archive/ES_0.5689899100436812---------------------------

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: 2023-04-25T08:15:23.536
Launch V∞: [6.233142792956231, -7.133491400747147, 0.40425615733868187] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-7.838229243664475e-7, -1.1828082363761214e-7, 1.5006310873468203e-7] km/s
	V∞_out: [-7.96616796639096e-7, 7.181066373284951e-8, -8.410158822430628e-8] km/s
	time of flight: 1.8749577787496114e8 seconds
	arrival date: 2029-04-03T10:25:00.536
	thrust profile: [0.7852433542042174 -0.16787916530840502 -0.18009998122121762; 0.21400875855744406 0.08087748233915253 -0.16115312178358893; 0.09263117554565868 0.06604910601139909 -0.12322073285250285; 0.09565118964921053 0.0921890986820352 -0.17382508920895712; 0.03719806667191489 0.045157586761380576 -0.0939075410236399; 0.01706063173581573 0.024389394773108287 -0.054624806272619356; 0.015087475412929973 0.02521661995486736 -0.058704602139458294; 0.006819157787332971 0.012815574785697524 -0.03128531154067952; 0.00948021884280246 0.020359539012279645 -0.051053509654981996; 0.0025071792742359603 0.0031821545614898507 -0.005114382582048007; 0.00021842822666226426 0.0007338467254935149 -0.0017084455667127781; 0.00030873342762061313 -0.0006034324268733811 -0.000349010497613946; 0.001210753420492105 0.004070983749098491 -0.0034279427705748667; -0.0026920110572660133 -0.0007872615734159471 -0.0023083881258596757; 0.002658646486255362 0.001195304816591414 0.0005418133675524892; -0.0018050804387781689 0.0011961078173494428 -0.0012192621649919954; 0.0024362109901419383 0.0050002453830115395 -0.002139009227419182; -0.0012235989037486122 -0.005139267891956827 -0.0017799515445401678; 9.2657912180403e-5 0.0004962853096092158 -0.0013858559648775863; 0.0026509629819115098 -0.0015766241697490783 -0.011921048267340747] %

Mass Used: 139.3921102354334 kg
Launch C3: 89.90219168266194 km²/s²
||V∞_in||: 8.067760944685201e-7 km/s