archive/ES_0.5648796174355584---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-08T21:45:55.979
Launch V∞: [7.6757265444883105, -5.491682245671845, 0.45294233505462184] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.254063974528267e-9, -2.728748983157911e-10, -6.190449309965719e-10] km/s
	V∞_out: [8.276326960827742e-10, -7.448626779081723e-10, -6.654772883323519e-10] km/s
	time of flight: 1.8576048952832606e8 seconds
	arrival date: 2030-03-28T21:54:04.979
	thrust profile: [1.0 -0.01343240604502063 -0.2588233003905733; 0.08543560222702407 0.05793023154048169 -0.08368225745059132; 0.04241516881629683 0.04686207750753955 -0.07169303820458736; 0.03225428044294903 0.04783309351688668 -0.08125198896016796; 0.02007200525273753 0.038207920279460926 -0.07252274663079519; 0.023272387723305313 0.05675948176127485 -0.1121116890288445; 0.010680226462046765 0.029770064047565672 -0.06460825973916241; 0.01029670105918232 0.0350631244241419 -0.07964282749625198; 0.0034362191791125945 0.013852132089053882 -0.034488188572954756; -0.0001391886962614576 0.00017438770951904987 -0.007383277810759364; 0.0014776767618254855 0.004609542561549683 -0.006710667807810056; 0.0007841337354640715 0.0019158014370127135 -0.005498592321271004; -0.002682020329065167 0.0030384353204090846 -0.004626429984531037; -2.1330377581293015e-5 0.001092122721298435 -0.003872295265972655; 0.0034153635559078903 0.002833623715062048 -0.005620645402110906; 0.012615217385683879 0.0068149144839275205 -0.0038236565698825673; -0.0008863913339049575 0.001785275503626765 -0.002946962307279601; -0.00020960599482320675 0.004603218896835132 0.00013982833826776074; 0.011029776912165109 -0.0064313961929341554 -0.017380639620498742; -0.008290926897811515 -0.011599231698945892 -0.00471088865794358] %

Mass Used: 138.22325332104992 kg
Launch C3: 89.28050863207454 km²/s²
||V∞_in||: 1.4249048350444453e-9 km/s