DOI QR코드

DOI QR Code

Quantitative Analysis for Surface Recession of Ablative Materials Using High-speed Camera and 3D Profilometer

초고속 카메라와 삼차원 표면 측정기를 이용한 삭마 재료의 정량적 표면 침식 분석

  • Choi, Hwa Yeong (Department of Aerospace Engineering, Chonbuk National University) ;
  • Roh, Kyung Uk (Department of Aerospace Engineering, Chonbuk National University) ;
  • Cheon, Jae Hee (Department of Aerospace Engineering, Chonbuk National University) ;
  • Shin, Eui Sup (Department of Aerospace Engineering, Chonbuk National University)
  • Received : 2018.06.12
  • Accepted : 2018.08.27
  • Published : 2018.09.01

Abstract

In this paper, the surface recession of ablative materials was quantitatively analyzed using a high-speed camera and a three-dimensional profilometer. The ablation tests of the graphite and carbon/phenolic composite samples were performed using a 0.4 MW arc-heated wind tunnel for simulating the atmospheric re-entry environment. The real-time images during the ablation test were captured by the high-speed camera, and analyzed to calculate the surface recession and recession rate. Also, the surface data of samples were obtained using a three-dimensional profilometer, and the surface recession was precisely calculated from the difference of height between the surface data before and after the test. It is effective to complement the two measurement results in the comprehensive analysis of surface recession phenomena.

본 논문에서는 초고속 카메라와 삼차원 표면 측정기를 이용하여 삭마 재료의 표면 침식량을 정량적으로 분석하였다. 대기권 재진입 환경을 모사하기 위해 0.4 MW 아크 가열 풍동을 이용하여 흑연과 탄소/페놀릭 복합재료의 삭마 실험을 수행하였다. 초고속 카메라를 이용하여 실시간 삭마 실험 영상을 획득하고, 이를 분석하여 침식량과 침식률을 산출하였다. 또한, 삼차원 표면 측정기를 이용하여 삭마 전후 시편의 표면 형상을 측정하였으며, 시편의 높이 차이로부터 침식량 분포를 정밀하게 산출하였다. 이를 통해 표면 침식 현상을 종합 분석하는데 있어서 두 측정 결과를 상호 보완하는 것이 유효함을 확인하였다.

Keywords

References

  1. Splinter, S. C., Bey, K. S., and Gragg, J. G., "Comparative Measurements of Earth and Martian Entry Environments in the NASA Langley HYMETS Facility," 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Jan. 2011.
  2. Yun, N. G., Jung, B., and Cho, Y. J., "Ablative Composite Materials for Rocket propulsion System," Composites Research, Vol. 3, No. 2, 1990, pp. 57-64.
  3. Zahra, E., Farchad, Y., and Mir, A. M., "Thermal and Mechanical Properties of Phenolic-based Compodites Reinforced by Carbon Fibres and Multiwall Carbon Nanotubes," Composites Part A: Applied Science and Manufacturing, Vol. 72, 2015, pp. 22-31. https://doi.org/10.1016/j.compositesa.2015.01.015
  4. David, M. D., Michael, W. O., Michael, D. B., and Matthew, M., "Understanding High Recession Rates of Carbon Ablators Seen in Shear Tests in an Arc Jet," 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Aerospace Sciences Meeting, AIAA Paper 2010-1177, Orlando, Florida, USA, 2010.
  5. Albert, T., Carl, F., Michael, R., and Joseph, R., "Development of a closed pore insulation material," NASA Contractor Report 2254, Washington, DC, 1973
  6. Stefan, L., and Thomas, R., "Experimental Investigation of Photogrammetric Surface Analysis of Heat Shield Materials during Plasma Wind Tunnel Testing," 7th European Workshop on Thermal Protection Systems and Hot Structures, Noordwijk, the Netherlands, 2013.
  7. Helber, B., Asma, C., Babou, Y., Magin, T., and Chazot, O., "Experimental Investigation of the Material Response of Carbon Composite Ablators in the VKI Plasmatron Facility," 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2011.
  8. Kim, N. J., Oh, P. Y., and Shin, E. S., "A Study on Surface Properties of Ablative Materials from 0.4MW Arc-heated Wind Tunnel Test," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 43, No. 12, 2015, pp. 1048-1053. https://doi.org/10.5139/JKSAS.2015.43.12.1048