archive/ES_0.5674585863499164---------------------------

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: 2023-04-30T13:22:01.327
Launch V∞: [6.157968743951819, -7.454662813292781, -0.05953205750760802] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.7138298198548577e-9, 5.6797817648142184e-9, 1.9887937730558055e-9] km/s
	V∞_out: [-2.803473406417777e-9, 4.457053956303746e-9, -7.090698590849978e-9] km/s
	time of flight: 1.8749577779548365e8 seconds
	arrival date: 2029-04-08T15:31:38.327
	thrust profile: [0.495241664901041 -0.10970789095985847 -0.1291717317483275; 0.09691637973888448 0.03596309658904661 -0.08453403511883385; 0.1077679580918508 0.0733762738151768 -0.15102259385642483; 0.07489172972871432 0.06716788955997267 -0.1460517935040199; 0.04345671387329062 0.05304733112025444 -0.1189392194765668; 0.027577754445322063 0.04052692338872483 -0.09909298715047807; 0.019545998204778717 0.028023522118189956 -0.0731312842776141; 0.007534102850428957 0.01049696529026044 -0.033994392455630726; 0.008319007859758313 0.01876558409088281 -0.05154030976496059; -0.00022387249977295041 0.007294723370766123 -0.015710539942577723; 0.003262988474043345 0.003993577554800045 -0.012874228952819141; -0.003182666114765183 0.004253580848664567 0.0012491285402733013; 0.0010020381314551421 -0.0002878189703065283 -0.0029504106709655783; 1.0445355050440531e-5 -0.0007624371415436947 0.0027395118787142993; 0.003834648094234338 0.0054471124051307575 -0.004048149886092714; 0.0009417693305957202 0.0012894454835764772 -0.006140540886135105; -0.018127452351373568 0.002265158330215662 0.0061620998640829865; -0.0007356555022514544 0.0006317003166381504 -0.002496329261184779; 0.01729723415548525 -0.005270036107446656 -0.011192728532787986; -0.005966682844232349 0.002406298861097025 -0.004899230254262388] %

Mass Used: 116.64097954095087 kg
Launch C3: 93.49612077724886 km²/s²
||V∞_in||: 7.071616045749715e-9 km/s