“…A value of 4 kcal represents over 16 700 J, whereas the heat insulation during re-entry would vary from 12 GJ to 340 GJ. Considering the Apollo space capsule, which had a mass of 12 200 lb, which is approximately 5500 kg and the total energy was reported to be 340 GJ (both potential and kinetic energies of 5500 kg), which is 62 kJ g –1 and, in contrast to the chemical heat of 16.7 kJ g –1 , as we previously mentioned, is ∼27% of the former energy value (62 kJ g –1 ), absorbing 27% of aerodynamic heat and conserving it in product form of a chemical reaction is quite a significant phenomenon; however, the much more modern ablative systems, which include ultrahigh temperature ceramics such as zirconium ceramics have reported that, upon the onset of oxidation of zirconium ceramics, which certainly leads to the formation of zirconia, much of the heat was consumed by zirconia for phase transformation and dilation , with the magnitude of heat sunk into the material albeit not been recorded. But few of the modern research groups (viz., Badhe et al , ) have doped resorcinol formaldehyde with carbon soot obtained from the controlled combustion of camphor, which could be a suitable matrix modifier for the requirements of moderate char yield of 59% after pyrolysis at 800 °C with an interesting ablation rates of 0.019 mm/s and 0.053 g/s, Badhe et al, had developed a novel idea by modifying resorcinol formaldehyde, a superorganic chain, with recycled waste rubber, and have reported that the degradation temperature was enhanced by 13% and mass ablation rates by 11%.…”