archive/ES_0.5604836013510789--------------------------- 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: 2024-05-10T15:43:31.020 Launch V∞: [7.694783728191287, -5.717176288374444, 0.5819068798802134] km/s Phase 1: Planet: Saturn V∞_in: [1.43342828294381e-8, -1.2799489570239335e-7, 2.3240652997518426e-8] km/s V∞_out: [-2.0794519257904523e-8, 6.945965027801902e-8, 1.1042695701200986e-7] km/s time of flight: 1.8749577787472397e8 seconds arrival date: 2030-04-19T17:53:08.020 thrust profile: [0.5406314390090866 0.025298330072389862 -0.09590024194290303; 0.20871004310176328 0.1523634031129578 -0.15009246679935076; 0.06481381760141115 0.0791339183408428 -0.09474999431915161; 0.08081273902568609 0.1387233110119409 -0.1730871416069591; 0.02303964317850747 0.051426729298393856 -0.07528368751386454; 0.012770077657664244 0.03625668272532286 -0.057537671882789264; 0.018407972297705067 0.06619817025281399 -0.10653298608851722; 0.0013016869194058308 0.006412927615775936 -0.011935880115878069; 0.0008083920411999756 0.004777031818532067 -0.009316017827292624; 0.0006824488322949591 0.0003138775943246491 -0.0014900507679733565; -0.000138239190353156 0.0019227107564720515 -0.0032003322895003514; 7.728087780787594e-5 -0.0004383768768840698 -0.0012575193244231402; -0.0005987222763326814 0.00024443825792812274 0.0006624315854341576; -0.00010078988283900885 -0.0003344043906047741 0.0008703146262734609; -0.0008846500639587221 4.069522366257451e-5 0.0008763760928179932; -7.721102709261997e-5 -0.0005562196454510416 -5.9913879491962094e-5; -0.00024435050619683266 0.00021257863315109996 0.0008089514832868828; -0.0011356869127682164 0.0001389770854321145 -0.00037888702250623457; -0.00013169470230192852 0.00022168340958404845 0.0005857656537055908; -0.0004848755846178132 -0.0004420232110504442 -1.1120371048535581e-5] % Mass Used: 115.86343601802355 kg Launch C3: 92.2344169528403 km²/s² ||V∞_in||: 1.3087510436233448e-7 km/s