archive/ES_0.566271536782522---------------------------

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: 2024-05-08T10:34:33.475
Launch V∞: [7.5072606383980105, -6.350116596222346, -0.17604881906521846] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.3698738684857038e-8, 2.9715672145919723e-8, -1.0906698273966597e-7] km/s
	V∞_out: [-3.411028973967394e-8, 1.0456196131891427e-7, -1.8539712964042605e-8] km/s
	time of flight: 1.626189788556862e8 seconds
	arrival date: 2029-07-03T14:30:51.475
	thrust profile: [0.3185864160958903 -0.05072842423172202 -0.1118186795519223; 0.08059495255090554 0.028996208211253087 -0.08745990294753868; 0.05547859218025323 0.03535033545180441 -0.10195985780100136; 0.08900655891054694 0.07750384224016724 -0.22333039216944048; 0.039477009701975825 0.040132875554138484 -0.1317460607091713; 0.035770802370850306 0.04259469830058214 -0.14758196406272658; 0.03586020238497134 0.047591234975000965 -0.1732131153986931; 0.010828987457532663 0.014564504005133965 -0.059125123910608486; 0.0016289944469981882 0.0008231206333478044 -0.007721093481697808; 0.0009920292325589894 0.001101767916333091 -0.0052735475373672; 0.004582325939044139 0.008560161892341827 -0.03447380242347163; 0.00256872391827525 0.004739511074876211 -0.02079745485580202; 0.003965703911020146 -0.0008786196092170353 -0.0023782588490415166; 0.0011170657859859115 0.0006147680327391289 -0.002896016561388861; -0.003086851238131774 0.003619922265883683 0.0004829379059540849; -0.0055393395133540605 -0.0015540601979559896 -0.0014927977313907081; 0.00039561288646976765 0.0007955546086766587 -0.003371032485076254; -0.0005206333618692164 -0.0014715506177903842 0.00015149027181619173; -0.0011975569328793031 0.002433826240878195 -0.009228211113362217; 0.0017083869777228659 0.0014968021438576651 -8.569923862991255e-5] %

Mass Used: 96.48549803288415 kg
Launch C3: 96.71393626515284 km²/s²
||V∞_in||: 1.1386958916486167e-7 km/s