Effects of carbon nanotubes and carbon fiber reinforcements on thermal conductivity and ablation properties of carbon/phenolic composites

Author:

Park Joung-Man,Kwon Dong-Jun,Wang Zuo-Jia,Roh Jeong-U,Lee Woo-Il,Park Jong-Kyoo,Lawrence DeVries K.

Funder

Defense Acquisition Program Administration and the Agency for Defense Development

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference24 articles.

1. Ankush B, Subrata R, Ryan G. Pyrolysis gas flow in thermally ablating media using time-implicit discontinuous Galerkin methods. In: 49th American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting & Exhibit, Jan. 2011.

2. Ahn HK, Park C, Sawada K. Dynamics of pyrolysis gas in charring materials ablation. In: 36th Aerospace Sciences Meeting & Exhibit, Jan. 1998.

3. Response of heatshield material at stagnation point of pioneer-venus probes;Ahn;J Thermophys Heat Transfer,2002

4. Modelling of carbon–carbon composite ablation in rocket nozzles;Vignoles;Compos Sci Technol,2010

5. Effect of combustion gas mass flow rate on carbon/carbon composite nozzle ablation in a solid rocket motor;Peng;Carbon,2012

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