archive/ES_0.5555981137552012---------------------------

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: 2024-05-14T15:07:07.613
Launch V∞: [8.082773809515784, -5.709511979563037, -0.08221754559998876] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-4.271618879525547e-10, -9.467188797709204e-10, 2.7925623958736294e-9] km/s
	V∞_out: [2.0710433474319867e-10, -6.893777317405418e-10, 1.1086040371862895e-10] km/s
	time of flight: 1.8749577786971304e8 seconds
	arrival date: 2030-04-23T17:16:44.613
	thrust profile: [0.19262882219372876 0.0017682977351410924 -0.06078570749456977; 0.07510854426601425 0.04483363097579235 -0.08152090897510195; 0.05247612556652213 0.05173429616485974 -0.10334129305288119; 0.03699212147964636 0.04836776779914272 -0.11420009851892877; 0.015257947545094692 0.023616672516294634 -0.06151535097167395; 0.05017375150264386 0.08830370298816641 -0.2186226342882601; 0.008321797426523236 0.020875746774835446 -0.0620611019471654; 0.0016554003603538512 0.004422884420023118 -0.014999979304444628; 0.0029079581542708643 0.008455953550443632 -0.03441057189742003; 0.0014578145592288889 0.005998444591665279 -0.021590817094686094; 0.00010189419917084582 0.00036538089525199125 -0.0013457387446312698; 3.4267406230693495e-5 0.00012128214999226729 -0.0004984499190272592; -3.630324776009653e-5 0.00013568298390632396 -0.0001933222589807255; -0.00011464061902182116 1.729493075479877e-5 -0.00022822609938822459; 3.130844266011417e-5 -6.033277523730223e-6 -0.00028834664280309296; -2.4080693230419574e-6 2.2064196459154254e-5 -0.00010496253498183353; 5.629619319618323e-5 -0.00017764941434590838 -8.429129071450761e-5; 4.5321256872056e-5 7.763583113794498e-5 3.631885057500916e-5; 0.0001761123035687706 0.00017277995294965204 6.818358448922729e-5; -0.0003107464502650623 6.280586170101499e-5 -5.122958464710797e-5] %

Mass Used: 76.90143723306119 kg
Launch C3: 97.9365192253726 km²/s²
||V∞_in||: 2.979454421648595e-9 km/s