TRAJECTORY OPTIMIZATION TOOL v2
Optimization Report - 29-Apr-2013 07:34:49
Flight Plan: EarthVenusMercury2020s(2_5_3)
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RESULTS
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OPTIMUM EARTH DEPARTURE DATE: 11/6/2026 23:13:17 - C3: 23.7011 km²/sec²
OPTIMUM VENUS SWINGBY DATE: 4/19/2027 2:2:2 - Powered Delta-V Required: 3.2051e-006 km/sec
OPTIMUM MERCURY ARRIVAL DATE: 8/29/2027 16:48:56 - Body-centric Arrival Velocity: 9.7144 km/sec
TOTAL COST: 76.5452879
ORBITAL ELEMENTS - J2000 Ecliptic Reference Frame
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LEG 1 (Number of Full Revolutions: 0)
-Semi-major Axis: 115932855.0054043 km
-Eccentricity: 0.2800488
-Inclination: 2.8754578 deg
-Long. of Ascending Node: 44.2347977 deg
-Argument of Periapse: 176.2990142 deg
-True Anomaly (start): 183.6494329 deg
-True Anomaly (end): 93.9358416 deg
LEG 2 (Number of Full Revolutions: 0)
-Semi-major Axis: 92190316.9100125 km
-Eccentricity: 0.3298355
-Inclination: 3.1714324 deg
-Long. of Ascending Node: 69.4435780 deg
-Argument of Periapse: 106.8876476 deg
-True Anomaly (start): 138.1723174 deg
-True Anomaly (end): 36.2324347 deg
GENETIC ALGORITHM INFORMATION
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Termination Reason: Average change in trajectory fitness function less than tolerance.
Number of Generations Computed: 51.0
Number of Fitness Function Evaluations: 8355.0
Random Number Generator Type: mt19937ar