archive/ES_0.5614687340958586---------------------------

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: 2024-05-10T10:37:10.041
Launch V∞: [8.0030579532713, -5.549546602667367, 0.08590361300954108] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [5.913175986933657e-7, -5.138174478963414e-6, 9.273149853035128e-7] km/s
	V∞_out: [-7.109139198077547e-7, 2.8550204814148046e-6, 4.318177380329509e-6] km/s
	time of flight: 1.8749577783679882e8 seconds
	arrival date: 2030-04-19T12:46:47.041
	thrust profile: [0.3781040548473894 0.019197378010033857 -0.09028541454091026; 0.14352525702567082 0.09432293878001174 -0.12535932691749135; 0.11743469521557719 0.1300831159146008 -0.1800044480281703; 0.03837638349673106 0.0631802166778748 -0.1035737999056608; 0.027087493619361244 0.058771474558190345 -0.10076488296588974; 0.0156614549286831 0.04191456225030813 -0.08101276112417818; 0.005004853699870046 0.017931573928163403 -0.03597642937569976; 0.006465184371527864 0.029058109698521496 -0.06158595257350754; -0.0002712680772862812 0.006137224418128583 -0.015158205150232279; 0.0002487861015250756 0.005251645642147462 -0.008631307067803077; 0.0009961612752937372 2.527023403774294e-5 -0.0028370864917238283; 0.0014800338430213933 -0.00042745732060745075 -0.0007917658614868335; 0.0003241261910803301 -3.192216530258432e-5 0.00010787771340109876; 2.280644907537194e-5 -0.0004240260556768067 -0.0009605103777238768; 0.0018490439294374997 -0.0010725399509246571 0.0010071595157740074; -0.0034879054583141287 0.002372885898044076 -0.0010967553413251622; 0.0011058564668276192 -0.006889943348802995 -0.0015897634593512577; 0.0005514490916645408 0.0003485275207663507 -0.009837517975703654; 0.0005331339220343974 -0.002777760622212732 -0.0013402958548325429; 0.00029202022310064 0.0016209086832611607 6.697988683405953e-5] %

Mass Used: 101.73311919077832 kg
Launch C3: 94.85378352932402 km²/s²
||V∞_in||: 5.254560548777023e-6 km/s