archive/ES_0.6135038202485792---------------------------

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: 2023-04-23T06:37:06.702
Launch V∞: [5.474538436552993, -8.64375343212144, -1.9278979168207633] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.045427238415002034, -0.0008531877779234282, 0.03322727445508061] km/s
	V∞_out: [-0.05507153556718313, 0.00046388659353478425, 0.011659321332444112] km/s
	time of flight: 1.1644321560338825e8 seconds
	arrival date: 2026-12-30T23:57:21.702
	thrust profile: [0.25902005223915875 -0.19269423015921627 -0.16575329041697967; 0.1709292135449643 -0.033613062100065254 -0.20360527100560463; 0.14068052235433134 0.0017488664962963534 -0.2432417895394372; 0.11040920241753252 0.014391216266190235 -0.24523995552500458; 0.07690555903671736 0.016041551283860457 -0.2060264420622446; 0.05176893566966967 0.013135095054262106 -0.15802500504430167; 0.03300534347308805 0.009099541719109731 -0.1083680028951355; 0.009420718427822456 0.002532536538335413 -0.037329822442185565; 0.004781181730293025 0.001628815875270554 -0.01834721282731855; 0.007743313459518287 0.0028361770989002084 -0.032320085453963886; 9.379171511853012e-5 0.001423760054072556 -0.003082428169712336; 0.0007411709613559403 3.682462009501241e-5 -0.0017062578280264474; 0.00020973696426396227 0.00012406724571751982 -0.0034663101084456997; 0.00043872538058149877 4.476262423569683e-5 -0.0011979890439457576; -0.0001368676779693014 -2.3820809096965993e-5 -0.00011265454911072413; -0.001380318683549747 -0.0010358763402151263 0.002267981354270303; 0.0007993158127090807 0.0002364201479942321 -0.0009234438312467133; 0.0007110073305852693 0.0007177466438188632 0.00020904310476371128; 0.0008697294745241185 -0.000545853289342793 0.0027919217941983904; 0.0015145391202897242 -0.0011166441600782885 -0.007296808812526631] %

Mass Used: 83.41042023665614 kg
Launch C3: 108.40183486628908 km²/s²
||V∞_in||: 0.056288663930769284 km/s