archive/ES_0.5584072778234828---------------------------

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: 2024-05-14T04:20:55.445
Launch V∞: [8.089215775688869, -5.634845007166464, 0.14996553482798738] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.00203537994289273, 0.001303617183288147, 8.820168465147944e-5] km/s
	V∞_out: [-0.0017743059349150595, -0.0008046226121725889, 0.0014577282607330113] km/s
	time of flight: 1.8749577787478366e8 seconds
	arrival date: 2030-04-23T06:30:32.445
	thrust profile: [0.2730087221065171 -0.00034027296224382723 -0.08924477678658817; 0.07442551670156886 0.042070486756309665 -0.08467298548396036; 0.05064014345204702 0.04587676932904794 -0.1029270650477812; 0.03583721720016671 0.041487872327085965 -0.1103018952201258; 0.028574126501608853 0.041452791554393006 -0.12130118338702081; 0.018643191018775034 0.02938681168509092 -0.09533712833018759; 0.015530800982869415 0.02848155056369794 -0.09636668359360537; 0.00424554230477929 0.009431768880712626 -0.03547286612049364; 0.0006728506792719225 0.0025409204606803622 -0.014829069658383874; 0.0019707848663760713 0.0025776818444121167 -0.01407548869314083; 0.002226218299227297 0.0026071629953406013 -0.008222649575123598; 0.002448187362340949 -0.0003433192942656478 -0.008024561811111245; -0.00013363432655545877 0.0035498673716862226 -0.0005557785561134659; 0.002093813501192796 0.004599663371419815 -0.0017335095346105408; -0.00443631448653857 0.006750556217927216 -0.005293854982843309; -0.00022545798018459157 -0.00024304737229406779 -0.006949008370760963; -0.00041468441138296975 -0.011426781380108681 0.0009973162477645266; 0.0028538712350747427 0.0022883978768627427 -0.010394010815438188; 0.004073785066927421 0.003976110737552098 0.0007020269312485205; 0.003937792982439478 0.0016924498479485293 0.0010920470853770649] %

Mass Used: 84.42044206527044 kg
Launch C3: 97.20937978207876 km²/s²
||V∞_in||: 0.0024186708766736936 km/s