Design and Analysis of Direct Abort Orbits in the Earth-Moon Transfer Phase of Crewed Lunar Exploration Missions

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Parameter</td><td class="align_center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Departure time</td><td class="align_center">2029-05-18 11:17:07.3131</td></tr><tr><td class="align_left">Semimajor axis (km)</td><td class="align_center">249547.1395</td></tr><tr><td class="align_left">Eccentricity</td><td class="align_center">0.9738</td></tr><tr><td class="align_left">Orbital inclination (deg)</td><td class="align_center">27.9922</td></tr><tr><td class="align_left">Right ascension of the ascending node (deg)</td><td class="align_center">143.7595</td></tr><tr><td class="align_left">Argument of perigee (deg)</td><td class="align_center">199.3091</td></tr><tr><td class="align_left">True anomaly (deg)</td><td class="align_center">28.4130</td></tr><tr><td class="align_left">Hybrid maneuver time</td><td class="align_center">2029-05-18 21:17:07.3131</td></tr><tr><td class="align_left">Hybrid maneuver impulse vector (m/s)</td><td class="align_center">(16.7923, 30.3731, -5.5991)</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Orbital parameters of the hybrid orbit.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Design and Analysis of Direct Abort Orbits in the Earth-Moon Transfer Phase of Crewed Lunar Exploration Missions 