Research Article
High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database
Table 6
Benchmarking analysis for mars pathfinder probe at a relative entry angle of
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| | Codes | Velocity at peak heating (km/s) | Altitude at peak heating (km) | Maximum deceleration (g’s) | Convective heat flux (W/) |
| | POST | 6.5 | 41.5 | 16.50 | 101.13 | | TrajOpt | 6.7 | 39.5 | 17.80 | 119.79 | | Sparta | 6.5 | 41.0 | 16.26 | 101.56 |
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