Research Article
High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database
Table 10
Stagnation Point TPS Recession thickness and in-depth thermal response comparison.
| | Material | Thickness type | Trajectory type | Methodology | | CMA | Sparta approximate | % difference |
| | PICA | Recession | Lunar return (11 kms) | 0.731 | 0.759 | 3.830 | | Lunar return (14 kms) | 3.823 | 1.19 | — | | Without recession | Lunar return (11 kms) | 7.608 | 7.747 | 1.827 | | Lunar return (14 kms) | 7.125 | 7.623 | 6.989 | | Total | Lunar return (11 kms) | 8.104 | 8.243 | 1.715 | | Lunar return (14 kms) | 10.675 | 9.14 | — |
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