Browse > Article
http://dx.doi.org/10.5139/JKSAS.2021.49.5.355

Evaluation of Heat Resistance of Lyocell-based Carbon/Phenolic for Aerospace  

Seo, Sang-Kyu (Agency for Defense Development)
Kim, Yun-Chul (Agency for Defense Development)
Bae, Ji-Yeul (Agency for Defense Development)
Hahm, Hee-Chul (Agency for Defense Development)
Hwang, Tae-Kyung (Agency for Defense Development)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.49, no.5, 2021 , pp. 355-363 More about this Journal
Abstract
Heat resistance performance evaluation and thermal analysis were performed to confirm the applicability of the lyocell-based carbon/phenolic composite material for heat-resistant parts for aerospace. Heat resistance performance evaluation of carbon/phenolic was conducted by Thermal Protection Evaluation Motor (TPEM). In this paper, boundary layer integration code considering the boundary layer analysis of combustion gas and MSC-Marc 2018 considering ablation and thermal pyrolysis were used for the thermal analysis. The ablation and thermal insulation performance were analyzed by the pressure curve of test motor and the cut carbon/phenolic specimens. The thermal response of the lyocell-based carbon/phenolic material was similar to that of the rayon-based carbon/phenolic material. Based on the results through the combustion test, the applicability of heat-resistant parts for aerospace to which domestic lyocell-based carbon fibers were applied was confirmed.
Keywords
Lyocell-based Carbon/Phenolic; Rayon-based Carbon/Phenolic; Thermal Protection Evaluation Motor; Chemical Ablation; Thermal Decomposition;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Shimada, T., Sekiguchi, M. and Sekino, N., "Flow inside a solid rocket motor with relation to nozzle inlet ablation," AIAA journal, Vol. 45, No. 6, 2007, pp. 1324-1332.   DOI
2 Shames, I. H., "Mechanics of fluids," 4th ed., McGraw-Hill, N.Y., U.S.A., 2003, Ch. 10.
3 Keswani, S. T. and Kuo, K. K., "An Aero-thermochemical Model of Carbon-Carbon Composite Nozzle Recession," In 24th Structures, Structural Dynamics and Materials Conference, p. 910.
4 Boyarintsev, V. I. and Zvyagin, Yu. V., "Turbulent Boundary Layer on Reacting Graphite Surface," Proceedings of the 5th International Heat Transfer Conference, September, 1974, pp. 264-268.
5 McBride, B. J. and Gordon, S., "Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications, II. Users Manual and Program Description," NASA RP-1311, 1996.
6 Vol, Marc., "A: Theory and User Information," MSC. Software Corporation, 2018, Ch. 6, pp. 247-314.
7 Seo, S. K., Ham, H. C. and Kang, Y. G., "Analysis of Boundary Layer in Solid Rocket Nozzle and Numerical Analysis of Thermal Response of Carbon/Phenolic using Finite Difference Method," Journal of the Korean Society of Propulsion Engineers, Vol. 22, No. 1, 2018, pp. 36-44.
8 Laturelle, F., Fiorot, S. and Wertheimer, T. B., "MSC.Marc-ATAS: Advanced Thermal Analysis Software for Modeling of Rocket Motors and Other Protection Systems," Worldwide Aerospace Conference and Technology Showcase, Toulouse, France, April 2002.
9 Jha, M. K., Kumar, V., Maharaj, L. and Singh, R. J., "Studies on leaching and recycling of zinc from rayon waste sludge," Industrial and engineering chemistry research, Vol. 43, No. 5, 2004, pp. 1284-1295.   DOI
10 Shabbir, M. and Mohammad, F., "Sustainable production of regenerated cellulosic fibres," In Sustainable Fibres and Textiles, Woodhead Publishing, 2017, pp. 171-189.
11 Jo, S. M., "Ecofriendly cellulose fibers," Fashion Information and Technology, Vol. 7, 2010, pp. 2-9.
12 Bahl, O. P., Shen, Z., Lavin, J. G. and Ross, R., "Manufacture of carbon fibers," Carbon Fibers, Third Edition, Marcel! Dekker, Inc, 270 Madison Avenue, New York, NY 10016, USA, 1998, pp. 1-83.
13 Gasch, M., Skokova, K., Stackpoole, M., Venkatapathy, E., Ellerby, D., Milos, F., Peterson, K., Prabhu, D., Gonzales, G., Violette, S. and Franklin, T., "Development of Domestic Lyocell Based Phenolic Impregnated Carbon Ablator (PICA-D) for Future NASA Missions," NASA Technical report ARC-E-DAA-TN69962, 2019.
14 Park, G. Y., Kim Y. S., Lee, S. O., Hwang, T. K., Kim, Y. C., Seo, S. K. and Chung, Y. S., "Study of the Crystal Structure of a Lyocell Precursor for Carbon Fibers," Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 5, 2019, pp. 36-42.   DOI
15 Lee, S. O., Park, G. Y., Kim, Y. S., Hwang, T. K., Kim, Y. C., Seo, S. K. and Chung, Y. S., "Effect of Cross-linking Treatment of Lyocell Fabric on Carbon Fabric Properties," Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 6, 2019, pp. 21-27.   DOI
16 Ham, H. C., "A Study on the Thermal Response Characteristics of Carbon/Carbon Composites for Nozzle Throat Insert," Journal of the Korean Society of Propulsion Engineers, Vol. 10, No. 1, 2006, pp. 30-37.
17 Seo, S. K., Ham, H. C. and Kang, Y. G, "Numerical Analysis for Thermal Response of Silica Phenolic in Solid Rocket Motor," Journal of the Korean Society of Propulsion Engineers, Vol. 22, No. 4, 2006, pp. 76-84.   DOI
18 Bartz, D. R., "Turbulent boundary-layer heat transfer from rapidly accelerating flow of rocket combustion gases and of heated air," Advances in Heat Transfer, Vol. 2, 1965, pp. 1-108.   DOI
19 Bae, J. Y., Bae, H. M., Ryu, J., Ham, H. and Cho, H. H., "Heat Transfer on Supersonic Nozzle using Combined Boundary Layer Integral Method," Journal of the Computational Structural Engineering Institute of Korea, Vol. 30, No. 1, 2017, pp. 47-53.   DOI