archive/ES_0.6486596222028239---------------------------

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: 2023-04-24T09:59:44.226
Launch V∞: [5.830408074451337, -8.825822567513498, -2.6898887561310563] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.00011718407187143226, -5.8970262971872454e-5, -0.00011660839083741748] km/s
	V∞_out: [3.477897306467986e-5, -0.0001227836724987138, 0.00012054562018379542] km/s
	time of flight: 1.0156283990566225e8 seconds
	arrival date: 2026-07-12T21:53:43.226
	thrust profile: [0.4055180953143717 -0.3152793861573408 -0.240784792038166; 0.23198340629136402 -0.05375005295986878 -0.21798838059892867; 0.11237222522605922 -0.0004689370651070596 -0.14606075179592645; 0.0491787229675948 0.006392726371608967 -0.0813302351607685; 0.030692946211900024 0.006300253917142578 -0.059845648235551684; 0.054939067064415856 0.017082737783862163 -0.1044453237619567; 0.0176030163357231 0.0048926441065403 -0.036372158154079584; 0.007093019010405424 0.002307013446454554 -0.01814411373389241; 0.02083256671310199 0.007814962309859806 -0.05364039413078733; 0.004857402462188891 0.0006781516511852308 -0.0020322516349163765; 0.0017119481206351159 0.0015220149477430602 -0.002424312774745002; -0.0011855028138625262 0.0010200303447772834 -0.0013119516040686772; 0.0016234345883404163 5.703654231008926e-5 -0.0012685024157802224; 0.005012495533830152 -0.00315115277546692 -0.0008406168568823324; 0.004604314572059195 0.006515405088766083 -0.0048308321454872405; 0.0007996437905995761 -0.0002362441829434561 -0.0018818250147130378; -0.006034305637915193 -0.0006500774366992601 -0.0021679994781411563; -0.0025774937493595043 0.0013129231172193541 0.0017006162416272866; 0.006109934706288331 0.0024775307547599506 -0.005153330157386858; -0.0021081546339124448 0.004122522098945839 0.005138826839157156] %

Mass Used: 61.87778690535515 kg
Launch C3: 119.12430382821819 km²/s²
||V∞_in||: 0.0001755195585370266 km/s