1. Multi-scale thermal response modeling of an AVCOAT-like thermal protection material
2. BartlettE.KendallR.MoyerC.RindalR. “An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part 1 Summary Report,” NASA CR-1060, 1968.
3. MoyerC. B.RindalR. A. “An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator. Part 2-Finite Difference Solution for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances,” NASA CR-1061, 1968.
4. ChanC. “Modifications to the Aerotherm Charring Material Thermal Response and Ablation Program (CMA) for Carbon Ablation Analysis,” Applied Physics Lab. ADA-A211069, Johns Hopkins Univ., Laurel, MD, 1989.
5. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis