archive/ES_0.5566428561477481---------------------------

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: 2024-05-14T03:06:50.129
Launch V∞: [7.9904655745217115, -5.816567765993122, 0.11449806474032297] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.1839950232741977e-6, -1.9303196860649243e-5, 0.000374325913271446] km/s
	V∞_out: [1.3129786916845373e-5, -0.0003745486882505314, 3.986103624987299e-6] km/s
	time of flight: 1.8325537600658333e8 seconds
	arrival date: 2030-03-05T03:23:06.129
	thrust profile: [0.26733204128291443 -0.011972022521882373 -0.0913859369837037; 0.026010295435686285 0.013008571561396934 -0.03198959628647852; 0.043145078536829334 0.03520214084364385 -0.09213774232149849; 0.0450254563607517 0.047746901798687444 -0.13906582061685477; 0.02820914779573896 0.03539732877796254 -0.11622688186879702; 0.02072819226425234 0.029902571346641385 -0.10783128493668631; 0.02261070872321436 0.03732842667152103 -0.14317395202459665; 0.004382582593660741 0.007973503663411268 -0.03399918952692313; 0.004163054127867918 0.008224005523697144 -0.03809726832256122; 0.0015642603055045744 0.003012204185371825 -0.01454430185627503; 0.0008630042021587069 0.0017748542290626503 -0.008850391559611022; 0.0004597312758080904 -7.08382389103411e-5 -0.0025008897672467003; 0.0010844825241997785 -0.0011336429994132893 -0.0006114373568926342; 0.0005133400318256399 0.00024610646563474886 -0.0012798616417332399; -0.0005800013960069496 -0.0003503376349496729 -0.000633589402142731; 0.00010344522438565652 4.969986130715185e-5 -0.0003057487889581071; -4.2506385365939533e-5 0.0009942840826732636 -0.0017574116641948107; -0.0002915727543048273 0.0001918456669195535 -0.00026025705353087565; 0.00018706150287576802 0.00025316263627356864 -0.004940150777385431; -0.0015121015527075029 0.0003673949892106 -0.0006822584770575116] %

Mass Used: 79.54018770082894 kg
Launch C3: 97.69311048083608 km²/s²
||V∞_in||: 0.00037482965809792156 km/s