted that half the drag of hypersonic vehicles will be caused by air friction on the aircraft's skin, due mainly to the turbulent boundary layer which forms on the skin. However, a new method of reducing skin friction, by injecting and burning fuel in the boundary layer, has been discovered. This .... Minimizing hypersonic skin-friction by boundary-layer combustion. The high drag associated with hypersonic flight has been a major obstacle to development of hypersonic aircraft. It is generally accepted that half the drag of hypersonic vehicles will be caused by air friction on the aircraft's skin, due mainly to the turbulent boundary layer which forms on the skin. However, a new method of reducing skin friction, by injecting and burning fuel in the boundary layer, has been discovered. This project is aimed at investigating the range of conditions under which this method will be effective. By this boundary-layer "lubrication" much more efficient hypersonic flight will be possible.
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    Funded Activity

    Discovery Projects - Grant ID: DP0665016

    Funder
    Australian Research Council
    Funding Amount
    $260,000.00
    Summary
    Enhancing scramjet performance by boundary layer combustion. Australia has developed a strong international reputation over the past 20 years for excellence in research into hypersonic flight technologies. This helps to reinforce the fact that this is a country in which advanced technologies can be conceived and developed. Australian companies and agencies are already collaborating with and are being supported by international organizations to develop further hypersonic flight technologies. Achi .... Enhancing scramjet performance by boundary layer combustion. Australia has developed a strong international reputation over the past 20 years for excellence in research into hypersonic flight technologies. This helps to reinforce the fact that this is a country in which advanced technologies can be conceived and developed. Australian companies and agencies are already collaborating with and are being supported by international organizations to develop further hypersonic flight technologies. Achieving another significant advance in this area by demonstrating significant reductions in frictional drag on hypersonic vehicles will keep us at the forefront of this field and lead to continued international support and collaboration.
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    Funded Activity

    Discovery Projects - Grant ID: DP0773371

    Funder
    Australian Research Council
    Funding Amount
    $490,000.00
    Summary
    Radiating hypersonic flows. Benefits will accrue through the involvement of Australia in the international program for future space missions. Through this project, Australia, already among the leaders in scramjet propulsion development, can also become a major player in spacecraft design. Significant educational benefits will be created due to the challenging nature of the work, through immediate contact with leading overseas researchers, and through subsequent marketing of flight vehicles. The .... Radiating hypersonic flows. Benefits will accrue through the involvement of Australia in the international program for future space missions. Through this project, Australia, already among the leaders in scramjet propulsion development, can also become a major player in spacecraft design. Significant educational benefits will be created due to the challenging nature of the work, through immediate contact with leading overseas researchers, and through subsequent marketing of flight vehicles. The project could lead to the involvement of Australian technology at a commercial level in a new generation of hardware for space exploration.
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    Funded Activity

    Discovery Projects - Grant ID: DP1094560

    Funder
    Australian Research Council
    Funding Amount
    $490,000.00
    Summary
    Hypervelocity re-entry. Addressing a critical area of space travel and its practical utilisation it will help expand a key technology niche which will facilitate our involvement in major programs of the future. In international space programs each participant provides a unique technical contribution and shares in the intellectual and economic returns. Educational benefits arise due to the challenging nature of the work, contact with overseas researchers, and through the marketing and developm .... Hypervelocity re-entry. Addressing a critical area of space travel and its practical utilisation it will help expand a key technology niche which will facilitate our involvement in major programs of the future. In international space programs each participant provides a unique technical contribution and shares in the intellectual and economic returns. Educational benefits arise due to the challenging nature of the work, contact with overseas researchers, and through the marketing and development of flight vehicles and associated technology. There will be opportunity for our graduates to be employed in senior positions overseas, and to subsequently return to Australia with advanced skills and facilitate Australian collaboration from positions of influence.
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