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 vehiclesConfiguration (shape)Nose radius (m)Base area ( )Length (m)Diameter (m)Mass (Kg)

Apollo AS-202Capsule Cone4.6912.023.623.91—
Apollo 4Capsule Cone4.6912.023.623.915424.9
Viking I Sphere Cone0.889.651.663.54980.0
Pathfinder Cone0.665.521.5082.65585.3
Genesis Blunt Cone0.4312.020.931.51201.0