archive/ES_0.5718548526512005---------------------------

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: 2023-05-05T23:20:07.715
Launch V∞: [6.370082729754531, -7.632283021554807, -0.42491559146609603] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.0009680454007002532, 0.005818228374755986, -0.008269555619351084] km/s
	V∞_out: [0.007102303002894247, 0.005646958002977331, 0.00457534723554265] km/s
	time of flight: 1.8749577781897807e8 seconds
	arrival date: 2029-04-14T01:29:44.715
	thrust profile: [0.26560320789822656 -0.07955256612738804 -0.11820527585854541; 0.019193890034137434 0.003988896037241503 -0.03067233587365715; 0.020244510807793107 0.006803329689751107 -0.050007298245507745; 0.04813162301253438 0.018627443463886346 -0.151830144314164; 0.03284110521324854 0.015096068531846212 -0.13647033466278002; 0.01168512670750576 0.0064464887843587405 -0.062226468334811616; 0.016037924883564886 0.008454805497921707 -0.09440314748390496; 0.031293433572147665 0.01567864297769995 -0.1807495102818963; 0.0025420776255597756 0.0010851777924797527 -0.014027367663581255; 0.000325281859469867 -0.000749009753493097 -0.02443342846376303; 0.00491945913704071 0.001536480627737306 -0.026125932599186517; -0.003842872932356826 -0.0012271632654671993 -0.0016260598319641157; -0.009557378108435136 0.003758029350912879 -0.0035457822572292014; -0.0003838523994869206 -0.010662997191053647 -0.001655868445897297; -0.0008305283235094268 -0.004300945485734622 0.009884048519642127; -0.002743104137359717 0.014034583421077215 -0.004394329647393734; -0.0061408875623675165 -0.000990344964730988 -0.0022385010514382564; 0.004930837364064772 0.0032760384434894468 0.0039017742385580216; 0.007409832471950165 0.006127689744637635 0.009121225928240138; 0.0012667909600039 0.006376125231008923 0.017284793051920475] %

Mass Used: 89.60419513114084 kg
Launch C3: 99.01025136490168 km²/s²
||V∞_in||: 0.010157482141760018 km/s