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 (m^2)	Length (m)	Diameter (m)	Mass (Kg)
Apollo AS-202	Capsule 33^∘ Cone	4.69	12.02	3.62	3.91	—
Apollo 4	Capsule 33^∘ Cone	4.69	12.02	3.62	3.91	5424.9
Viking I	70^∘ Sphere Cone	0.88	9.65	1.66	3.54	980.0
Pathfinder	70^∘ Cone	0.66	5.52	1.508	2.65	585.3
Genesis	59.81^∘ Blunt Cone	0.43	12.02	0.93	1.51	201.0