1. Transient ablation regime in circuit breakers;Martin;Plasma Sci. Technol.,2007
2. Ablative materials for high-temperature thermal protection of space vehicles;Bowman;J. Chem. Educ.,1971
3. Strongly coupled computation of material response and nonequilibrium flow for hypersonic ablation;Martin;J. Spacecraft Rock.,2015
4. H.K. Tran, C.E. Johnson, D.J. Rasky, F.C.L. Hui, M.T. Hsu, T. Chen, Y.-K. Chen, D. Paragas, L. Kobayashi, Phenolic Impregnated Carbon Ablators (Pica) as Thermal Protection Systems for Discovery Missions, Technical Report NASA-TM-110440, NASA Ames Research Center, Moffett Field, CA, April 1997. .
5. Calculation of stagnation-point heating rates associated with stardust vehicle;Park;J. Spacecraft Rock.,2005