Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight
Paper
Choudhury, Rishabh and Neely, Andrew J.. 2012. "Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight." 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012). Tours, France 24 - 28 Sep 2012 United States. https://doi.org/10.2514/6.2012-5899
| Paper/Presentation Title | Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight |
|---|---|
| Presentation Type | Paper |
| Authors | Choudhury, Rishabh and Neely, Andrew J. |
| Journal or Proceedings Title | Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012) |
| Article Number | 2012-5899 |
| Number of Pages | 12 |
| Year | 2012 |
| Place of Publication | United States |
| ISBN | 9781600869310 |
| Digital Object Identifier (DOI) | https://doi.org/10.2514/6.2012-5899 |
| Web Address (URL) of Paper | https://arc.aiaa.org/doi/10.2514/6.2012-5899 |
| Conference/Event | 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012) |
| Event Details | 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012) Event Date 24 to end of 28 Sep 2012 Event Location Tours, France |
| Abstract | Post-flight recovery of USAF/DSTO's HIFiRE-0 mission indicated that the patches of permanent-change thermal paints applied on the aluminium instrumentation can of the vehicle had undergone visible colour change due to heating during the flight. Calibration of the same permanent change thermal paints have been performed at UNSW Canberra using an electric-arc based heating rig which reproduced surface temperature histories obtained from transient numerical conjugate-heat-transfer simulations to quantify the heating history of the painted region. The electric-arc based heating rig is able to replicate the transient heating histories encountered during hypersonic flight. Numerical simulations have been conducted to predict the temperature rise of the vehicle during it's flight which act as an input for the calibration system. The change in the colour of the interested paint due to in-flight heating has been compared and quantified using the CIELAB colour space. © 2012 by Rishabh Choudhury & Andrew J. Neely. |
| Public Notes | There are no files associated with this item. |
| Byline Affiliations | University of New South Wales |
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