archive/ES_0.5727724139065546---------------------------

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: 2023-04-28T19:52:10.648
Launch V∞: [5.728527403187237, -8.138608331149676, -0.3489855791331802] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-5.671928380561865e-8, 3.0320120155357914e-8, 5.2131038033973404e-8] km/s
	V∞_out: [-3.492098392460245e-8, 4.6247083581916645e-8, -5.546356589436199e-8] km/s
	time of flight: 1.5999053651757675e8 seconds
	arrival date: 2028-05-23T13:41:06.648
	thrust profile: [0.16919839001846862 -0.08636128307530151 -0.0819204617007119; 0.06603724119230643 -0.0019735762464899434 -0.08325782982196032; 0.07594003212740458 0.009440542554134738 -0.15244311178410577; 0.05979412208058979 0.012614774533608205 -0.16387805642582742; 0.048049890093125235 0.012153795419595461 -0.1628213573273256; 0.038105044924752404 0.010467066145041164 -0.15374480925597186; 0.03539457510025978 0.011466917083237481 -0.156706038600294; 0.02582609198983531 0.009628186790212549 -0.1329552335299961; 0.005832833692430322 0.001906318612936706 -0.037104195104963975; 0.0032896439331997545 -0.0007741091858372558 -0.01677126431704659; 0.0039149537548989035 0.0017168871502257453 -0.03205762739710853; -0.00023630050451029267 -0.00024421100945103884 -0.005790188161174171; 0.0006158250287064 -0.0002492562468763194 -0.0058516757620133975; -0.002757790116923408 0.0007794557390271666 -0.0019884553720874616; -0.0009244478186178324 0.004302868828872286 -0.0013889565322280346; 0.0007734221011277453 0.00221803870787473 0.0001838102784714763; -0.0009030867719588242 0.0036434166458055948 0.00028387918392873727; 0.00028884232796963104 -0.0006022852751186858 0.0001652931286490304; 0.004763711312724533 0.005295544686063497 0.0011372581720139933; -0.0005931244731254563 0.00035308564594672086 0.002877625963347176] %

Mass Used: 89.71503374132817 kg
Launch C3: 99.17476271136896 km²/s²
||V∞_in||: 8.27890812133897e-8 km/s