Research Article
Design and Analysis of Direct Abort Orbits in the Earth-Moon Transfer Phase of Crewed Lunar Exploration Missions
Table 1
Orbital parameters of the hybrid orbit.
| Parameter | Value |
| Departure time | 2029-05-18 11:17:07.3131 | Semimajor axis (km) | 249547.1395 | Eccentricity | 0.9738 | Orbital inclination (deg) | 27.9922 | Right ascension of the ascending node (deg) | 143.7595 | Argument of perigee (deg) | 199.3091 | True anomaly (deg) | 28.4130 | Hybrid maneuver time | 2029-05-18 21:17:07.3131 | Hybrid maneuver impulse vector (m/s) | (16.7923, 30.3731, -5.5991) |
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