archive/ES_0.5575633113772067--------------------------- 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: 2024-05-11T11:40:37.693 Launch V∞: [7.852573643423757, -5.548063181709071, 0.2750685616249827] km/s Phase 1: Planet: Saturn V∞_in: [-1.5032754348917953e-9, 4.760890177927125e-10, -6.3174525640689765e-9] km/s V∞_out: [-1.9529761391795367e-9, 6.876858195745231e-9, -1.0864238372136336e-9] km/s time of flight: 1.874957778741773e8 seconds arrival date: 2030-04-20T13:50:14.693 thrust profile: [0.6577919945672711 0.0007273318119973165 -0.17038917754168537; 0.09613848567199035 0.060424432700709456 -0.09574371461434814; 0.05465670412725712 0.05702719243744343 -0.1019298488260888; 0.052081795006155805 0.07179390780426102 -0.14052927566569134; 0.015335916965827395 0.027505181859755992 -0.06313375961869112; 0.01254031364692076 0.02738562797564909 -0.06784791612118253; 0.011901706828453556 0.031532924963926665 -0.08226001108785663; 0.006941441458028691 0.022068505061608203 -0.06140138752241862; 0.0020036229295855865 0.0069756313430837024 -0.0203288315954864; 0.001207125357674441 0.005541368285151253 -0.018864883905928755; 0.000879447284924116 0.0034390257977164112 -0.012219509486297065; 2.2300235175791872e-5 0.0005949048642786994 -0.0021204377073580183; 0.00013131633786300014 0.0004325645931848928 -0.0015786735981175638; -0.00010594503516549403 0.00016353768251275197 -0.0005508148571624078; -5.279077622562459e-5 0.00041047967077305597 -0.0005399116395913491; 7.060253205844282e-6 -4.718194580901366e-5 -0.0004969395885567097; 0.00023895232108799415 0.00015658438967314708 -0.0002615802433665631; -7.405409463817346e-5 3.049850075406864e-5 0.00018925458009889755; 0.0001602681785364353 -7.143979562023394e-5 -0.0004702909106885857; 0.00026654886003091185 0.0002904331496345976 -0.0007110268895467238] % Mass Used: 110.7929763979364 kg Launch C3: 92.51958060722369 km²/s² ||V∞_in||: 6.511275196555098e-9 km/s