Research Article
High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database
Table 3
Apollo 4 Trajectory data calculated by Sparta trajectory engine.
| | Trajectory analysis for flight vehicle: Apollo 4 | | Altitude | Velocity | Flight path angle | Mach | Reynolds | Stag point pressure | Stag point heat | | (ft) | (ft/sec) | γ (deg) | number | number | (lbf/) | transfer rate (W/) |
| | 250000.00 | 22513.69 | 12.00 | 23.83 | 25524.59 | 30.70 | 191.30 | | 249000.00 | 22512.32 | 12.00 | 23.80 | 26672.87 | 32.16 | 195.82 | | 248000.00 | 22510.96 | 12.01 | 23.77 | 27869.44 | 33.69 | 200.44 | | 247000.00 | 22509.59 | 12.01 | 23.73 | 29116.20 | 35.28 | 205.17 | | 246000.00 | 22508.23 | 12.02 | 23.70 | 30415.12 | 36.95 | 209.99 | | 245000.00 | 22506.86 | 12.02 | 23.67 | 31768.23 | 38.69 | 214.90 |
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