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 TypePaper
AuthorsChoudhury, Rishabh and Neely, Andrew J.
Journal or Proceedings TitleProceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012)
Article Number2012-5899
Number of Pages12
Year2012
Place of PublicationUnited States
ISBN9781600869310
Digital Object Identifier (DOI)https://doi.org/10.2514/6.2012-5899
Web Address (URL) of Paperhttps://arc.aiaa.org/doi/10.2514/6.2012-5899
Conference/Event18th 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 AffiliationsUniversity of New South Wales
Library Services
Permalink -

https://research.usq.edu.au/item/wqvyz/calibration-of-thermal-paints-for-surface-temperature-measurement-of-hifire-0-flight

  • 25
    total views
  • 0
    total downloads
  • 1
    views this month
  • 0
    downloads this month

Export as

Related outputs

Hypersonic Pitching Control Model Development
Stern, Nathan, Buttsworth, David, Choudhury, Rishabh and Birch, Byrenn. 2018. "Hypersonic Pitching Control Model Development." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 Reston, United States. https://doi.org/10.2514/6.2018-5267
Pressure Fluctuations in a Hypersonic Ludwieg Tube with Free Piston Compression Heating
Birch, Byrenn J. C., Choudhury, Rishabh, Stern, Nathan and Buttsworth, David R.. 2018. "Pressure Fluctuations in a Hypersonic Ludwieg Tube with Free Piston Compression Heating." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 Reston, United States. https://doi.org/10.2514/6.2018-5266
Analysis of Reentry and Break-Up Forces from Impulse Facility Experiments and Numerical Rebuilding
Leiser, David, Loehle, Stefan, Zander, Fabian, Buttsworth, David R., Choudhury, Rishabh and Fasoulas, Stefanos. 2022. "Analysis of Reentry and Break-Up Forces from Impulse Facility Experiments and Numerical Rebuilding." Journal of Spacecraft and Rockets. 59 (4), pp. 1276-1288. https://doi.org/10.2514/1.A35204
Hypersonic oscillating shock-wave/boundary-layer interaction on a flat plate
Currao, Gaetano M. D., McQuellin, Liam P., Neely, Andrew J., Gai, Sudhir L., O'Byrne, Sean, Zander, Fabian, Buttsworth, David R., McNamara, Jack J. and Jahn, Ingo. 2021. "Hypersonic oscillating shock-wave/boundary-layer interaction on a flat plate." AIAA Journal: devoted to aerospace research and development. 59 (3), pp. 940-959. https://doi.org/10.2514/1.J059590
An Experimental and Numerical Investigation into the Aerodynamics of the ISS Re-entry
Zander, F., Leiser, D., Choudhury, R., Loehle, S. and Buttsworth, D.R.. 2018. "An Experimental and Numerical Investigation into the Aerodynamics of the ISS Re-entry." Lau, T.C.W. and Kelso, R.M. (ed.) 21st Australasian Fluid Mechanics Conference (AFMC 2018). Adelaide, Australia 10 - 13 Dec 2018 Australia.
Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 United States. https://doi.org/10.2514/6.2018-5252
Aerodynamic database of the HEXAFLY‑INT hypersonic glider
Schettino, Antonio, Pezzella, Giuseppe, Marini, Marco, Di Benedetto, Sara, Villace, Victor F., Steelant, Johan, Choudhury, Rishabh, Gubanov, Anatoly and Voevodenko, Nina. 2020. "Aerodynamic database of the HEXAFLY‑INT hypersonic glider." CEAS Space Journal. 12 (2), pp. 295-311. https://doi.org/10.1007/s12567-020-00299-4
Measurement of water vapour in axisymmetric jet development using TDLAS
Al-Manea, A., Buttsworth, D., Leis, J., Choudhury, R. and Saleh, K.. 2018. "Measurement of water vapour in axisymmetric jet development using TDLAS." Lau, T. C. W. and Kelso, R. M. (ed.) 21st Australasian Fluid Mechanics Conference (AFMC 2018). Adelaide, Australia 10 - 13 Dec 2018 Australia.
Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames." Combustion and Flame. 197, pp. 369-377. https://doi.org/10.1016/j.combustflame.2018.08.019
Spacecraft Material Tests under Aerothermal and Mechanical Reentry Loads
Leiser, David, Lohle, Stefan, Zander, Fabian, Fasoulas, Stefanos, Buttsworth, David R. and Choudhury, Rishabh. 2019. "Spacecraft Material Tests under Aerothermal and Mechanical Reentry Loads." AIAA SciTech Forum 2019 . San Diego, United States 07 - 11 Jan 2019 United States. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0161
Study of an axisymmetric backward facing step model in a supersonic flow
Zhao, Mengmeng, Buttsworth, David R., Choudhury, Rishabh, Malpress, Ray and Xing, Fei. 2016. "Study of an axisymmetric backward facing step model in a supersonic flow." 21st AIAA International Space Planes and Hypersonics Technologies Conference (Hypersonics 2017). Xiamen, China 06 - 09 Mar 2017 United States. https://doi.org/10.2514/6.2017-2181
Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model
Zhao, M. M., Choudhury, R., Malpress, R. and Buttsworth, D. R.. 2016. "Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model." 20th Australasian Fluid Mechanics Conference (AFMC 2016). Perth, Australia 05 - 08 Dec 2016 Australia.
Hypersonic wind-tunnel free-flying experiments with onboard instrumentation
Mudford, Neil R., O'Byrne, Sean, Neely, Andrew, Buttsworth, David and Balage, Sudantha. 2015. "Hypersonic wind-tunnel free-flying experiments with onboard instrumentation." Journal of Spacecraft and Rockets. 52 (1), pp. 231-242. https://doi.org/10.2514/1.A32887
A new method for prescribing non-uniform wall temperatures on wind tunnel models
Neely, A. J., Dasgupta, A. and Choudhury, R.. 2014. "A new method for prescribing non-uniform wall temperatures on wind tunnel models." 19th Australasian Fluid Mechanics Conference (AFMC 2014). Melbourne, Australia 08 - 11 Dec 2014 Australia.
Thermal-structural modelling of TDLAS system for SCRAMSPACE hypersonic flight test
Dasgupta, Arnab, Choudhury, Rishabh, Neely, Andrew, O'Byrne, Sean and Kurtz, Joe. 2012. "Thermal-structural modelling of TDLAS system for SCRAMSPACE hypersonic flight test." 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012). Tours, France 24 - 28 Sep 2012 United States.
Super-orbital re-entry in Australia: laboratory measurement, simulation and flight observation [Keynote lecture]
Buttsworth, David, Jacobs, Peter, Potter, Daniel, Mudford, Neil, D'Souza, Mary, Eichmann, Troy, Jenniskens, Peter, McIntyre, Tim, Jokic, Michael, Jacobs, Carolyn, Upcroft, Ben, Khan, Razmi, Porat, Hadas, Neely, Andrew and Lohle, Stefan. 2012. "Super-orbital re-entry in Australia: laboratory measurement, simulation and flight observation [Keynote lecture]." Kontis, Konstantinos (ed.) 28th International Symposium on Shock Waves (ISSW 28). Manchester, United Kingdom 17 - 22 Jul 2011 Heidelberg, Germany. https://doi.org/10.1007/978-3-642-25688-2_5
Measurement of Aerothermal Heating on HIFiRE-0
Neely, Andrew J., Choudhury, Rishabh, Paukner, Daniel and Odam, Judy. 2011. "Measurement of Aerothermal Heating on HIFiRE-0." 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (2011). United States 11 - 14 Apr 2011 United States. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2356
Hypersonic Drop-Tests of a Sphere: CFD Comparison to Experimental Results
Choudhury, R., Doig, G., Neely, A. and Barber, T.. 2010. "Hypersonic Drop-Tests of a Sphere: CFD Comparison to Experimental Results." 17th Australasian Fluid Mechanics Conference (AFMC 2010). Auckland, New Zealand 05 - 09 Dec 2010 New Zealand. pp. 465-468