archive/ES_0.5663740952672771---------------------------

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: 2023-05-01T17:55:55.403
Launch V∞: [6.583334535087103, -7.427288338899205, 0.11382310149702253] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-6.907972380885023e-8, 1.0747350999082834e-7, 7.61955180432935e-8] km/s
	V∞_out: [-3.5615785178365307e-8, 7.879324878210975e-8, -1.1850222185153701e-7] km/s
	time of flight: 1.860001076632514e8 seconds
	arrival date: 2029-03-23T12:37:42.403
	thrust profile: [0.17177766302561517 -0.047779466832964114 -0.0654978740197048; 0.04991529262827161 0.010981929248579325 -0.0582815059057979; 0.061068386172672524 0.027540184109749625 -0.11874603835719369; 0.06080643825410009 0.03681400457351515 -0.16360316475170392; 0.04542418992809965 0.03272823946481818 -0.15653803201309066; 0.02750957047504217 0.022253672584880386 -0.11671759761836571; 0.011532826954948781 0.009990429275963095 -0.05789067354911983; 0.005879562029262534 0.005419971461820461 -0.03357212276089584; 0.007112176353615891 0.006813501584887533 -0.04425624123162434; 0.0056921099590958885 0.005199081145811089 -0.03419510423103766; 0.0028515898442818145 0.0023921876360134143 -0.017938184651648627; -0.0008234853933764138 0.0010415800701535295 -0.00667123220144056; 0.0011209183425556204 -0.0016047422965183638 0.0006560317392395355; 0.006617756224059108 0.012875060292201698 -0.004454779853044795; 0.009447120282848425 -0.0014294340684349476 -0.004721183955322417; -0.01282058335082275 -0.007127068100516965 -0.019609579151216715; -0.0005200639140423733 -0.0009046935945238141 0.0038288920031971756; 0.0008499508278294082 0.0052350024906229475 0.007443070625035671; 0.004715064200811622 0.007251162157120081 -0.014011364238889965; -0.0022962285131022287 0.003809422855117624 0.009020319540318341] %

Mass Used: 86.08225316251401 kg
Launch C3: 98.51786136845303 km²/s²
||V∞_in||: 1.4875590933183654e-7 km/s