archive/ES_0.5718409557896349--------------------------- 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: 2024-05-07T07:21:56.193 Launch V∞: [7.435816629974283, -5.79267339838994, 0.0011984836760086757] km/s Phase 1: Planet: Saturn V∞_in: [-0.0004076536863218443, -0.00032580544828378214, -0.00026214489203088526] km/s V∞_out: [-5.342004207510438e-5, 0.00037058861209174126, -0.00044665055167672306] km/s time of flight: 1.8749577787061194e8 seconds arrival date: 2030-04-16T09:31:33.193 thrust profile: [0.6843626168983197 0.03958614700531103 -0.10414866306230014; 0.2662886657977923 0.20706450294723708 -0.14474108898270183; 0.16239568820641262 0.2275006099082793 -0.1699384287122316; 0.05233429956795594 0.10511225020855197 -0.09571185154845968; 0.04098893427798517 0.11433487283560811 -0.1089328491283928; 0.019200640185354268 0.06882361568277812 -0.0728517496284314; 0.006986402147871146 0.034195932735185515 -0.04026503586667389; 0.006009788904431868 0.04291131486085503 -0.05065089784489313; 0.0003934076797187982 0.0034988780060796216 -0.004270893361700056; 0.003560820966124698 0.03272282405238961 -0.03975212312359403; -0.00021537413212458889 -0.0007694781795039524 0.0007275200936690824; -5.1027174186472305e-5 -0.000815809846853853 0.0001399653150578054; -0.0009218918658660499 -4.928908244784954e-5 -0.00039793435684107884; -2.7633963264080857e-5 0.0004850721009236268 -0.0008691627649469517; -0.0011342723049894304 -0.0005048984060576215 -0.00048733677349791795; 6.349509671393455e-5 4.7994432310831544e-5 -0.0009093092629562887; -0.0005279208649277239 0.0017541382789762732 -0.0008852182062264295; -0.0012790183314062775 -4.1450966153496675e-5 -0.0004970361936130209; -4.0777109369353613e-5 -0.0009967471897851768 -0.0001127734486226619; 0.0016074773222735906 0.0005785178780263903 0.0013758044717791106] % Mass Used: 148.8769080548591 kg Launch C3: 88.8464354913797 km²/s² ||V∞_in||: 0.0005839954302227624 km/s