archive/ES_0.5596636167122055---------------------------

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: 2024-05-12T20:22:37.175
Launch V∞: [7.965190460328733, -5.622653511103036, 0.0101282892367901] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.782423658195696e-9, 5.40622209358256e-9, 2.943405525873186e-9] km/s
	V∞_out: [4.936408393870634e-9, -4.7701421454792045e-9, -2.847349721626374e-9] km/s
	time of flight: 1.873184671347415e8 seconds
	arrival date: 2030-04-19T21:17:04.175
	thrust profile: [0.4471499071901701 0.010543968340600347 -0.12440716012301897; 0.06659668691191227 0.04309259588116524 -0.07177642151525607; 0.06333421049979894 0.06765133805425526 -0.12118119011354384; 0.03277686434289246 0.04758712377190952 -0.09672496661307102; 0.01603843582096584 0.02938921528227259 -0.06679687241883515; 0.012701384333523242 0.028668699884011325 -0.07202106161919423; 0.011076654000790092 0.03063054034988422 -0.08218470102807356; 0.012830988243824708 0.03981178253415083 -0.10655720971283322; 0.005511380989898838 0.02687212836538729 -0.07336976783964312; 2.9818842239592988e-5 0.0010362379061746975 -0.005734712972967346; 0.00038582566317230853 -6.420708633914161e-5 7.816118542539724e-5; 0.0009955799842781563 -0.0009733208240890431 -0.0014490970765884158; 0.0008553906889067525 -0.00026312102303960717 0.0002741674001525109; -0.0003973792866319458 0.000996014116898926 0.0005693624308721807; -0.004595931935174298 -0.0038135443712606332 -0.001100374724233598; 0.008822537553335012 -0.004183459956757467 -0.00020164845467261858; 0.0016028639669512733 -0.0007455909112100562 0.003549011848314632; -0.004825432702531668 -0.004050925561105311 -0.002133835845858946; -0.0012801895584931503 -0.0019300519232302916 0.0019003249142780939; 0.004320033820435045 -0.006250149680080806 0.004645613392965233] %

Mass Used: 98.43242024564142 kg
Launch C3: 95.05859415747402 km²/s²
||V∞_in||: 6.755202056827621e-9 km/s