Processing of thermo-structural carbon-fiber reinforced carbon composites

Journal Of Aerospace Technology And Management

Endereço:
Pr Mal Eduardo Gomes, 50
São José dos Campos / SP
Site: http://www.jatm.com.br
Telefone: (12) 3947-5115
ISSN: 19849468
Editor Chefe: Francisco Cristóvão Lourenço de Melo
Início Publicação: 31/05/2009
Periodicidade: Quadrimestral
Área de Estudo: Engenharia aeroespacial

Processing of thermo-structural carbon-fiber reinforced carbon composites

Ano: 2009 | Volume: 1 | Número: 2
Autores: Luiz Cláudio Pardini, Adriano Gonçalves
Autor Correspondente: Luiz Cláudio Pardini | [email protected]

Palavras-chave: carbon-carbon composites, processing, carbon fibers, pyrolysis, rocket nozzle throat

Resumos Cadastrados

Resumo Inglês:

The present work describes the processes used to obtain thermostructural Carbon/Carbon composites. The processing of these materials begins with the definition of the architecture of the carbon fiber reinforcement, in the form of stacked plies or in the form of fabrics or multidirectional reinforcement. Incorporating fiber reinforcement into the carbon matrix, by filling the voids and interstices, leads to the densification of the material and a continuous increase in density. There are two principal processing routes for obtaining these materials: liquid phase processing and gas phase processing. In both cases, thermal processes lead to the formation of a carbon matrix with specific properties related to their precursor. These processes also differ in terms of yield. With liquid phase impregnation the yield is around 45 per cent, while gas phase processing yields around 15 per cent.