The X2 expansion tube facility at The University of Queensland is capable of simulating entry into most of the planetary bodies in our solar system, producing test conditions with stagnation enthalpies in excess of 100 MJ/kg. Models used in X2 are typically made from steel and, consequently, manufacture is often constrained to conventional methods, with associated long lead times, and high cost. Through an experimental campaign, the survivability and applicability of Rapid Prototype models was investigated. Three prototyping methods were investigated; Selective Laser Sintering, Stereolithography, and Fused Deposition Modelling, and these were compared to a steel baseline. A computational stress analysis was used to design an internally holl...
Initial studies of the aerodynamic characteristics of proposed launch vehicles can be made more acc...
We describe the X-series impulse facilities at The University of Queensland and show that they can p...
The Hayabusa sample return capsule is scheduled for re-entry near Woomera, Australia in June 2010 an...
Hypersonic testing in impulse facilities replicates various flow characteristics accurately; however...
Future space missions, such as return from Mars, will require entry speeds of the order of 15 km/s. ...
Due to the high cost and danger associated with both manned and unmanned flight testing, a large por...
The design of hypersonic flight systems requires extensive ground testing to understand the flow cha...
Numerical simulations have been performed to study radiative and ablative processes experienced by a...
Future space missions, such as return from Mars, will require entry speeds of the order of 15 km∕s. ...
This paper represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of...
We describe the X-series impulse facilities at The Univer-sity of Queensland and show that they can ...
There is a need to determine the equations of state of materials in regimes of extreme high pressure...
Hypervelocity aerothermodynamic processes which occur during atmospheric re-entry scenarios, are ver...
Thermal protection is required for vehicles entering planetary atmospheres to protect against the se...
A shock-expansion tube/tunnel is a ground-based test facility to generate hypervelocity test flows f...
Initial studies of the aerodynamic characteristics of proposed launch vehicles can be made more acc...
We describe the X-series impulse facilities at The University of Queensland and show that they can p...
The Hayabusa sample return capsule is scheduled for re-entry near Woomera, Australia in June 2010 an...
Hypersonic testing in impulse facilities replicates various flow characteristics accurately; however...
Future space missions, such as return from Mars, will require entry speeds of the order of 15 km/s. ...
Due to the high cost and danger associated with both manned and unmanned flight testing, a large por...
The design of hypersonic flight systems requires extensive ground testing to understand the flow cha...
Numerical simulations have been performed to study radiative and ablative processes experienced by a...
Future space missions, such as return from Mars, will require entry speeds of the order of 15 km∕s. ...
This paper represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of...
We describe the X-series impulse facilities at The Univer-sity of Queensland and show that they can ...
There is a need to determine the equations of state of materials in regimes of extreme high pressure...
Hypervelocity aerothermodynamic processes which occur during atmospheric re-entry scenarios, are ver...
Thermal protection is required for vehicles entering planetary atmospheres to protect against the se...
A shock-expansion tube/tunnel is a ground-based test facility to generate hypervelocity test flows f...
Initial studies of the aerodynamic characteristics of proposed launch vehicles can be made more acc...
We describe the X-series impulse facilities at The University of Queensland and show that they can p...
The Hayabusa sample return capsule is scheduled for re-entry near Woomera, Australia in June 2010 an...