1. Barbosa CAL (2004) Obtenção e caracterização de materiais ablativos a base de compósitos de fibra de carbono/resina fenólica. Instituto Tecnológico de Aeronáutica, São José dos Campos
2. Silva SFC, Machado HA, Bittencourt E (2015) Effect of the fiber orientation relatively to the plasma flow direction in the ablation process of a carbon-phenolic composite. J Aerosp Technol Manag. São José dos Campos, 7(1):43–52
3. Nguyen-Bui NTH, Duffa G, Dubroca B, Leroy B (2006) New methods for the simulation of ablative thermal protections. In: European workshop of thermal protection systems and hot structures, 5, Noordwijk
4. da Costa LEVL (2003) The composite option for solid rocket motor cases in Brazil. In: International Astronautical Congress of The International Astronautical Federation, The International Academy of Astronautics, And the International Institute of Space Law, 54, Bremen. Reston: AIAA.
5. Auweter-Kurtz M (2002) Plasma source development for the qualification of thermal protection materials for atmospheric entry vehicles at IRS, Vacuum, 65(3–4):247–261