archive/ES_0.5684101991076171---------------------------

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: 2024-05-18T16:15:57.418
Launch V∞: [8.16998217102016, -5.880946888183414, -0.26368287857865486] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.045286572417431e-6, -2.4621728030110603e-5, -4.793595016232642e-7] km/s
	V∞_out: [-2.3544412342328448e-5, 4.179875343075191e-6, -6.19479668552582e-6] km/s
	time of flight: 1.874957778755006e8 seconds
	arrival date: 2030-04-27T18:25:34.418
	thrust profile: [0.04202186258525911 -0.00197568737384465 -0.018234699506615177; 0.021956451177793847 0.008410857738519236 -0.031998723658939784; 0.029470267727784844 0.018548341538820637 -0.07532746913221362; 0.03248037423742059 0.02450141524213732 -0.11779645495331857; 0.02860839685423074 0.023968366443935758 -0.13480460057639368; 0.022736069329456866 0.020424318860782775 -0.12917895181318292; 0.008339598979702151 0.007909022560207628 -0.05774221404657654; 0.004907537460482163 0.004843620864099521 -0.03784117613356993; 0.005229681011171165 0.005495389306726299 -0.04577646062767342; 0.007120976208820196 0.006894721641901804 -0.06560905990443847; 0.0037249024387533587 -0.006811902659940842 -0.00116505006540918; 0.0005830088512573312 0.0005949163257201487 -0.010033377325494431; -0.011552261589062758 0.00915138260780549 -0.008855878575509013; 0.005933666622666067 9.833080623433037e-5 0.00525071191364147; 0.002163198767321356 1.4475537739866402e-5 -0.006001226293558618; 0.015664987207035835 -0.029421495921283215 -0.0035014368266351563; -0.01675382483024132 0.019763278192448393 0.00547272430890848; 0.019190914736231503 0.022653161667804733 -0.010613006274891224; 0.006748524837195469 -0.01137826578892523 -0.0366045015041789; -0.002504335778860241 0.0015499130219679101 -0.002067491015903016] %

Mass Used: 71.62380274377074 kg
Launch C3: 101.40367363687702 km²/s²
||V∞_in||: 2.4648567924709276e-5 km/s