archive/ES_0.5641776240733896---------------------------

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: 2023-04-29T02:43:25.202
Launch V∞: [6.414690673026299, -7.548065925128721, 0.09700226562651526] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [2.470260176794377e-8, -9.470288622302613e-9, 3.139846673802793e-8] km/s
	V∞_out: [1.0717287144531205e-8, -2.39353316215673e-8, -3.176251267378959e-8] km/s
	time of flight: 1.7898976762779105e8 seconds
	arrival date: 2028-12-29T18:06:12.202
	thrust profile: [0.16839805600916932 -0.0529282306234034 -0.06433514769235524; 0.08881862514174126 0.0184432852622202 -0.09897194128763233; 0.06616728761402342 0.029658618959957854 -0.12318904491060209; 0.053984660813677116 0.032144751644004495 -0.13516506232320347; 0.04457232007983585 0.03207963153538172 -0.14243261167194401; 0.0358517909854601 0.030896939684311273 -0.14106474339577493; 0.022883794665471618 0.022109436800534253 -0.10859172612399011; 0.014073479237509545 0.014022430660448833 -0.074038936818469; 0.008642257134688285 0.00848883828497967 -0.04785030432725029; 0.003066739803052123 0.0033625383467429265 -0.020505388786202942; 8.674842572441938e-5 0.000276380372201988 -0.0011793232380791908; -0.0003020427927103919 0.002296809400092457 -0.00457517802861623; -0.0008517741640015212 0.000988385601020528 -0.003045912344045693; 0.0014990209450960865 -0.0011261481735002751 -0.0006119694025433758; -0.0017342716186769976 -2.1322616810561933e-5 -0.0006449612137361177; -0.00011000580340913397 0.00010977260746994431 -8.410571333720442e-5; -0.000476895721089735 -0.0004777044199428134 0.0002410147207196258; -0.003252559578955123 -0.0023901948051272405 0.005733380226175796; 0.0019997023043979703 0.0010666652216865255 0.0015533289552462429; 0.0016457930762404267 0.001733354949286066 -0.002718751902839541] %

Mass Used: 85.77659845090784 kg
Launch C3: 98.13096508023658 km²/s²
||V∞_in||: 4.105811264773844e-8 km/s