High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database

Table 9

Database of entry vehicles and flight entry trajectory data.

Flight vehicles	Inertial entry velocity	Relative entry velocity	Peak heat velocity	Inertial entry angle	Control method
	(km/s)	(km/s)	(km/s)	(degrees)
Apollo AS-202	—	8.29	7.77	—	Roll modulation
Apollo 4	11.14	10.73	10.25	−6.92	Roll modulation
Viking Lander 1	4.61	4.42	4.02	−16.99	3-axis RCS
Pathfinder	7.26	7.48	6.61	−14.06	Ballistic
Genesis	11.00	10.80	9.2	−8.00	Ballistic