archive/ES_0.5561948554952668---------------------------

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: 2024-05-14T19:19:51.086
Launch V∞: [8.027257771426303, -5.751029742465006, 0.1332415757372591] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.996704513595591e-9, -2.8872595064365186e-9, -1.698222051698766e-9] km/s
	V∞_out: [-3.763168813343039e-9, 3.5323913902041604e-9, -1.3096993558089484e-9] km/s
	time of flight: 1.8566238283265916e8 seconds
	arrival date: 2030-04-02T16:12:53.086
	thrust profile: [0.27011754470687466 -0.006788958430169067 -0.09578769835213245; 0.06747294728421041 0.03511777475448707 -0.0832653851106804; 0.03154083920002875 0.026401029320391782 -0.07186440392301507; 0.03672728710830956 0.03914617170684921 -0.12110595144850904; 0.023936028510890498 0.030436904958904675 -0.10439172603420367; 0.022780991713095576 0.03365951098157784 -0.12387430576467613; 0.010174497362932635 0.0173773577030187 -0.0711691767840183; 0.005848639306299848 0.010802316391505064 -0.048532454539923255; 0.00480814153615586 0.007486704052793657 -0.04013851328129602; 0.003415466018552759 0.007740631446456661 -0.03404779727895638; 0.0002969032935140123 0.0005399420346092684 -0.002904757101885378; 0.0014217940840119702 0.0035854264794126364 -0.019904284203254016; 1.4722210025941665e-5 1.5206434210977642e-5 -0.0002680635990710089; 4.0161696444535055e-5 1.3549201179789951e-6 3.9094005441680556e-5; 0.00010710897230466654 -1.7092843794915374e-5 -1.9145966940746148e-5; 2.4042287697298816e-5 -7.506572619830177e-5 -0.0001261706526671556; 1.3079608336918317e-6 0.0002093422883720336 -0.00012193093537209886; -5.54742825427106e-5 2.5849767443424473e-5 -0.0001337513594711011; -0.00019794414385452915 -0.00032359234100760197 -0.000631925222085503; 2.231779451480098e-6 0.00011838883407374892 0.00011126627900560291] %

Mass Used: 79.97504289779272 kg
Launch C3: 97.52896374514604 km²/s²
||V∞_in||: 5.21477444990475e-9 km/s