archive/ES_0.5647677684606803---------------------------

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: 2024-05-20T20:25:48.706
Launch V∞: [8.065732858499672, -6.049608929497405, 0.06137928347124824] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.0543286399746387e-6, 1.695447299374871e-5, -3.117667975206961e-6] km/s
	V∞_out: [2.6809428775302765e-6, -9.867692410258092e-6, -1.4185368116177491e-5] km/s
	time of flight: 1.8749577786880606e8 seconds
	arrival date: 2030-04-29T22:35:25.706
	thrust profile: [0.11367459515256198 -0.013369043542301968 -0.05081414328959648; 0.02555922087127929 0.006497291350389676 -0.04257148199262253; 0.018276071599037807 0.004891065996660272 -0.048410100500582; 0.04888865169700986 0.012386629239138226 -0.17717008637822995; 0.015971788258942538 0.004905053414835345 -0.07765163919749242; 0.018218404582748808 0.004188727319480356 -0.1017696959366769; 0.01632203122353004 0.003228264534802086 -0.10134840768125318; 0.01465180946627576 0.0019759399823183208 -0.09941162695803402; 0.004153460424234228 2.9183495592686608e-5 -0.02562401215393424; 0.0009309328263994855 0.0005540838003878519 -0.01718717553898231; 5.4830604791208395e-5 -8.181531327022301e-5 -0.002379101478144297; 0.002068946737432569 -0.00012878227695683868 -0.01399609514473025; 5.1495754166753875e-5 0.0003893444371901552 -0.0005220550330731922; 0.0020132822031893845 0.00038626644702734593 0.000598940492158675; -0.00033490008399433857 -0.0006110304976251565 0.0015624682316568474; 0.0022000529001268403 0.003729594140549238 -0.0014994230909240404; -0.00026797192685207495 -0.0002622040991580028 0.003608580448011668; -0.00016485092078939696 -0.002356548255852936 0.00241180233550838; -0.004108642727085965 0.0005936217786665085 0.007165573331781934; -0.0004254008186550434 0.00027644160776314227 0.0007511125670282608] %

Mass Used: 65.89316726510333 kg
Launch C3: 101.65758216097548 km²/s²
||V∞_in||: 1.7360710649636593e-5 km/s