Research Article
Optimal Two-Impulse Trajectories with Moderate Flight Time for Earth-Moon Missions
Table 6
Lunar mission, major parameters, km, km.
| | Model | Maneuver | | | | | | Feasibility | | (km/s) | (km/s) | (km/s) | (days) | (deg) |
| | | 3.8483 | 3.0648 | 0.7835 | 4.560 | −116.881 | Yes | | | 3.8504 | 3.0652 | 0.7852 | 14.157 | 8.851 | Yes | | Simplified | Counterclockwise | 3.8471 | 3.0646 | 0.7825 | 23.798 | 135.197 | Yes | | PCR3BP | | 3.8127 | 3.0585 | 0.7542 | 32.111 | 232.260 | Yes | | | 3.8161 | 3.0591 | 0.7570 | 40.874 | 347.201 | Yes | | | 3.7633 | 3.0498 | 0.7135 | 58.685 | 220.409 | Yes |
| | | 3.8541 | 3.0678 | 0.7863 | 4.760 | −114.110 | Yes | | | 3.8559 | 3.0681 | 0.7878 | 14.809 | 17.504 | Yes | | Simplified | Clockwise | 3.8513 | 3.0673 | 0.7840 | 24.948 | 150.265 | Yes | | PCR3BP | | 3.8026 | 3.0586 | 0.7440 | 32.080 | 232.475 | Yes | | | 3.8060 | 3.0592 | 0.7467 | 40.864 | 347.620 | Yes | | | 3.7530 | 3.0498 | 0.7031 | 58.488 | 220.014 | Yes |
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