archive/ES_0.564616864537854---------------------------

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: 2024-05-11T05:52:57.006
Launch V∞: [7.844160776463345, -5.75903303310965, 0.1447459112174354] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.003173672580468977, 0.002052709932958694, 0.000135533632893882] km/s
	V∞_out: [-0.002734899818801752, -0.0013113736433467446, 0.002265130236276142] km/s
	time of flight: 1.81226098251239e8 seconds
	arrival date: 2030-02-06T18:27:55.006
	thrust profile: [0.4938063807246066 -0.02406345450440812 -0.1356724532478948; 0.058840383642930656 0.03344481835074325 -0.06603447221410709; 0.05873172083143201 0.054936751258174384 -0.11609096192381418; 0.04537451373568675 0.05566210809593241 -0.1305004419333469; 0.026752018914926637 0.04141386203114067 -0.11449136386618135; 0.02174985029477291 0.0341538739438068 -0.1048400665814302; 0.012677617459514727 0.02288066356024928 -0.07805108694556062; 0.009832706310768083 0.02665439069570893 -0.08586248403334744; 0.0012591558670443717 0.005266625461229069 -0.02072553110203884; 0.002735195363023335 0.011923670102733177 -0.042632615393584185; -0.002219017324489689 -0.005148365782042266 -0.004231252341207124; -0.00040251198452216164 -0.004494042103840719 -0.00046612277594578703; -0.00010048647346090736 -0.00022047472081886729 0.0031074156896714836; 0.00324820007304821 0.003813280338680172 0.004751126647234675; 0.0015704473324641127 0.0009999219426868882 0.002928120474331429; -0.007074092364580663 -0.011874133489487921 0.007717819413084495; -0.002488790908688655 -0.0022112123872473073 0.00901794228146628; -0.020421336114170238 -0.003516625346029074 0.008087916154398168; -0.010897414008977766 -0.014024238969464638 0.013375817315974628; 0.001221654539080745 0.0008488137871399713 -0.003356699977570332] %

Mass Used: 106.19642696426445 kg
Launch C3: 94.71827114226832 km²/s²
||V∞_in||: 0.0037820873975271 km/s