Thermomechanical response of out-of-autoclave infused carbon-phenolic laminates for rocket engine applications subjected to surface ablation

Author:

Caporale Antonio Maria,Airoldi Alessandro,Natali Maurizio,Boiocchi Matteo,Torre Luigi,Rallini Marco

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference42 articles.

1. Mechanical Properties with High Temperature and the Microstructure of Carbon/Phenolic Ablative Composites;Wang;J Wuhan Univ Technol-Mater,2012

2. Satyanarayana Gupta M, Ekta J. Review on Evaluation of properties of carbon phenolic composite structure using gas chromatography for analysis of thermal performance. In: IOP Conference Series: Materials Science and Engineering, Telangana, India; 2018.

3. Arnold SM, Murthy PL, Bednarcyk BA, Lawson JW, Monk JD, Bauschlicher CWJ. Multiscale Modeling of Carbon/Phenolic Composite Thermal Protection Materials: Atomistic to Effective Properties. NASA, NASA Glenn Research Center Cleveland, OH United States; 2016.

4. Science and technology of polymeric ablative materials for thermal protection systems and propulsion devices: a review;Natali;Progr Mater Sci,2016

5. High Temperature Thermochemical Behavior of Carbon-Phenolic and Carbon-Carbon Composites, I. Analysis;Mcmanus;J Compos Mater,1992

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