archive/ES_0.5580752694488134---------------------------

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: 2024-05-15T00:28:53.414
Launch V∞: [7.983677717520839, -5.762047118347824, 0.3349771199332594] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [3.50830900751041e-5, 2.5509981099322192e-5, 0.002238790117606869] km/s
	V∞_out: [-0.0019881080010378423, -0.0006864626127812944, 0.0007643857817611048] km/s
	time of flight: 1.8586415501271877e8 seconds
	arrival date: 2030-04-05T05:24:48.414
	thrust profile: [0.34457976959723313 -0.005509751829652309 -0.11022146624880402; 0.036667356546714325 0.01927401904879624 -0.04372204134170654; 0.032909585546722166 0.027828046546774135 -0.0702297701320876; 0.022369512402589734 0.024340590082302816 -0.06998964870657211; 0.03389271647541419 0.0451686694465599 -0.14357705416154848; 0.01322316034774274 0.01979831994829106 -0.06959371655907541; 0.011443400190114347 0.019237223704783795 -0.07254684063159271; 0.007926440968444678 0.013965222319127063 -0.05757185223272792; 0.005870982573769138 0.011901417575569324 -0.05217421794633252; 0.010169555264443146 0.022353912716897087 -0.0981766209707774; 0.0027568667269406034 0.0057417957946208934 -0.02337656083047833; 0.0020987056639081353 -0.0003246922727575698 -0.0016747900871350062; 0.000423052395187118 0.00040808633908653467 -0.002745992239673884; 0.0007096027193183587 0.00042546003238409693 -0.0037072633095432; 0.00017045989762041742 0.0004276790034851022 -0.0026329991336762814; -0.0008951597723249735 -5.4835196525157516e-5 -0.0011060120299366278; 0.0009223231828094508 -3.6962231458426836e-5 -0.0024268679318460735; 0.0007405025454011579 -0.0011639116784528981 0.0001737217894406751; -0.0012716438224397923 0.0006546346238885301 0.004193359046155809; 0.00019138424600451695 9.879408483048745e-5 0.001312854472394349] %

Mass Used: 84.9481927442439 kg
Launch C3: 97.05250656217801 km²/s²
||V∞_in||: 0.0022392103012086836 km/s