archive/ES_0.5783585941308016---------------------------

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: 2023-04-30T12:34:27.049
Launch V∞: [5.3839663660879, -8.370985481191598, -0.9801945602070417] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-4.5115968369533314e-6, 2.211209643517411e-6, 4.32551414540708e-6] km/s
	V∞_out: [-3.010174399262927e-6, 3.870055597115154e-6, -4.4592989106327e-6] km/s
	time of flight: 1.5557259013202807e8 seconds
	arrival date: 2028-04-04T03:10:57.049
	thrust profile: [0.2727283047842904 -0.15503619434373994 -0.15450093943776957; 0.0902065578437795 -0.010224015401796795 -0.13171979922498747; 0.06314487140324293 0.0013292464408968506 -0.1512324708016447; 0.0494580275113698 0.0037416956280581404 -0.16173610335580874; 0.040120368849187425 0.003761652008222334 -0.16318906618360493; 0.018788743560447622 0.00207541356337418 -0.09474887254151348; 0.028567332671762518 0.0033039265377616555 -0.1590928746948554; 0.021481206219555897 0.002430040355998009 -0.13344176226695229; 0.006150598654876201 0.00041681455553435625 -0.043055566588020865; 0.0014229889229746755 7.808632165640074e-5 -0.009831860361950192; 0.00030852773662916403 0.0001229793683890217 -0.002718458452966068; 0.0003484509852065448 -0.0001570357602184003 -7.98110030671178e-5; 0.00011724583969214368 -9.436344468836472e-5 -0.0015194141020532178; -7.367759071018809e-5 -0.00012022884175761403 -0.001055951443837918; 0.00043793344151847147 6.466269498935842e-5 -0.00047433126489739453; 0.0006138790633049131 -6.117012119826438e-5 -0.0009176006531558837; 0.0005825004826681508 -0.00021483393481763465 -0.0006049515329959851; 1.4868533741596358e-5 -0.0010734123505000616 -0.00027895097026609206; 9.374874560359872e-5 -0.002135310226065472 0.0024030800756186356; 0.0016276311061247206 -0.00038858209314572144 0.0028973981037510896] %

Mass Used: 91.29426654141844 kg
Launch C3: 100.02127313334573 km²/s²
||V∞_in||: 6.629783309347934e-6 km/s