archive/ES_0.56015008448963---------------------------

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: 2024-05-13T00:31:20.401
Launch V∞: [7.739586967611511, -5.81694516772151, 0.1656871023210437] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [2.984956769822344e-8, 1.053112476240227e-7, -1.467406006554363e-8] km/s
	V∞_out: [3.2308832548078255e-8, 6.425995417585346e-8, 1.5836415408430052e-9] km/s
	time of flight: 1.8735229396593234e8 seconds
	arrival date: 2030-04-20T10:49:33.401
	thrust profile: [0.4088730297211385 0.01422038467959477 -0.099817717834136; 0.23886723820231034 0.16545714120752594 -0.19412857388508722; 0.044899886386895974 0.0517295099456061 -0.07827562358062098; 0.034946165682723164 0.059106831577206795 -0.09622591657502039; 0.02127466907425809 0.044964210937194965 -0.08466894706693895; 0.012855064022270667 0.03652362946310989 -0.07080651007861932; 0.016038692071298155 0.05386048037379311 -0.10856788147942699; 0.0065449534078038454 0.02587647773913631 -0.055959103612853583; 0.00046400710283102246 0.0036198479901024603 -0.008545138766712628; -0.0003186635252487766 0.00015883317735548448 -0.000414704409304814; -0.0004695589454897695 0.0005133188851025941 -0.0023255036986977594; 0.0007954358275000411 0.0025300563841010345 -0.003210107449297748; -0.0014723415048132078 0.004751746126128662 -0.003368777490346894; 0.006503111734937828 0.005647577718409438 -0.012290063972093326; 3.136276653229532e-5 -4.9667334002895854e-5 -0.00229268178241992; 0.006157277508586682 -0.0025135456961985136 -0.007159902706785126; 0.002291396215495209 0.0001347783037447996 -0.0004171336250216027; -0.001430998368702404 0.002575388598243115 -0.012476363977754526; -0.004012561843802845 0.0038185006803433323 -0.004447948594051887; -0.00012699111396066048 9.136227650836633e-5 -0.0004006433187695004] %

Mass Used: 106.54295848320771 kg
Launch C3: 93.7655097293761 km²/s²
||V∞_in||: 1.1043904928378474e-7 km/s