黄片看片神器

Title: Dispersion of spacecraft components during re-entry 
Leader:  
Project Team: | | Flynn Hack | Gerard Armstrong 
Project Partners:  
Funding Body: Australian Research Council

Hypersonic wind tunnel experiments and computational simulations will be performed to enhance our understanding of how spacecraft components are dispersed during re-entry.  Through this new knowledge, Australia will be positioned to meaningfully engage in the global management of destructive re-entries of spacecraft to achieve outcomes that respect our sovereign interests.

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Title: Novel Testing of a Supersonic Airbreathing Rotating Detonation Engine 
Leader:  
Project Team: Maciej Grybko 
Funding Body: Australian Research Council
 
Rotating detonation engines have the potential provide improved performance when compared to regular combustion engines. Although commonly demonstrated in a rocket configuration, this project is investigating the next stage of developed by looking at an airbreathing RDE for testing in the 黄片看片神器 TUSQ facility.

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Title: Fluid-thermal-structural interactions on high-speed aerospace vehicles 
Leader:  
Project Partners: UNSW (https://www.unsw.edu.au/) 
Funding Body: Australian Research Council  

Robust and efficient designs for light-weight hypersonic vehicles must address the problem of aerodynamic heating and its effect on structural performance. This project will design and perform first-of-kind experiments that reproduce the complex fluid-thermal-structural interactions representative of those experienced by these aircraft and rockets.

Title: Australian Airborne Observation of the Hayabusa2 Re-Entry Capsule
Leader:
Project Team: | | | Lachlan Noller
Project Partners: RTI
Funding Body: RTI

This mission demonstrated the rapid response capability of the UniSQ and RTI relationship to undertake airborne observation missions of aerospace phenomena. The mission was planned and executed in 8 days. Detailed spectral measurements of the Hayabusa2 capsule were taken and analysed resulting in knowledge of the capsules surface temperature and the radiating gas in the shock layer.

Title: Airborne Observation of the Tau Herculids Meteor Shower
Leader:
Project Team:
Project Partners: RTI |  | | Funding Body: RTI

An airborne observation of the Tau-Herculids meteor shower was undertaken, flying from Forth Worth Texas. An international team led by UniSQ and RTI captured a range of imaging and spectroscopy measurements of the meteor shower. A significantly larger number of meteors were imaged from the aircraft than from the ground

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Title: Remote diagnostics for space-access flight testing
Leader:
Project Team:
Project Partners: RTI | DLR | Southern Launch | Hypersonix
Funding Body: Australian Research Council

Aerospace flight testing is essential for assessing the reliability of space-access technologies including re-usable rockets and hypersonic air-breathing systems. This project develops the essential optical diagnostic tools and techniques and establishes an enduring capability for space-access flight testing in Australia.

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Title: HORIS - Hypervelocity OSIRIS-REx Imaging and Spectroscopy
Leader: 
Project Team: | Gerard Armstrong | Flynn Hack | Dr Tamara Sopek | Sam Lock (UQ) | Nathan Lu (UQ) | Scott Gray (RTI) | Rick Pegus (Navair) | | | Stefan Loehle (HEFDiG) | | Ingo Jahn | Peter Jacobs | | Maciej Grybko | Simon Castles | Martin Eberhart (HEFDiG) | Felix Grigat (HEFDiG) | Toby van der Herik (UQ) | Benjamin Fernando (Johns Hopkins)
Project Partners: , ,
Funding Body: RTI | iLAuNCH

On September 24th 2023 the NASA capsule, OSIRIS-REx, returned from the asteroid Bennu safely bringing back dust samples. The 12km/s re-entry was observed by a team of over 50 scientists from around the world. UniSQ and RTI lead a team including personnel on a NASA aircraft, our own aircraft with instruments, and three ground stations. This daytime re-entry provided many imaging challenges, however, successful data was captured across a whole range of instruments. Data analysis is now on-going. 

Title: Expanding the scramjet operating envelope through oxygen enrichment  
Leader:  
Project Partners: |  
Funding Body: Australian Research Council  
 
The project aims to establish the benefits of oxygen enrichment for expanding the operating range of hydrogen-fuelled hypersonic air-breathing vehicles to higher altitudes and augmenting thrust at high speeds.

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Title: Co-design and dynamic mission optimisation of hypersonic flight vehicles   

Leader:  
Project Partners: |  
Funding Body: Australian Research Council  
 
This project will develop key competencies and tools for design and control of next-generation hypersonic vehicles and train the future workforce. We will develop fundamental insights into the contributing disciplines of control systems, optimisation and fluid dynamics and new methods to simultaneously optimise vehicle geometry, trajectory, and control system that remain computationally tractable.