archive/ES_0.5675872770426034---------------------------

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: 2024-05-08T09:30:30.388
Launch V∞: [7.423840754763571, -5.993486665511341, -0.3805250385681088] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.8575731844542856e-10, 2.651831628723303e-9, -2.0731797999487318e-9] km/s
	V∞_out: [1.4411491528421186e-9, 2.975622768429407e-9, 7.66097793706461e-11] km/s
	time of flight: 1.819774341160874e8 seconds
	arrival date: 2030-02-12T14:47:44.388
	thrust profile: [0.4919297650391586 0.01668617690597681 -0.10123177133865217; 0.2855293083654524 0.20523684476309176 -0.18654523127872458; 0.13862321831822033 0.17345551414052524 -0.17294110844439087; 0.06398287405382841 0.11056335390464357 -0.12558827166237493; 0.04362948887020997 0.10111323904006324 -0.12355611139788192; 0.02101016232834756 0.06127240466552729 -0.08168872483023888; 0.014391016312139977 0.05073332936775758 -0.07192658282512956; 0.005918492485722643 0.02746460390463617 -0.04163292750550281; 0.0002844704612067493 0.0029692129226568183 -0.006492799445297629; 0.0004776332918575937 0.0015407898453700655 -0.002232158510909608; 0.0008472656311632805 0.0022629556482613713 -0.003787092414417667; 0.0006598846449721023 -0.000276919946998791 0.00029106325619180143; -0.0003653239110435859 0.00023328725788551634 -0.0007979279521709751; 4.132927390874865e-5 -9.396254501798447e-5 0.00032477604860064774; 0.0019614450625192906 -0.001296330442514372 0.000666683506263239; -0.0010122908423282383 -0.00134674621523986 0.00128733918124626; -8.372254255323351e-5 -0.0001775617355963229 0.0003861155383553276; 0.0003836389362796312 -0.0015656680955269465 0.0028286848901242995; -0.0013191437674364107 0.001664309787850797 0.0007976406722698304; -0.0007212691900268222 -0.0005821740476965626 0.00017438514444238437] %

Mass Used: 130.30127916045694 kg
Launch C3: 91.18009326672805 km²/s²
||V∞_in||: 3.3781567037450867e-9 km/s