Name | Simulation of conditions | ||||
Mesh | Ma | Ma A0A | T | ρ | |
Space Shuttle Orbiter | 114,960 | 6.02 | 29.18 | 254.2 | 4.18e−3 |
AS-202 | 33,438 | 10 | 18.2 | 274 | 1.16e−3 |
Fire-II | 24,467 | 25.6 | 0 | 253 | 6.05e−3 |