archive/ES_0.626379305298443---------------------------

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: 2023-04-24T08:47:51.234
Launch V∞: [5.408304270702902, -8.743812594497424, -2.180707880578458] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [7.54132498143821e-5, -0.00010667940882707948, 0.0001026993586217969] km/s
	V∞_out: [0.0001032166243928711, 0.00010436223762339354, 7.85166781543103e-5] km/s
	time of flight: 1.0913697107047422e8 seconds
	arrival date: 2026-10-08T12:37:22.234
	thrust profile: [0.4888617614415419 -0.38351700129483846 -0.31207329356311814; 0.2583314457364551 -0.062385569216167724 -0.28846040363273795; 0.16895795350710788 -0.00653243979321702 -0.26992391168575885; 0.11525907547906458 0.008215316217207088 -0.2343766786988071; 0.03637753141913267 0.004645967975641071 -0.0895743549249069; 0.021215805483795744 0.004027721931198392 -0.06002120441690467; 0.012981789395908855 0.0028560280814991373 -0.04133652925988223; 0.009459946148923514 0.0019805362056392467 -0.02976978902609066; 0.0038471310700120046 0.003304141779008289 -0.02232830341386636; 0.0018056964219016027 0.0010870599576444295 -0.0050361416742854635; 0.003481039004068949 0.001361452695296955 -0.015231579242469123; -0.0006428304801527645 0.00042452266904790403 1.2648772628603977e-7; -0.0022444735138082055 0.00015094361679745643 0.0015014299378302465; -0.00511521894361131 0.003585517628796636 -0.00544672863757952; 0.002543433089115722 -0.0008531087964355468 -0.0007313055276268452; -0.004348509871156881 0.001309296817059514 0.0010629288630821633; -0.0008663643270725113 0.0006772705000101531 0.0009351667667512791; -0.0004814672311302373 -0.00033633834907573245 0.005105502105205013; -0.00788828367394365 -0.0037253008314233017 0.0050460921126171615; 0.001566576583370093 0.0008621672437037314 -0.0059952624707459035] %

Mass Used: 86.42876915794659 kg
Launch C3: 110.45950063261202 km²/s²
||V∞_in||: 0.00016617705249699795 km/s