archive/ES_0.5589242185811312---------------------------

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: 2024-05-11T06:07:19.671
Launch V∞: [7.728685570579666, -5.7792261495067105, 0.2156552918068296] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.07754725653451996, -0.44268819428603867, -0.6405477545232795] km/s
	V∞_out: [0.33481763272328174, 0.15914039343352784, 0.6885834960480645] km/s
	time of flight: 1.841807229846551e8 seconds
	arrival date: 2030-03-12T23:26:01.671
	thrust profile: [0.5150434592312306 0.003645514858358353 -0.12468356040152485; 0.1869753317868984 0.120316458507851 -0.16300237737969006; 0.0417517204323041 0.045062059611664526 -0.07294597233987189; 0.02744217151788338 0.03943495374500119 -0.07222407967415895; 0.028717317090825964 0.056238595403451504 -0.10676639913110977; 0.03413984157255523 0.07885456221314993 -0.1567465961348576; 0.013783935631017902 0.036476450411204224 -0.0826210404235288; 0.006108854938174416 0.020747095736963893 -0.04918717935990979; 0.0012367544427133754 0.005754204056422212 -0.013713163116784612; 0.0008632095343847066 0.003628621968725169 -0.010647512593448812; 7.137905239831553e-5 0.0006950847766475539 -0.001107913344465886; 0.00024748809425791313 0.00036090341828721464 -0.0018473799239923055; 9.11632490002281e-5 -0.00016166271180565362 0.0004873260190136556; -0.00035193174937943046 0.0005727682207522177 -0.0005356209248846633; -1.0890626177853363e-5 -0.0006754304160792631 -0.0006983794652851366; -8.433848487500242e-5 -0.00032124304569903595 -0.001023367669028189; 0.0005323620724780574 0.001924646261608525 0.0027608856760679; 0.0011160472678325465 0.0004512445158302769 0.0012500763711584524; 0.0010712611814912738 -0.0011757990690148654 -0.002701605641069247; 0.001119094554187083 -0.002264099284977592 0.0019442458692963823] %

Mass Used: 108.5367556893284 kg
Launch C3: 93.17854274091279 km²/s²
||V∞_in||: 0.7824882364490087 km/s