archive/ES_0.5604813103810956---------------------------

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: 2024-05-13T23:26:10.303
Launch V∞: [7.86586145126251, -6.026566670034078, 0.093148818514249] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-5.060877906111634e-5, -0.00039823137783029475, 0.006815496225404231] km/s
	V∞_out: [0.0007059947616333972, -0.00678998548283126, 8.287972268632665e-5] km/s
	time of flight: 1.79034006544541e8 seconds
	arrival date: 2030-01-15T03:06:16.303
	thrust profile: [0.18583165597640502 -0.01519074269052968 -0.06708723787760915; 0.08551699823459524 0.036960413326273936 -0.10138087997898503; 0.04515032776300946 0.031619707521598255 -0.09605010501410084; 0.04586668208347554 0.040731373912582365 -0.13814819981212137; 0.04158860321359826 0.04321950144952022 -0.16204405101887331; 0.019600809886506438 0.023478374309474807 -0.09642157490219541; 0.011303641068443048 0.015279614196406627 -0.06816340716049059; 0.006600666629154375 0.007963023893977812 -0.04214379692805423; 0.008908097321475433 0.01341484951024588 -0.07096954786173466; 0.0006789291135548065 0.0024374618452696396 -0.012187618872986443; 0.0021669509350638223 0.0033643025299078064 -0.02175869805958046; 0.001453604774646337 -0.0006066375838362603 0.0004459822619551383; -0.003335470164158003 -0.000447373842860297 -0.00547543418803093; 1.5935100861304757e-7 -0.0015131985797301852 0.0014586450703113546; -0.00507603267716146 -0.002230783033669459 -0.0017813560791265922; 0.0003189486231810684 -0.0006314528117163742 0.0036204162146410293; -0.006115862639810536 0.004436509736468053 0.005541692700922474; -0.006070252059724919 -0.006660465047395849 -7.08809461609412e-5; -0.00029282559694241426 0.003203498902423018 -0.0010157964872795958; 7.862321126124931e-5 0.0024537233988695425 0.00013232824532727165] %

Mass Used: 81.06176852086446 kg
Launch C3: 98.19995890121379 km²/s²
||V∞_in||: 0.0068273082746647664 km/s