Research Article
High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database
Table 5
Benchmarking analysis for
Apollo 6 at an entry angle of
.
| | Codes | Velocity at peak heating (km/s) | Altitude at peak heating (km) | Maximum deceleration (g’s) | Mach number |
| | POST | 8.45 | 24.01 | 12.15 | 26.40 | | TrajOpt | 7.98 | 23.00 | 11.16 | 24.93 | | Sparta | 8.32 | 23.16 | 11.96 | 26.00 |
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