Original Article
  • Evaluation of Permeability Performance by Cryogenic Thermal Shock in Composite Propellant Tank for Space Launch Vehicles

  • Jung-Myung Kim*, Seung-Chul Hong*, Soo-Young Choi*†, Sang-Won Jeong*, Hyon-Su Ahn**

  • * ANH Structure ANH Design Center
    ** ANH Structure

  • 우주 발사체용 복합재 산화제 탱크 구조물의 극저온 열충격에 따른 투과도 성능 평가

  • 김정명* · 홍승철* · 최수영*† · 정상원* · 안현수**

References
  • 1. SPACEX FALCON HEAVY Capabilities & Services, https://www.spacex.com/about/capabilities, [Accessed 16/09/2019].
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  • 2. Shimoda, T., Morino, Y., Ishikawa, T., Morimoto, T., and Cantoni, S., “Study of CFRP Application to Cryogenic Fuel Tank for RLV,” Proceeding of the Japan International SAMPE Symposium, Vol. 7, 2001, pp. 275-278.
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  • 3. Kang, S.K., Kim, M.G., and Kim, C.G., “Evaluation of Cryogenic Performance of Adhesives Using Composite-Aluminum Double Lap Joints,” Composite Structures, Vol. 78, No. 3, 2007, pp. 440-446.
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  • 4. Kang, S.G., Kim, M.G., Kim, C.G., and Kong, C.W., “Effects of Curing Temperature and Autofrettage Pressure on a Type 3 Cryo-genic Propellant Tank,” Composites Research, Vol. 19, No. 4, 2006, pp. 31-38.
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  • 5. Flanagan, M., Grogan, D.M., Goggins, J., Appel, S., Doyle, K., Leen, S.B., and Ó Brádaigh, C.M., “Permeability of Carbon Fibre PEEK Composites for Cryogenic Storage Tanks of Future Space Launchers,” Composites Part A: Applied Science and Manufacturing, Vol. 101, 2017, pp. 173-184.
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  • 6. Choi, S.J., and Sankar, B.V., “Gas Permeability of Various Graphite/Epoxy Composite Laminates for Cryogenic Storage Systems,” Composites Part B: Engineering, Vol. 39, No. 5, 2008, pp. 782-791.
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  • 7. Yokozeki, T., Ogasawara, T., Aoki, T., and Ishikawa, T., “Experimental Evaluation of Gas Permeability through Damaged Compo-site Laminates for Cryogenic Tank,” Composite Science and Technology, Vol. 69, No. 9, 2009, pp. 1334-1340.
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  • 8. Grenoble, R.W., and Gates, T.S., “Hydrogen Permeability of Polymer Matrix Composites at Cryogenic Temperatures,” Proceeding of 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan. 2005, AIAA, pp. 2005-2086.
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  • 9. Jackson, J.R., Vivkers, J., and Fikes, J., “Composite Cryotank Technologies and Development 2.4 and 5.5M out of Autoclave Tank Test Results,” Proceeding of Composites and Advanced Materials Expo, Oct. 2015, M15-4801.
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  • 10. Johnson, T., Sleight, D.W., and Martin, R.A., “Structures and Design Phase I Summary for the NASA Composite Cryotank Tech-nology Demonstration Project,” Proceedingsof the 54th AIAA/ASME/ASCE/AHS/ASC, Structures, Structural Dynamics, and Mate-rials Conference, Apr. 2013, Document ID. 20130013009.
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  • 11. Cho, K.J., Jung, Y.S., Cho, I.H., Kim, Y.W., and Lee, D.S., “The Heat and Flow Analysis of the Liquid Helium for the Pressurization of Liquid Rocket Propellant Tank,” Journal of the Korean Society of Propulsion Engineers, Vol. 7, No. 1, 2003, pp. 10-17.
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This Article

Correspondence to

  • Soo-Young Choi

  • ANH Structure ANH Design Center

  • E-mail: sychoi@anhstructure.com