archive/ES_0.5851910255096334--------------------------- 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: 2023-05-09T07:01:13.033 Launch V∞: [6.092520453231594, -8.237743089736895, -1.065310727619139] km/s Phase 1: Planet: Saturn V∞_in: [-0.007747548528841879, 0.003576899223135753, -0.00851706942728192] km/s V∞_out: [0.007858383773936675, 0.0029892950955808023, 0.008649030751120754] km/s time of flight: 1.7708129877207664e8 seconds arrival date: 2028-12-17T20:16:11.033 thrust profile: [0.01343138386362536 -0.008655079767215901 -0.009171290640394642; 0.010364992538997019 -0.005908993116905651 -0.024104556825926375; 0.027359569120943318 -0.025180201654265683 -0.11791305733509903; 0.017025172423799376 -0.02172559377403855 -0.10157287860273914; 0.01859719070314952 -0.029794587139660503 -0.13657979674799287; 0.01130597914517879 -0.02031326975619058 -0.09272390871712831; 0.014120756706472668 -0.026247156520417064 -0.12454046431799279; 0.009769468969442969 -0.019993934147057423 -0.09017157590843515; 0.008734665131361214 -0.019512577945804303 -0.08646945497720798; 0.003943501006459424 -0.0077723449801612625 -0.03550652225403761; 0.003115781392621162 -0.0066495519654080504 -0.030106184285836255; 0.00046752333164908153 -0.0015619412499343261 -0.008237290006143176; 0.00045033160549715946 -0.00024163619012709873 -0.00019695844193068747; 1.0694356422877977e-5 -5.1006879187660695e-5 -0.0012847811828370604; 0.00010617541465970945 5.191807464736904e-5 -0.0006489342602647348; 0.0006131363256836819 -5.671220790393617e-5 0.00011859411286997386; -0.00026966851903133043 0.0001727145843439978 -0.0008977604244850205; -0.0005988156718989093 5.748486411870756e-5 -0.0007031536683959031; -0.0001700033179035565 -0.0003750896860997243 0.00042502508000223584; 0.00034275292771669956 -0.0012874792168824883 0.0002544017493287515] % Mass Used: 63.72392524162569 kg Launch C3: 106.11410363193369 km²/s² ||V∞_in||: 0.01205649981911705 km/s