archive/ES_0.5650117562897803---------------------------

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: 2023-04-30T13:34:54.684
Launch V∞: [6.641857042051145, -7.342694412230446, 0.08892534612791025] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.009778854831442814, -0.0002890292931707255, 0.006528362546980653] km/s
	V∞_out: [-0.011277635792272424, 0.00010950620246591982, 0.003316412392858195] km/s
	time of flight: 1.8749577787483868e8 seconds
	arrival date: 2029-04-08T15:44:31.684
	thrust profile: [0.17431680448760167 -0.04176441097203346 -0.05908544502195798; 0.069390986040397 0.01989811777418745 -0.0682670193420096; 0.07709908148464197 0.042737765959599126 -0.12810301640262436; 0.06457446722023936 0.04787536866037427 -0.14797163223358786; 0.056056068188067354 0.05028803711541609 -0.1625993427746123; 0.03576901518780513 0.03521073497442765 -0.1212153365827561; 0.012884158836863023 0.020001959945255658 -0.05823325938676115; 0.004071584372422746 0.00853843787885133 -0.029502082917042934; 0.00757170817587902 0.012218231212635058 -0.03938920483068942; 0.005750112268380684 0.004550189164889187 -0.01910662876357168; 0.0008476659161366694 -0.0010710740788114244 -0.010128564476232777; 0.0015105394900769109 0.003189710981956118 -0.012513452625592425; 0.003548145176426214 -0.0025567241919159382 -0.005185135907461184; -0.0004857953277653935 -0.0007916713105497622 0.0022870581635773763; 0.004438032759544429 0.003793003756042758 -0.0069279227515909175; -0.00688530035942535 0.0022260915985163852 0.0017006189050458014; 0.0034687100687843357 -0.00433788663596487 -0.011519443419041743; 0.00817247572642714 0.0029896246900799357 -0.009042444590233392; -0.002793238910097407 0.0018084797433586314 -0.00840361478635135; -0.0016490261970687464 -0.0034482674390600068 0.006166256108593031] %

Mass Used: 87.29593449691038 kg
Launch C3: 98.03733391562857 km²/s²
||V∞_in||: 0.011761337393832512 km/s