High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database : Table 9

]>High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database : Table 9

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
Flight vehicles	(km/s)	(km/s)	(km/s)	(degrees)	Control method

Apollo AS-202	—	8.29	7.77	—	Roll modulation
Apollo 4	11.14	10.73	10.25		Roll modulation
Viking Lander 1	4.61	4.42	4.02		3-axis RCS
Pathfinder	7.26	7.48	6.61		Ballistic
Genesis	11.00	10.80	9.2		Ballistic