archive/ES_0.5809039723548683---------------------------

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: 2024-05-23T03:41:34.687
Launch V∞: [7.909238451578536, -6.536820396957248, 0.23401141762581298] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.002145964332949543, 0.0021491378908045002, 0.0021310963158293634] km/s
	V∞_out: [1.1869201509560617e-10, -3.858981596699397e-10, 6.482388151860139e-11] km/s
	time of flight: 1.8215345104353204e8 seconds
	arrival date: 2030-03-01T09:52:25.687
	thrust profile: [0.011223836345057607 -0.002405491450338093 -0.005035848091993523; 0.010192238047969806 -1.815902558530685e-5 -0.01534141662708523; 0.027843945214572667 -0.0015274624207794363 -0.07517215424257974; 0.041120842260989644 -0.006814024190591671 -0.14742916645536588; 0.03538521069239052 -0.009688077852085484 -0.15072147724310106; 0.029817542607801596 -0.010830847436505479 -0.1414987860010657; 0.021178192777742365 -0.009141829613532826 -0.10694770909844549; 0.009730865685205715 -0.004820783828936357 -0.050966963296696324; 0.007623172462812513 -0.004334018176009227 -0.042537971601205204; 0.0012318414237798671 0.0009732745198074371 -0.0073380600411727046; 0.003241986824040332 -0.0022718508044426607 -0.01889615896003673; -0.003469510507351066 -0.0021296196773950026 -0.005767191660868389; -0.002443359801392004 -0.0023157982369630915 -0.006152637627868374; 0.005878497056382689 0.004807752990210958 -0.006074228685341771; 0.0018853109344169558 0.002770283897219178 -0.0026938332268605664; 0.010874673578507929 0.0041606059657862396 -0.014087127072923587; -0.0011947460302190016 -0.0006661098103249367 -0.002447325602800236; -0.007283427175156565 -0.007581128771031615 -0.01388625177354469; 0.0008959184262979086 0.00016214696530379575 -0.0006254102390689763; 0.00470496329600598 0.005321020962407007 -0.003380944911063422] %

Mass Used: 63.23309615810649 kg
Launch C3: 105.340835129584 km²/s²
||V∞_in||: 0.003710192461224172 km/s