archive/ES_0.6355259765311058---------------------------

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: 2023-04-15T17:28:01.493
Launch V∞: [6.9546589202623945, -7.174810846268905, -0.7500129047133607] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-7.138959570219678e-9, 5.201047298026891e-11, -6.427193682881074e-9] km/s
	V∞_out: [-1.2912563430556722e-9, 3.0432142103353773e-9, 4.114552212632997e-9] km/s
	time of flight: 1.8279570135159373e8 seconds
	arrival date: 2029-01-29T10:03:02.493
	thrust profile: [0.3036095422666621 -0.07518571153093291 -0.06326544452097949; 0.24970132439214823 0.10076786145983235 -0.1414568533449631; 0.2009884836637603 0.15718546190037502 -0.18563790167076755; 0.15112172746670158 0.1655507961925028 -0.19588120690867464; 0.10451290496825659 0.14490374775073947 -0.17793657514639483; 0.07122355960132781 0.11931488750928605 -0.1526487010288201; 0.040159300130532746 0.07907609649719098 -0.10681184639065662; 0.016489200342817503 0.03805879751540265 -0.05406076591349519; 0.0012813707026118394 0.004301775977988875 -0.006397816131067182; -0.002473119431158756 -0.004283466296901427 0.0006432474110838098; -0.005607458746736986 -0.01265831066728459 0.017692788561714034; -0.007888631260682484 0.01277422380199924 0.011508195699845382; -0.020014103021523972 -0.011781964844367927 -0.000928796168148154; -0.002987242221644407 -0.010462766886559925 0.018728368869810757; -0.011679608683262855 -0.024226879806927906 -0.003730750445789025; -0.0006500675197867873 -0.0017599781962099798 -0.0004949001088808651; -0.013680109737262029 -0.045750880224089296 0.012223398094854659; 0.0013776456605903561 0.0043699164965250534 -0.0018314703613908237; 0.012652339594081494 0.015597343377026607 0.025173341063761356; 0.0015212232454925082 0.006969779244607658 0.021791489398645784] %

Mass Used: 155.73532667035806 kg
Launch C3: 100.40771073415978 km²/s²
||V∞_in||: 9.606053688783815e-9 km/s