Research Article
High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database
Table 8
Database of entry vehicles and flight vehicle geometric dimensions.
| Flight vehicles | Configuration (shape) | Nose radius (m) | Base area () | Length (m) | Diameter (m) | Mass (Kg) |
| Apollo AS-202 | Capsule Cone | 4.69 | 12.02 | 3.62 | 3.91 | ā | Apollo 4 | Capsule Cone | 4.69 | 12.02 | 3.62 | 3.91 | 5424.9 | Viking I | Sphere Cone | 0.88 | 9.65 | 1.66 | 3.54 | 980.0 | Pathfinder | Cone | 0.66 | 5.52 | 1.508 | 2.65 | 585.3 | Genesis | Blunt Cone | 0.43 | 12.02 | 0.93 | 1.51 | 201.0 |
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