archive/ES_0.7518603574347142--------------------------- 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: 2024-05-09T20:35:38.280 Launch V∞: [8.833950564623855, -7.462061032839446, -2.4489243957625613] km/s Phase 1: Planet: Saturn V∞_in: [2.700383185462534e-6, -2.624162594082143e-5, 3.951012107607454e-6] km/s V∞_out: [-4.109444996577938e-6, 1.6474659247455933e-5, 2.0571205050598835e-5] km/s time of flight: 8.107464098583187e7 seconds arrival date: 2026-12-04T05:19:38.280 thrust profile: [0.721003428335907 -0.35219709649361847 -0.2812989362998257; 0.4559321515932038 -0.04434988692102357 -0.25606221475434593; 0.23770659364621036 0.020533453100153816 -0.1791327265006237; 0.09737463100130572 0.019792562332712343 -0.09273127702901691; 0.01725200453612236 0.0053915253639849284 -0.019487749357427107; 0.0031222415356415064 0.001906881506150944 -0.0007417234777805947; 0.0044513428162406355 0.001467854137759506 -0.005749270334138087; 0.004889823436740351 0.0007210231288620668 -0.004394063995842682; 0.002698814244801409 0.0016386808161073046 0.0002036446997903626; 0.006344770865925558 -0.0006397489483257143 -0.00642024910941294; 0.0022127332336135176 -0.0027106094835372724 -0.005823175835217078; -0.0012248328749366625 -0.006836782905778038 -0.0020523283436130555; -0.0015879086849126098 0.0024410854278245735 -0.00027086400533448676; -0.0007721208076038712 -0.0024447819743308036 0.0003291097484811158; 0.0013709371481675598 -0.0015285318177885108 -0.0008830739631450436; -0.0009522705876473683 -0.009029129989637688 0.007502468784670106; -0.007787537890339004 -0.00457095323266268 0.002036023714349611; 0.002065522795291425 0.00795014838121496 -0.0048843953608595225; -0.0008920844493379135 0.0007729990446604252 -0.0004161828744149716; -0.0035079875595290123 0.0009184001130969949 -0.004160487063743205] % Mass Used: 62.14718623599947 kg Launch C3: 139.71826813220008 km²/s² ||V∞_in||: 2.6674435290007207e-5 km/s