archive/ES_0.5674516581713827---------------------------

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: 2023-05-02T13:52:51.771
Launch V∞: [6.63651511234221, -7.411757998154956, 0.16794491749541263] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [3.600269623236405e-7, -3.405748245232093e-7, -4.005973004650344e-7] km/s
	V∞_out: [-5.167547600015091e-7, -3.1064646883101867e-7, -9.498686057984501e-9] km/s
	time of flight: 1.8749577787471753e8 seconds
	arrival date: 2029-04-10T16:02:28.771
	thrust profile: [0.16443526663303384 -0.04300985325677338 -0.06373133172551369; 0.022149230402439064 0.005144720513601866 -0.022152811982333133; 0.045848751454602175 0.021665156557054532 -0.09109044419236217; 0.04630589799843643 0.029824017565015647 -0.12846972791929445; 0.048981330669423485 0.03690565394741575 -0.17387963970836237; 0.04191402722166129 0.034852259204891455 -0.17826452149590605; 0.010774215842308235 0.009981413228998974 -0.059212188300755184; 0.011644129737341014 0.009182174873016941 -0.0501104069277831; 0.012475303083749424 0.000927515156295881 -0.050717197094707026; -0.0007172180444077136 0.0006042005115948477 -0.00859261522438617; 0.004228558335815281 0.0008988100391302781 -0.017096010849607362; -0.005055434549449866 -0.0010826441447762596 0.005410100656348212; -0.0032893966476105667 0.010595476206741585 -0.018940515817862255; -0.006574055228514127 0.010908223262711285 0.0009493741662257153; -0.0035930970845927802 0.004717053182704411 0.006596974047920898; 0.0011004709630278789 -0.002804592659570458 -0.0015095424062064671; -0.006538277228227252 -0.007261353565214913 -0.006381571212558587; -0.00873510430455629 0.001966591115642455 0.003867789618249351; 0.010684598543229767 -0.030328431452260787 -0.0010379904666724033; 0.001998968396780912 -0.0026757155543232717 -0.0018400072961115657] %

Mass Used: 84.49371396318702 kg
Launch C3: 99.00569495487304 km²/s²
||V∞_in||: 6.372509881034912e-7 km/s