archive/ES_0.5671638489803492--------------------------- 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: 2024-05-21T07:57:39.152 Launch V∞: [8.02799167953936, -6.21945078112879, -0.2480256607518069] km/s Phase 1: Planet: Saturn V∞_in: [-0.004122530908280575, 0.00277302635222581, 0.00017557330716542666] km/s V∞_out: [-0.003627676612661042, -0.0016563441553418888, 0.0029820496369078846] km/s time of flight: 1.8542558144880286e8 seconds arrival date: 2030-04-06T11:04:00.152 thrust profile: [0.01238659047021895 -0.0017041265851715495 -0.005914924751124166; 0.059099857914449445 0.012665934483907047 -0.09631439166233294; 0.019709964460072373 0.006063796376019237 -0.05473801049106226; 0.018300992883413428 0.004820591263157671 -0.06897300961021403; 0.023833677844967382 0.0052983591589800755 -0.11173209431744943; 0.015882020148939947 0.0027452293320211485 -0.0862480265737424; 0.009417068728404872 0.0009751020930700582 -0.05787017336767542; 0.02428708727042855 0.005063480837427333 -0.1625645229032626; 0.0123560966070828 0.00016408092203597441 -0.0870413212022531; 0.000191421431992681 6.65768494336354e-5 -0.0038082841843931495; 0.0021366867324922054 -0.0001441455805661688 -0.016417436906795584; 0.0007513290137278542 0.0002833852540375084 -0.00458137387517342; 0.0006512179297833952 0.0005251273870885459 -0.0013819732108859195; -0.00018871021555624248 2.127141597313046e-6 -0.00047045740246799055; 0.00019501354215182122 2.4747211852259787e-5 -0.0014974800828377176; 0.00030196060106617707 0.00022525477285959667 -0.0005838200254834559; -0.0002766681552028913 2.4525549657394137e-5 -0.0005855899123335777; -0.0006718428585305565 -0.0006689028959147235 -0.0016885477480926537; 0.0003819922481899097 -1.8515067322701933e-5 -0.002282519488836446; 0.0020017328622556826 -0.0031000590571535085 0.0019666382211998555] % Mass Used: 59.73936874524361 kg Launch C3: 103.19173515402808 km²/s² ||V∞_in||: 0.004971494968925992 km/s