archive/ES_0.5589866850116092--------------------------- 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: 2024-05-13T06:32:29.328 Launch V∞: [8.015705463212925, -5.694641809904868, 0.19785760350969475] km/s Phase 1: Planet: Saturn V∞_in: [-1.064688409533968e-9, -4.4004313078380864e-10, -1.0855092874781092e-9] km/s V∞_out: [-1.4079465213247278e-10, -2.871147760411587e-10, -7.640177620739982e-12] km/s time of flight: 1.8552766468799746e8 seconds arrival date: 2030-03-30T14:00:13.328 thrust profile: [0.30029969383376676 -0.006151316839868422 -0.09069906883316357; 0.06969721952933149 0.040742667598431266 -0.07529073071475856; 0.0721074455216705 0.06713403677569085 -0.13802397437249728; 0.04124897400701979 0.05109085219170572 -0.11841518014631608; 0.024406314579260457 0.03741617293624384 -0.09622745718829216; 0.02266563193634918 0.04116808091632249 -0.11375561952718528; 0.008012587795885562 0.013499938625792043 -0.041089020613872186; 0.008193601070818577 0.01617700750740553 -0.051902431439673644; 0.0058916490652947285 0.015286473335970286 -0.05127359331912535; 0.00226871259797063 0.0028465827236193717 -0.0029214486542975533; -0.0048748247185496415 -0.004074877177715267 -0.013664741460293305; -0.007599070291479545 -0.0014734331870206053 -0.0012991921417806666; -0.0003654069181813856 -0.0004944297094640808 -0.001502689308175136; 2.4985018806385098e-5 -0.0014584061926795964 -0.0016556062193015405; -0.005406342099960073 -0.00139313054097906 -0.014779268019143624; -0.002115135962130081 -0.006120204708505066 -0.016009269264263413; 0.0004681773735779346 -0.002238232468078076 -9.43754968601634e-5; 0.00047496020669182367 0.0033428967658338197 -0.00030060160904642235; -0.0002409547170344851 -0.0011813926484833916 -0.0049759410286317075; -0.0003153941583804233 0.0028860449306335086 -0.0030142958094638733] % Mass Used: 87.95330807058326 kg Launch C3: 96.71962704736472 km²/s² ||V∞_in||: 1.5828865340090613e-9 km/s