Discovery Projects - Grant ID: DP120102663

Funding Activity

Website
https://dataportal.arc.gov.au/NCGP/Web/Grant/Grant/DP120102663

Funding Status
Closed

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Funded Activity Summary

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.

Funded Activity Details

Start Date: 01-01-2012

End Date: 30-04-2015

Funding Scheme: Discovery Projects

Funding Amount: $540,000.00

Funder: Australian Research Council

Research Topics

ANZSRC Field of Research (FoR)

Aerospace Materials | Aerospace Engineering | Hypersonic Propulsion and Hypersonic Aerodynamics | Satellite, Space Vehicle and Missile Design and Testing

ANZSRC Socio-Economic Objective (SEO)

Space Transport |

Other Keywords

Aerospace Engineering | Aerospace Materials | Hypersonic Propulsion and Hypersonic Aerodynamics | Satellite, Space Vehicle and Missile Design and Testing | Space Transport

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