Experimental investigation on thermochemical phenomena in SiFRP
Author:
Affiliation:
1. a IHI Aerospace Co., Ltd, Technologies Development Department , Fujiki 900, Tomioka-shi , Gunma , 370-2307 , Japan
2. b Japan Aerospace Exploration Agency , 2-1-1 Sengen, Tsukuba-shi , Ibaraki , 305-8505 , Japan
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
https://www.tandfonline.com/doi/pdf/10.1080/09243046.2012.743715
Reference8 articles.
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3. Hirai K. Numerical and experimental characterizations of the SiFRP ablator for the combustion chamber heat shields of liquid rocket engines. Trans. JSASS Space Tech. Japan. 2008;7:37–42.
4. Kinefuchi K, Kamita K, Hirai K. Study for validation of a liquid rocket engine ablative chamber (in Japanese). In: 49th Conference on Aerospace Propulsion and Power; 2009.
5. Ho DWK, Koo JH, Bruns MC, Ezekoye OA. A review of numerical and experimental characterization of thermal protection materials – Part III. Experimental testing. AIAA-2007-5773; 2007.
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