Modelling of carbon–carbon composite ablation in rocket nozzles

Author:

Vignoles G.L.,Aspa Y.,Quintard M.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference48 articles.

1. Borie V, Brulard J, Lengellé G. An aerothermochemical analysis of carbon–carbon nozzle regression in solid-propellant rocket motors. In: 24th Joint propulsion conference, AIAA/ASME/SAE/ASEE, Boston, MA; 1988.

2. Carbon/carbon composites;Savage,1993

3. Carbon reinforcements and C/C composites;Manocha,1998

4. A comprehensive theoretical model for carbon–carbon composite nozzle recession;Kuo;Combust Sci Technol,1986

5. Vignoles G, Aspa Y, Lachaud J. Roughness evolution in ablation of carbon-based materials: multi-scale modelling and material analysis. In: Fletcher K, editor. 5th European workshop on thermal protection systems and hot structures. ESA confs. procs., vol. SP-631. ESA-ESTEC, ESA, Noordwijk,The Netherlands; 2006.

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